{"id":3545,"date":"2026-09-16T10:58:46","date_gmt":"2026-09-16T07:58:46","guid":{"rendered":"https:\/\/www.defencemetal.com\/index.php\/en\/nimonic-80a\/"},"modified":"2026-09-25T16:25:42","modified_gmt":"2026-09-25T13:25:42","slug":"nimonic-80a","status":"publish","type":"page","link":"https:\/\/www.defencemetal.com\/index.php\/en\/nimonic-80a\/","title":{"rendered":"Nimonic 80A \/ ASTM B637"},"content":{"rendered":"<p><!-- dm-hap --><\/p>\n<h1 class=\"dm-ust-baslik\" style=\"font-family:-apple-system,BlinkMacSystemFont,'Segoe UI',Helvetica,Arial,sans-serif !important;text-transform:none !important;font-size:27px;line-height:1.3;font-weight:800;color:#12303f;margin:0 0 10px;letter-spacing:-.01em;\">Nimonic 80A \/ UNS N07080 \/ ASTM B637<\/h1>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:0 0 22px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"background:#12303f;padding:14px 16px 12px;position:relative;z-index:2;\">\n<div style=\"font-size:22px;font-weight:700;color:#fff;line-height:1.25;\">Nimonic 80A<\/div>\n<div style=\"font-family:ui-monospace,Menlo,Consolas,monospace;font-size:12.5px;color:#b9cfdb;line-height:1.5;margin-top:5px;word-wrap:break-word;\">UNS N07080 \u00b7 W.Nr. 2.4952 and 2.4631 \u00b7 NiCr20TiAl \u00b7 18.0-21.0% Cr \u2013 1.8-2.7% Ti \u2013 1.0-1.8% Al \u2013 balance Ni. Strengthening comes from the \u03b3\u2032 (Ni\u2083(Al,Ti)) precipitate formed by titanium and aluminium; the alloy contains no niobium.<\/div>\n<div data-dmkars-blok=\"1\" style=\"border-top:1px solid rgba(255,255,255,.16);margin-top:13px;padding-top:11px;\">\n<div style=\"font-size:10px;letter-spacing:.09em;text-transform:uppercase;color:#7f9fb0;font-weight:700;margin-bottom:8px;\">Not to be confused with<\/div>\n<p><a href=\"https:\/\/www.defencemetal.com\/index.php\/2026\/09\/16\/nimonic-80a-waspaloy-difference\/\" data-dmkars=\"1\" style=\"display:inline-block;padding:4px 11px;border:1px solid rgba(36,190,229,.45);background:rgba(36,190,229,.12);border-radius:99px;margin:0 6px 6px 0;font-size:12.5px;font-weight:600;color:#9fe2f7;text-decoration:none;\">Waspaloy<\/a><\/div>\n<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">For what<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">Bought for parts that must carry load and resist creep at high temperature: gas turbine blades, rings and discs, high-temperature bolting and fasteners, and automotive exhaust valves. Producer technical bulletins define the alloy for service up to 815 \u00b0C (1500 \u00b0F).<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Forms<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">Round bar \u00b7 flat bar \u00b7 plate \u00b7 sheet \u00b7 tube \u00b7 forging. All forms supplied to order.<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Standards<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">NO AMS SPECIFICATION. The only specification for this alloy that four independent sources confirm is ASTM B637 \/ ASME SB-637 (UNS N07080; rod, bar, forgings and forging stock). ASTM B637 does NOT cover flat product (plate, sheet, strip) or tube.<br \/><span style=\"font-size:12.5px;color:#7b8f9b;line-height:1.6;display:inline-block;margin-top:6px;\">The AMS numbers shown on the page could not be confirmed. AMS 5829 belongs to Nimonic 90 (UNS N07090), not to this alloy;<\/span><\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Advantage<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">After precipitation hardening the ASTM B637 minimums are 930 MPa tensile strength, 620 MPa yield strength and 20% elongation, and the same material is used in continuous service to 815 \u00b0C.<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Welding<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">Sheet is joined by the resistance welding processes. TIG and MIG fusion welding is usable on thin sections; as the section gets thicker, micro-fissuring appears in the weld and in the heat affected zone. Post-weld heat treatment is necessary to restore properties.<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#fdeceb;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#c0392b;font-weight:600;line-height:1.5;\">Limits<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;background:#fdeceb;\">The service temperature ceiling is 815 \u00b0C; the producer bulletins define the alloy up to that temperature. Because ageing is carried out at 690-710 \u00b0C, long-term service above that temperature coarsens the \u03b3\u2032 precipitate and the hardening effect falls away \u2014 this mechanism is why the service ceiling is held at 815 \u00b0C;<\/div>\n<\/div>\n<div style=\"padding:14px;border-top:1px solid #eceff1;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/contact\/\" style=\"display:inline-block;padding:11px 20px;font-size:14px;font-weight:700;text-decoration:none;margin:0 8px 6px 0;background:#dd3333;color:#ffffff;\">REQUEST A QUOTE<\/a><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/nickel-alloys\/\" style=\"display:inline-block;padding:11px 20px;font-size:14px;font-weight:700;text-decoration:none;margin:0 8px 6px 0;font-weight:600;border:1px solid #12303f;color:#12303f;\">All nickel alloys &rarr;<\/a><span data-dm=\"dm-teknik\" style=\"cursor:pointer;display:inline-block;padding:11px 20px;font-size:14px;font-weight:700;text-decoration:none;margin:0 8px 6px 0;border:1px solid #dd3333;color:#dd3333;\">TECHNICAL DETAILS &darr;<\/span><\/div>\n<div style=\"padding:9px 14px;border-top:1px solid #eceff1;font-size:11.5px;color:#8a9aa4;line-height:1.5;\">Compiled from manufacturer data sheets \u00b7 confirm against the current specification before ordering<\/div>\n<\/div>\n<\/div>\n<p><!-- \/dm-hap --><!-- dm-nav --><\/p>\n<style>h4[id^=\"dm-b\"]{scroll-margin-top:120px}#dm-teknik{scroll-margin-top:120px}<\/style>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:0 0 22px;padding:12px 14px;\">\n<div style=\"font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;margin-bottom:9px;\">On this page &middot; click to jump<\/div>\n<div><span data-dm=\"dm-b0\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">What Nimonic 80A Is<\/span><span data-dm=\"dm-b1\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Standards by Product Form<\/span><span data-dm=\"dm-b2\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">ASME Code Acceptance and Code Temperatures<\/span><span data-dm=\"dm-b3\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Product Forms With NO Standard<\/span><span data-dm=\"dm-b4\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Chemical Composition<\/span><span data-dm=\"dm-b5\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Mechanical Properties<\/span><span data-dm=\"dm-b6\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Physical Properties<\/span><span data-dm=\"dm-b7\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Heat Treatment and Thermal Stability<\/span><span data-dm=\"dm-b8\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Welding<\/span><span data-dm=\"dm-b9\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Machining<\/span><span data-dm=\"dm-b10\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Corrosion<\/span><span data-dm=\"dm-b11\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Frequently Asked Questions<\/span><span data-dm=\"dm-b12\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Common Datasheet Errors and Traps<\/span><\/div>\n<\/div>\n<p><script>(function(){function go(id){var e=document.getElementById(id);if(e){var s=document.scrollingElement||document.documentElement;var y=e.getBoundingClientRect().top+s.scrollTop-118;if(y-0-0-0-0!==y){y=0;}window.scrollTo(0,y);}}function bind(el){el.addEventListener(\"click\",function(ev){ev.preventDefault();go(el.getAttribute(\"data-dm\"));});}function init(){var l=document.querySelectorAll(\"[data-dm]\");Array.prototype.forEach.call(l,bind);if(location.hash){if(location.hash.indexOf(\"#dm-\")===0){try{history.replaceState(null,\"\",location.pathname+location.search);}catch(e){}window.scrollTo(0,0);setTimeout(function(){window.scrollTo(0,0);},80);}}}if(document.readyState===\"loading\"){document.addEventListener(\"DOMContentLoaded\",init);}else{init();}})();<\/script><!-- \/dm-nav --><br \/>\n<span id=\"dm-teknik\" style=\"display:block;height:0;overflow:hidden;\"><\/span><br \/>\nNimonic 80A is a nickel-based superalloy, alloyed with chromium and hardened by ageing. Within the nickel alloy group it stands out for holding its mechanical strength over long periods in the 650-850 \u00b0C range. Its UNS designation is N07080.<\/p>\n<p>Its hardening mechanism rests on the \u03b3\u2032 (Ni\u2083(Al,Ti)) precipitates formed by the titanium and aluminium additions. This precipitate phase gives high resistance to the softening that comes with temperature. The combined Ti and Al content is normally held in the 3.5-4% range, which is the critical threshold for forming the \u03b3\u2032 phase.<\/p>\n<p>Oxidation resistance is very high at service temperatures up to 900 \u00b0C. Resistance to thermal fatigue under repeated thermal cycling, and easier weldability than other nickel superalloys, are the alloy&#8217;s outstanding practical advantages.<\/p>\n<p>It is used for gas turbine blades, seals, brackets and fastening components; in nuclear power for in-reactor components and high temperature bolting; and in automotive and motorsport for turbocharger wheels and exhaust systems. It carries NACE MR0175 \/ ISO 15156-3 approval for H\u2082S-bearing environments.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Chemical Composition \u00b7 Nimonic 80A (N07080)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Ni \u2014 Nickel<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">76% (bakiye)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Cr \u2014 Chromium<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">19.0 \u2013 21.0%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Ti \u2014 Titanium<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">1.8 \u2013 2.7%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Al \u2014 Aluminium<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">1.0 \u2013 1.8%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Fe \u2014 Iron<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">3.0% max<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">C \u2014 Carbon<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">0.10% max<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Mn \/ Si<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">1.0% max<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Mechanical and Physical Properties \u00b7 Age Hardened<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Tensile strength (R<sub>m<\/sub>)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">1000 \u2013 1200 MPa<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Yield strength (R<sub>p0.2<\/sub>)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">700 \u2013 850 MPa<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Elongation<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">15 \u2013 20%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Service temperature range<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">-200 \u00b0C \u2026 850 \u00b0C<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Density<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">8.19 g\/cm\u00b3<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Melting range<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">1320 \u2013 1380 \u00b0C<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div class=\"dm-std\" style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Standards and Equivalents \u00b7 Nimonic 80A<\/div>\n<div data-dmtw=\"1\" style=\"position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;overflow-x:auto;\">\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Trade name<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Nimonic 80A<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">UNS<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">N07080<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">AMS<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">4378 \u00b7 5829<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Available forms<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Round bar \u00b7 Flat bar \u00b7 Plate \u00b7 Sheet \u00b7 Tube \u00b7 Forgings<br \/><span style=\"font-size:13px;color:#6b7a84;\">All forms are supplied to order.<\/span><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"margin:28px 0 0;padding:14px 16px;border:1px solid #e0e0e0;background:#FBFCFD;font-size:15px;line-height:1.7;\">\n<p style=\"margin:0 0 10px;\"><span style=\"color:#DD3333;font-weight:700;\">\u2192<\/span> Contact us for Nimonic 80A stock availability, sizes and ASTM B637 certified supply.<\/p>\n<p style=\"margin:0;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/contact\/\" style=\"display:inline-block;background:#DD3333;color:#ffffff;font-weight:700;font-size:14px;padding:9px 16px;text-decoration:none;\">Request a quote<\/a><\/p>\n<\/div>\n<div style=\"margin:22px 0 0;padding:14px 16px;border:1px solid #e0e0e0;background:#FBFCFD;\">\n<p style=\"font-size:11px;font-weight:700;letter-spacing:.08em;text-transform:uppercase;color:#9aa3a8;margin:0 0 8px;line-height:1.4;\">Related grades<\/p>\n<p style=\"margin:0;font-size:15px;line-height:2;color:#333;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-x750\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Inconel X750<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/waspaloy\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Waspaloy<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-718\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Inconel 718<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/hastelloy-x\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Hastelloy X<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/nickel-alloys\/\" style=\"color:#666;font-weight:600;text-decoration:none;\">All nickel alloys \u2192<\/a><\/p>\n<\/div>\n<p><!-- dm-zengin --><\/p>\n<h4 id=\"dm-b0\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">What Nimonic 80A Is \u2014 Nichrome With Titanium and Aluminium Added<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">Nimonic 80A (UNS <b>N07080<\/b> \/ W.Nr. <b>2.4952<\/b> and <b>2.4631<\/b> \/ EN chemical name <b>NiCr20TiAl<\/b> \/ AFNOR <b>NC 20 TA<\/b> \/ BS <b>NA20<\/b>) is a <b>precipitation-hardenable (age-hardenable) nickel-chromium alloy<\/b> made by adding <b>1.8\u20132.7 % titanium<\/b> and <b>1.0\u20131.8 % aluminium<\/b> to a nominal <b>20 % chromium, balance nickel<\/b> matrix. Metallurgically the description is that simple: <b>80\/20 nichrome, plus just enough Ti and Al to form \u03b3\u2032<\/b>. The hardening mechanism is coherent precipitation of the ordered intermetallic <b>\u03b3\u2032 \u2014 Ni\u2083(Ti,Al)<\/b>.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The single sentence that distinguishes this alloy:<\/b> among \u03b3\u2032-hardened nickel alloys it is <b>the simplest, the cheapest and the highest in chromium<\/b> \u2014 no cobalt, no molybdenum, no niobium, effectively no iron. <b>18\u201321 % chromium<\/b> gives it the best oxidation and combustion-deposit resistance in the \u03b3\u2032 family; \u03b3\u2032 gives it hot hardness and fatigue strength at valve temperature. <b>The price is the temperature ceiling: about 815 \u00b0C under load.<\/b> Above that \u03b3\u2032 coarsens and begins to dissolve, and the alloy starts behaving like a plain solid-solution nichrome. Nimonic 80 was developed in 1941 at Wiggin in Birmingham for the first jet engine turbine blades and 80A followed in 1945; <b>it lost the turbine-blade job decades ago and the surviving commercial application, which carries the overwhelming majority of today&#8217;s tonnage, is exhaust valves in internal combustion engines.<\/b><\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Honest Positioning Against Its Siblings<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Nimonic 75<\/b><br \/>(N06075 \/ 2.4951)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>NO \u03b3\u2032.<\/b> Ti 0.2\u20130.6 %, no aluminium \u2014 a <b>solid-solution<\/b> alloy. Excellent formability and weldability, oxidation resistance to about 1000 \u00b0C, but its <b>load-carrying capacity is far below 80A<\/b>. Static furnace parts, combustor liners, exhaust ducting. <b>A certificate that confuses 75 with 80A sells a material that cannot be aged as a valve alloy.<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Nimonic 80A<\/b><br \/>(N07080 \/ 2.4952)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>The reference point.<\/b> Cr 18\u201321 \u00b7 Ti 1.8\u20132.7 \u00b7 Al 1.0\u20131.8 \u00b7 <b>Co \u22642 % (deliberately not alloyed)<\/b> \u00b7 Fe \u22643 % \u00b7 no Mo \u00b7 no Nb. <b>815 \u00b0C<\/b> under load, scaling resistance to <b>1000 \u00b0C<\/b>. <b>The exhaust-valve alloy.<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Nimonic 90<\/b><br \/>(N07090 \/ 2.4632)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>80A plus 15\u201321 % COBALT.<\/b> Ti 2\u20133 %, Al 1\u20132 %. Cobalt lowers stacking-fault energy and raises the \u03b3\u2032 solvus; the result is <b>creep and rupture strength to about 920 \u00b0C<\/b>. <b>The price:<\/b> the cobalt itself, harder hot working, a narrower forging window. <b>This is where you go when 80A genuinely is not enough<\/b> \u2014 and only then<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Inconel X-750<\/b><br \/>(N07750 \/ 2.4669)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Cr <b>14\u201317<\/b> (lower than 80A) \u00b7 Fe <b>5\u20139 %<\/b> \u00b7 <b>Nb+Ta 0.70\u20131.20 %<\/b> \u00b7 Ti 2.25\u20132.75 \u00b7 Al 0.40\u20131.00. Niobium enters the \u03b3\u2032 and makes X-750 the <b>spring and fastener alloy<\/b>. It is <b>cheaper<\/b> (more iron, less nickel) and has a <b>far wider AMS specification family<\/b> \u2014 including sheet, tube and wire. <b>But its chromium is low: it does not replace 80A in exhaust-gas oxidation.<\/b> Detail: <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-x750\/\">Inconel X-750<\/a><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>21-4N valve steel<\/b><br \/>(X50CrMnNiNbN21-9 \/ 1.4882)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>This, not Nimonic 90, is the real commercial competitor.<\/b> A manganese-nitrogen balanced austenitic valve steel at <b>a fraction of 80A&#8217;s price per kilogram<\/b>. The exhaust valve of an ordinary petrol engine is made from it. <b>There is exactly one reason to move up to 80A:<\/b> when valve temperature and mechanical loading in a turbocharged or heavy-fuel engine exceed the hot hardness and fatigue strength of the austenitic steel<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b1\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Standards by Product Form<\/h4>\n<p><!-- dm-diy-std --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">STANDARDS BY PRODUCT FORM<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:12px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"overflow-x:auto;position:relative;z-index:2;\">\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;min-width:430px;background:transparent;\">\n<tr>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Product form<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Standards<\/th>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Round bar, flat bar, forging, forging stock<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">ASTM B637 \/ ASME SB-637 \u2014 UNS N07080. It defines the solution + stabilize + precipitation-harden cycle and the room-temperature mechanical minimums. There is no AMS number for this form.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Plate, sheet, strip<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">NO specification confirmed by four independent sources. ASTM B637 does not cover flat product. The sources cite BS HR 201, AECMA prEN 2191 and ISO 6208; none of them reached the four-source threshold.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Tube<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">NO specification confirmed by four independent sources. ASTM B637 does not cover tube. The sources cite BS HR 401; it was found in two sources.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">High-temperature bolting and fasteners<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">NO specification confirmed by four independent sources. The sources cite EN 10269 (NiCr20TiAl \/ 2.4952); it was found in two sources. There is no AMS number for this form either.<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\">Standard coverage for this alloy is NOT even across product forms: the only specification that four independent sources confirm is for bar and forgings. The plate, sheet, tube and fastener rows have candidate specifications, but none of them was found in four independent sources; when ordering those forms the acceptance route has to be set by the project specification. The BS HR numbering appears in the sources in this pattern: HR 1 for bar, HR 201 for plate, sheet and strip, HR 401 for tube. The same pattern holds for Nimonic 90 (HR 2 \/ HR 202 \/ HR 402) and Nimonic 75 (HR 5 \/ HR 203 \/ HR 403). AMS 5829 does not belong to this alloy: two independent sources list it as the Nimonic 90 (UNS N07090) rod, bar, wire and forging stock specification. That caveat rests on two sources, so it is a warning note and not diagram data.<\/div>\n<\/div>\n<p><!-- \/dm-diy-std --><\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Read this section carefully: the standards map for 80A is markedly WEAKER than for most nickel alloys.<\/b> This is a bar and forging alloy: there is no ASTM equivalent for plate, pipe or wire.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Standards by Product Form \u00b7 Nimonic 80A (N07080 \/ 2.4952 \/ 2.4631)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Rod \u00b7 bar \u00b7 forgings \u00b7 forging stock<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>ASTM B637 \/ ASME SB-637<\/b> \u2014 \u201cPrecipitation-Hardening and Cold Worked Nickel Alloy Bars, Forgings, and Forging Stock for Moderate or High Temperature Service\u201d. <b>N07080 is explicitly listed<\/b>; the other grades in scope are N07252, N07001, N07500, N07750, N07752, N07718. <b>This is the only genuine ASTM specification 80A has.<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Rod \u00b7 bar (British route)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>BS 3076 NA20<\/b> \u2014 nickel and nickel alloy round, square and hexagonal bar (hot worked 12\u2013300 mm dia., cold worked 8\u201355 mm dia.). NA20 = \u201cnickel-chromium-titanium-aluminium alloy\u201d. Also <b>BS HR 1<\/b> (bar). German route: <b>DIN 17742<\/b> (current edition <b>DIN 17742:2020-12<\/b>, superseding 2002-09) and <b>DIN 17240<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Bolts \u00b7 nuts \u00b7 studs<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>EN 10269<\/b> \u2014 \u201cSteels and nickel alloys for fasteners with specified elevated and\/or low temperature properties\u201d. <b>NiCr20TiAl \/ 2.4952 is named in it<\/b>; delivery condition <b>+AT+P<\/b> (solution annealed + precipitation hardened), <b>d \u2264160 mm<\/b>. <b>This is 80A&#8217;s strongest and clearest European specification<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>As a valve alloy<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>EN 10090<\/b> \u2014 \u201cValve steels and alloys for internal combustion engines\u201d. <b>2.4952 \/ NiCr20TiAl is one of the standard&#8217;s ten grades<\/b>, and one of only two nickel based grades (the other is <b>2.4955 \/ NiFe25Cr20NbTi<\/b>). The remaining eight are X-series steels (separate table below). Creep design data comes from <b>EN 10302<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Strip \u00b7 sheet \u00b7 plate<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>BS HR 201<\/b> \u00b7 <b>DIN EN 10302<\/b> \u00b7 <b>ISO 6208<\/b>. <b>There is NO ASTM equivalent.<\/b> ASTM B637 is bar, forgings and forging stock only \u2014 not plate or sheet<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Pipe \u00b7 tube<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>BS HR 401<\/b>. <b>Nothing else could be verified<\/b> \u2014 no ASTM, no EN, no ASME. See the \u201cno standard\u201d section below<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>ASME Section IX P-No \/ F-No<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u2014 not verified. Do not publish a number.<\/b> Precipitation-hardenable nickel alloys do not always carry a P-number in ASME IX, and no assignment for N07080 could be confirmed independently. Qualify any welded 80A joint <b>specifically for the alloy<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Where 80A sits inside EN 10090 \u2014 and its relation to the X-series<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">The Ten Grades of EN 10090 \u2014 the Whole Ladder<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Martensitic valve steels<\/b> (inlet valve, light duty)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>1.4718 \/ X45CrSi9-3<\/b> \u00b7 <b>1.4731 \/ X40CrSiMo10-2<\/b> \u00b7 <b>1.4748 \/ X85CrMoV18-2<\/b>. Quenched and tempered (+QT). Cheap, good wear resistance, <b>but they temper-soften at exhaust-side temperature<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Austenitic valve steels<\/b> (exhaust valve, medium to heavy duty)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>1.4866 \/ X33CrNiMnN23-8<\/b> \u00b7 <b>1.4870 \/ X53CrMnNiNbN21-9<\/b> \u00b7 <b>1.4871 \/ X53CrMnNiN21-9<\/b> \u00b7 <b>1.4875 \/ X55CrMnNiN20-8<\/b> \u00b7 <b>1.4882 \/ X50CrMnNiNbN21-9<\/b>. This is the <b>\u201c21-4N\u201d family<\/b>: Mn and N stabilise the austenite, Nb precipitates carbides and nitrides. Usually delivered <b>+AT+P<\/b> \u2014 <b>the same condition code as 80A<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Nickel-base valve alloys<\/b> (exhaust valve, heaviest duty)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>2.4952 \/ NiCr20TiAl (= Nimonic 80A)<\/b> \u00b7 <b>2.4955 \/ NiFe25Cr20NbTi<\/b>. <b>The top rung of the standard<\/b> \u2014 where you go, without leaving the standard, when the hot hardness and fatigue strength of the austenitic steel run out<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>2.4952 versus 2.4955<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>NiFe25Cr20NbTi contains iron<\/b> (nominally about 25 %) and hardens with niobium \u2014 broadly A-286 \/ alloy 901 logic, and <b>cheaper<\/b>. <b>NiCr20TiAl (80A) is effectively iron-free<\/b> and hardens with \u03b3\u2032. 80A buys higher temperature capability; 2.4955 is the cost-performance rung. For iron-base precipitation-hardened equivalents see <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/incoloy-a286\/\">A-286<\/a> and <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/incoloy-925\/\">Incoloy 925<\/a><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>What this means for selling<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>There is no such material as \u201cEN 10090 valve steel\u201d.<\/b> If a customer says EN 10090 you must ask <b>which grade<\/b> \u2014 the same standard contains grades whose price per kilogram differs by an order of magnitude. <b>Finding 2.4952 in the same standard as an X-series steel does not make them interchangeable.<\/b> The only thing they share is the product form: a valve<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b2\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">ASME Code Acceptance and Code Temperatures \u2014 Where We Have To Be Honest<\/h4>\n<p><!-- dm-diy-isil --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">HEAT TREATMENT \u2014 SCHEMATIC<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:14px 12px 4px;display:flex;flex-wrap:wrap;gap:10px;align-items:stretch;\">\n<div style=\"flex:1 1 180px;min-width:150px;background:#12303f;color:#fff;padding:12px 14px;\">\n<div style=\"font-size:12.5px;font-weight:700;letter-spacing:.06em;line-height:1.35;\">1 \u00b7 SOLUTION TREATMENT<\/div>\n<div style=\"font-size:12.5px;line-height:1.5;margin-top:4px;opacity:.88;\">1050-1080 \u00b0C (1922-1976 \u00b0F)<br \/>8 hours<\/div>\n<\/div>\n<div style=\"flex:1 1 180px;min-width:150px;background:#c0392b;color:#fff;padding:12px 14px;\">\n<div style=\"font-size:12.5px;font-weight:700;letter-spacing:.06em;line-height:1.35;\">2 \u00b7 COOL<\/div>\n<div style=\"font-size:12.5px;line-height:1.5;margin-top:4px;opacity:.88;\">air<\/div>\n<\/div>\n<div style=\"flex:1 1 180px;min-width:150px;background:#1b7f4b;color:#fff;padding:12px 14px;\">\n<div style=\"font-size:12.5px;font-weight:700;letter-spacing:.06em;line-height:1.35;\">3 \u00b7 AGEING<\/div>\n<div style=\"font-size:12.5px;line-height:1.5;margin-top:4px;opacity:.88;\">see the table below<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 10px 0;\"><svg viewBox=\"0 0 740 148\" style=\"width:100%;height:auto;display:block;\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\" role=\"img\"><line x1=\"70\" y1=\"68\" x2=\"690\" y2=\"68\" stroke=\"#9fb0ba\" stroke-width=\"2\"\/><line x1=\"70.0\" y1=\"68\" x2=\"70.0\" y2=\"42\" stroke=\"#c7d2d9\" stroke-width=\"1.5\"\/><circle cx=\"70.0\" cy=\"68\" r=\"5\" fill=\"#12303f\"\/><text x=\"70.0\" y=\"34\" text-anchor=\"middle\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Stage 2<\/text><text x=\"70.0\" y=\"19\" text-anchor=\"middle\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">710 \u00b0C<\/text><line x1=\"670.0\" y1=\"68\" x2=\"670.0\" y2=\"42\" stroke=\"#c7d2d9\" stroke-width=\"1.5\"\/><circle cx=\"670.0\" cy=\"68\" r=\"5\" fill=\"#12303f\"\/><text x=\"670.0\" y=\"34\" text-anchor=\"middle\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Stage 1<\/text><text x=\"670.0\" y=\"19\" text-anchor=\"middle\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">860 \u00b0C<\/text><text x=\"370\" y=\"142\" text-anchor=\"middle\" font-size=\"11.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Ageing temperature (\u00b0C)<\/text><\/svg><\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">Solution treatment<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Solution treatment<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">1050-1080 \u00b0C (1922-1976 \u00b0F)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">8 hours<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">air<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">Solution treatment \u2014 the tolerance windows published by the three sources<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Solution treatment \u2014 the tolerance windows published by the three sources<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">1050-1080 \u00b0C (1922-1976 \u00b0F)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">8 hours<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">air<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Purpose<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Takes the \u03b3\u2032-forming titanium and aluminium into solid solution and sets the starting condition for the two stages that follow.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Specifications<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Special Metals bulletin 1080 \u00b0C \u00b7 ASTM B637 \/ ASME SB-637 1066 \u00b1 14 \u00b0C \u00b7 VDM Metals 1050-1080 \u00b0C<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Standards<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Special Metals bulletin 1080 \u00b0C \u00b7 ASTM B637 \/ ASME SB-637 1066 \u00b1 14 \u00b0C \u00b7 VDM Metals 1050-1080 \u00b0C<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">Stage 1 \u2014 stabilizing treatment<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Stage 1 \u2014 stabilizing treatment<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">840-860 \u00b0C (1544-1580 \u00b0F)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">24 hours<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">air<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Purpose<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">The intermediate stage that stabilises the precipitation. All three sources give 24 hours and air cooling.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Specifications<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Special Metals 850 \u00b0C \u00b7 ASTM B637 849 \u00b1 14 \u00b0C \u00b7 VDM Metals 840-860 \u00b0C<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Note<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Full cycle: 1050-1080 \u00b0C \/ 8 h \/ air \u2192 840-860 \u00b0C \/ 24 h \/ air \u2192 690-710 \u00b0C \/ 16 h \/ air.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Standards<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Special Metals 850 \u00b0C \u00b7 ASTM B637 849 \u00b1 14 \u00b0C \u00b7 VDM Metals 840-860 \u00b0C<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">Stage 2 \u2014 precipitation hardening (ageing)<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Stage 2 \u2014 precipitation hardening (ageing)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">690-710 \u00b0C (1274-1310 \u00b0F)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">16 hours<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">air<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Purpose<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">The stage that produces the final strength. The ASTM B637 mechanical minimums apply to the completed cycle.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Specifications<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Special Metals 700 \u00b0C \u00b7 ASTM B637 699 \u00b1 14 \u00b0C \u00b7 VDM Metals 690-710 \u00b0C<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Note<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">The final stage of the cycle; this is the stage that forms the \u03b3\u2032 precipitate.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Standards<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Special Metals 700 \u00b0C \u00b7 ASTM B637 699 \u00b1 14 \u00b0C \u00b7 VDM Metals 690-710 \u00b0C<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\">Schematic: the time axis is not to scale. No published TTT or CCT curve for Nimonic 80A was used. The cycle shown is for rod, bar, forgings and forging stock (the scope of ASTM B637 \/ ASME SB-637). EN 10269 defines the material in the &#8216;+AT+P&#8217; condition (solution treated and precipitation hardened); the temperatures of that two-stage route were found in a single source only and are therefore not in the diagram. The producer bulletin additionally gives separate cycles for cold rolled sheet, for welded sheet and for interstage annealing; those cycles were found in a single source only and are not in the diagram (see the &#8216;atlananlar&#8217; list). The temperature windows of the three sources overlap; the range shown in the box is the union of the three windows, not an average.<\/div>\n<\/div>\n<p><!-- \/dm-diy-isil --><\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>This is the section most distributor pages quietly skip, and that is exactly why it is commercially valuable.<\/b><\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">ASME Status \u00b7 N07080<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>ASME SB-637<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>EXISTS.<\/b> ASTM B637 has been adopted by ASME as <b>SB-637<\/b> and N07080 is within its scope. <b>That means the material specification is adopted \u2014 it does NOT mean allowable stresses have been published for pressure design<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Section II Part D allowable stresses<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>\u2014 not verified.<\/b> Published allowable stress tables and a maximum code temperature for N07080 in Section II Part D <b>could not be independently confirmed<\/b>. <b>Do NOT publish a code temperature on this page<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>The correct sentence<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Write this to the customer: \u201c<b>N07080 has an adopted material specification as ASME SB-637. For a pressure-retaining code application, the allowable stress and maximum temperature must be confirmed project by project from the current ASME Section II Part D; as supplier we do not declare a code temperature.<\/b>\u201d <b>That sentence protects you and is also true.<\/b> On the European side the picture is clearer: <b>EN 10269<\/b> covers NiCr20TiAl 2.4952 as elevated-temperature bolting and publishes mechanical minima<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b3\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Product Forms With NO Standard \u2014 the Commercially Valuable Section<\/h4>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Specification Gaps for N07080<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Wire \u2014 cold drawn, spring wire<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>There is NO ASTM, EN or ISO wire product specification for N07080.<\/b> Wire makers list their product against <b>BS 3076 NA20, BS HR 1, BS HR 601 and ASTM B637<\/b> \u2014 <b>and none of those is a wire specification<\/b>; every one of them is a bar, rod or forging document. In practice 80A wire is sold <b>to company specification<\/b>; published typical tempers are <b>annealed &lt;1000 N\/mm\u00b2<\/b> and <b>spring temper + aged 1500\u20131800 N\/mm\u00b2<\/b> (single source). <b>The honest answer to \u201c80A wire to ASTM\u201d is: chemistry to B637, mechanical properties and temper by agreement<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Plate \u00b7 sheet \u00b7 strip<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>NO ASTM specification.<\/b> Only <b>BS HR 201<\/b>, <b>DIN EN 10302<\/b> and <b>ISO 6208<\/b>. If a customer asks for \u201c80A plate to ASTM\u201d, <b>that document does not exist<\/b> \u2014 B637 does not cover plate. Compare: <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-x750\/\">X-750<\/a> has the same gap (only AMS 5542\/5598), whereas <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-625\/\">625<\/a> and <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-600\/\">600<\/a> have complete ASTM families<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Seamless and welded pipe \u00b7 tube<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Only BS HR 401 could be verified.<\/b> No ASTM, ASME or EN pipe specification was <b>found<\/b>. If a trader offers you \u201c80A pipe to ASTM B622\u201d, <b>that specification is for Ni-Mo-Cr alloys and does not cover N07080<\/b>. Offer <b>BS HR 401 or company specification<\/b> and write it into the order acknowledgement. The same applies to forged fittings and flanges: <b>no dedicated specification exists<\/b> and parts are machined from B637 bar to the buyer&#8217;s drawing<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>NACE MR0175 \/ ISO 15156<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Listing of N07080 in ISO 15156-3 Annex A could NOT be verified.<\/b> The alloy contains <b>no molybdenum<\/b> and manufacturer pages carry no NACE statement. <b>Never issue a \u201cNACE MR0175 compliant\u201d certificate for N07080.<\/b> The nickel alloys listed for sour service are the Ni-Cr-Mo grades: <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/hastelloy-c-276\/\">C-276<\/a>, <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/hastelloy-c-22\/\">C-22<\/a>, <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-625\/\">625<\/a>, <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-718\/\">718<\/a><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b4\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Chemical Composition \u2014 ASTM and EN Describe the Same Alloy With Different Limits<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The ASTM and EN composition tables for 80A are NOT the same, and the difference genuinely matters on a certificate.<\/b> Three elements diverge: <b>aluminium, iron and cobalt<\/b>. Unless the order states which table governs, <b>a heat that passes ASTM can fail EN<\/b>.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">ASTM B637 \u00b7 UNS N07080 (weight %)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Carbon<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u22640.10<\/b> \u2014 <b>ASTM sets no lower limit<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Mn \u00b7 Si \u00b7 S<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">\u22641.00 \u00b7 \u22641.00 \u00b7 \u22640.015<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Nickel<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Remainder<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Chromium<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>18.00\u201321.00<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Titanium<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>1.80\u20132.70<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Aluminium<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>0.50\u20131.80<\/b> \u2014 <b>floor of 0.50<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Iron<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u22643.00<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Cobalt \u00b7 boron \u00b7 zirconium \u00b7 copper \u00b7 phosphorus<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>NOT LISTED in the B637 table for the N07080 row.<\/b> That does not mean \u201cunlimited\u201d; it means <b>the specification sets no limit<\/b> for those elements. Commercial practice commonly applies Co \u22642.0 %, B \u22640.008 %, Zr \u22640.15 %, Cu \u22640.2 % \u2014 <b>but those are not ASTM requirements and must be written into the order<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">EN route \u00b7 NiCr20TiAl \u00b7 W.Nr. 2.4952 (EN 10269 \/ EN 10090 \/ DIN 17742), weight %<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Carbon<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>0.04\u20130.10 \u2014 THERE IS A LOWER LIMIT.<\/b> ASTM has none. The reason is metallurgical: carbon forms grain-boundary carbides that <b>impede grain-boundary sliding and preserve creep-rupture ductility<\/b>. <b>A heat at 0.02 % carbon passes ASTM and FAILS EN<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Silicon \u00b7 manganese<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">\u22641.00 \u00b7 \u22641.00<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Phosphorus \u00b7 sulphur<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u22640.020<\/b> \u00b7 \u22640.015 \u2014 <b>ASTM sets no P limit<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Chromium<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>18.0\u201321.0<\/b> \u2014 <b>identical in both systems<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Nickel<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u226565.0<\/b> \u2014 EN sets a numerical floor, ASTM says \u201cremainder\u201d<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Titanium<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>1.80\u20132.70<\/b> \u2014 <b>identical in both systems<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Aluminium<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>1.0\u20131.8<\/b> \u2014 <b>DOUBLE the ASTM floor of 0.50<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Iron<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>\u22641.50<\/b> \u2014 <b>HALF the ASTM ceiling of 3.00<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Cobalt<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u22641.0<\/b> \u2014 half the \u22642.0 % of commercial\/BS practice<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Copper \u00b7 boron<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">\u22640.2 \u00b7 \u22640.008<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">The Two Divergences That Really Matter on a Certificate<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Aluminium: 0.50 (ASTM) vs 1.0 (EN)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>This is the most important difference and it has a metallurgical consequence.<\/b> Aluminium is a \u03b3\u2032 former. <b>A heat at 0.6 % Al passes ASTM B637<\/b>, but its \u03b3\u2032 volume fraction is low and <b>its strength after ageing lands at the bottom of the table<\/b>. The same heat is <b>rejected<\/b> as EN 2.4952. <b>If you are buying valves or bolting, write the EN band (1.0\u20131.8) into the order<\/b> \u2014 the B637 floor does not guarantee the material you think you are buying<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Iron: \u22643.00 (ASTM) vs \u22641.50 (EN)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Second in importance.<\/b> Iron lowers cost and makes scrap easier to use; in exchange it <b>degrades the protectiveness of the oxide scale and high-temperature stability<\/b>. A heat at 2.5 % Fe passes ASTM and fails EN. <b>For exhaust-gas service ask for the EN band.<\/b> Note also that the nominal analysis quoted by mills \u2014 roughly <b>Ni 75 \u00b7 Cr 19.5 \u00b7 Ti 2.2\u20132.4 \u00b7 Al 1.4<\/b> \u2014 is <b>NOT a purchasing limit<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">\u03b3\u2032 \u2014 the metallurgical core of this page<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">All of 80A&#8217;s strength comes from <b>\u03b3\u2032, the ordered intermetallic Ni\u2083(Ti,Al)<\/b>. The phase precipitates <b>coherently<\/b> with the FCC \u03b3 matrix \u2014 its lattice planes continue those of the matrix. Dislocations can pass a coherent particle only by <b>cutting<\/b> it or by <b>looping around<\/b> it; both cost energy, and the alloy hardens.<br \/><b>The Ti + Al sum is the critical number.<\/b> Across the specification band it is <b>2.8 % to 4.5 %<\/b> (Ti 1.8\u20132.7 + Al 1.0\u20131.8). <b>That single sum fixes three things at once:<\/b> the \u03b3\u2032 volume fraction (strength), the \u03b3\u2032 solvus (service ceiling) and <b>susceptibility to strain-age cracking<\/b> (weldability). They cannot be separated \u2014 <b>nobody can sell you an 80A that is both stronger and easier to weld<\/b>.<br \/><b>The Ti\/Al ratio matters too.<\/b> A titanium-rich \u03b3\u2032 <b>coarsens faster<\/b> than an aluminium-rich one, so long-term high-temperature stability does not like Ti near the top of the band. <b>That is the second reason the ASTM aluminium floor of 0.50 is risky.<\/b><\/p>\n<h4 id=\"dm-b5\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Mechanical Properties \u2014 Do Not Confuse Minimum With Typical<\/h4>\n<p><!-- dm-diy-sert --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">STRENGTH VALUES<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:12px 10px 0;\"><svg viewBox=\"0 0 740 98\" style=\"width:100%;height:auto;display:block;\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\" role=\"img\"><rect x=\"16\" y=\"6\" width=\"12\" height=\"12\" fill=\"#12303f\"\/><text x=\"34\" y=\"16\" font-size=\"11.5\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Yield (MPa)<\/text><rect x=\"146\" y=\"6\" width=\"12\" height=\"12\" fill=\"#7fa8bd\"\/><text x=\"164\" y=\"16\" font-size=\"11.5\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Tensile (MPa)<\/text><text x=\"16\" y=\"44\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">ASTM B637 \/ ASME SB-637 \u2014 UNS N07080<\/text><rect x=\"16\" y=\"50\" width=\"652.0\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"675.0\" y=\"62\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">930<\/text><rect x=\"16\" y=\"68\" width=\"434.7\" height=\"15\" fill=\"#12303f\"\/><text x=\"457.7\" y=\"80\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">620<\/text><\/svg><\/div>\n<div style=\"padding:12px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"overflow-x:auto;position:relative;z-index:2;\">\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;min-width:430px;background:transparent;\">\n<tr>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Condition<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Hardness<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Yield MPa<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Tensile MPa<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Elongation<\/th>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">ASTM B637 \/ ASME SB-637 \u2014 UNS N07080<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">\u2014<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">620<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">930<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">20%<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\"><b style=\"color:#12303f;\">The row is a SPECIFICATION MINIMUM, not a manufacturer typical value. The figures are for room temperature and are what must be met after the complete cycle (solution + stabilize + precipitation harden). ASTM B637 covers rod, bar, forgings and forging stock only; the row does not apply to plate, sheet or tube.<\/b> The figures are room-temperature specification minimums; what a given part achieves depends on section size, specimen location and the actual heat treatment. The mechanical minimums of BS HR 201 (plate, sheet and strip) and EN 10269 (fasteners) could NOT be confirmed by four independent sources and are therefore not in the table; the single-source values that were found are listed under &#8216;atlananlar&#8217;. No hardness value for fully heat treated material could be confirmed by four sources; two sources disagree and that disagreement is recorded under &#8216;celiskiler&#8217;. The stress-rupture requirement that ASTM B637 sets for N07080 (760 \u00b0C, 325 MPa) rests on one specification text only and is therefore not in the table.<\/div>\n<\/div>\n<p><!-- \/dm-diy-sert --><\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Three separate sets of minima are published for 80A, and mixing them is the most common error in the trade.<\/b> Read the tables below separately.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Specification Minima \u2014 Three Separate Systems, Do NOT Mix Rows<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>ASTM B637 \/ ASME SB-637<\/b><br \/>rod, bar, forgings \u00b7 fully heat treated<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Tensile <b>Rm \u2265930 MPa (135 ksi)<\/b> \u00b7 Yield <b>Rp0.2 \u2265620 MPa (90 ksi)<\/b> \u00b7 Elongation in 50 mm <b>\u226520 %<\/b>. <b>B637 sets no minimum for reduction of area or hardness<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>ASTM B637 \u00b7 stress-rupture requirement<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>At 760 \u00b0C (1400 \u00b0F) under 325 MPa (47,000 psi): minimum 23 hours with minimum 3.5 % elongation.<\/b> <b>This, not the tensile figures, is B637&#8217;s real acceptance criterion.<\/b> A heat can pass the tensile test and fail the rupture test \u2014 look for this line on the certificate<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>EN 10269<\/b><br \/>fasteners \u00b7 +AT+P \u00b7 d \u2264160 mm<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Yield <b>Rp0.2 \u2265600 MPa<\/b> \u00b7 Tensile <b>Rm 1000\u20131300 MPa<\/b> \u00b7 Elongation <b>A \u226512 %<\/b> \u00b7 Reduction of area <b>Z \u226512 %<\/b> \u00b7 <b>ISO-V impact at 20 \u00b0C: \u226520 J<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>In EN, Rm is a BAND \u2014 in ASTM it is a floor<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>This is the distinction the trade most often misses.<\/b> ASTM sets only a floor (930 MPa) with no upper limit. <b>EN 10269 sets both a floor (1000) and a CEILING (1300 MPa).<\/b> An over-aged, very high strength heat <b>sails through ASTM and is rejected under EN 10269<\/b> for exceeding 1300 MPa. Note also that <b>ASTM is the stricter one on ductility<\/b>: 20 % elongation against EN&#8217;s 12 %. A heat that meets ASTM 20 % and EN 1000 MPa simultaneously sits in a narrow window<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Typical Mill Values \u2014 NOT GUARANTEED, and sources CONFLICT<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Fully heat-treated bar, room temperature<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Published typicals are <b>scattered<\/b>: one German producer gives <b>Rp0.2 800 MPa \/ Rm 1200 MPa \/ A 20 %<\/b>; another publisher <b>Rp0.2 780 MPa \/ Rm 1250 MPa \/ A 30 %<\/b>; a third <b>Rp0.2 670 MPa \/ Rm 1150 MPa \/ A 17 %<\/b>. <b>The 100 MPa spread is real<\/b> and comes from Al\/Ti level, grain size and ageing route. <b>Do not publish a single \u201ctypical\u201d figure; publish the band<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Solution-annealed (un-aged) condition<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>There is a serious CONTRADICTION here.<\/b> One producer datasheet labels its table \u201c<b>solution annealed<\/b>\u201d and gives <b>Rp0.2 600 \/ Rm 930 MPa \/ A 20 %<\/b> \u2014 <b>but those numbers are almost exactly ASTM B637&#8217;s FULLY HEAT TREATED minima<\/b>. Another producer publishes <b>Rp0.2 600 \/ Rm 900 \/ A 30 %<\/b> for the solution-annealed state. <b>An 80A with no \u03b3\u2032 precipitated is not metallurgically expected to yield at 600 MPa.<\/b> The likely explanation is a labelling error, or that \u201csolution annealed\u201d is being used to mean the delivery condition (annealed + aged). <b>If you are buying un-aged material, have the mechanical values tested on the heat; do not trust a published number<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Yield strength at temperature (typical)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rp0.2: <b>100 \u00b0C 586 \u00b7 200 \u00b0C 568 \u00b7 300 \u00b0C 560 \u00b7 400 \u00b0C 540 \u00b7 500 \u00b0C 520 \u00b7 600 \u00b0C 500 MPa<\/b>. <b>The thing to notice is how FLAT the curve is<\/b>: from room temperature to 600 \u00b0C the yield falls only about 17 %. That is the signature of a \u03b3\u2032 alloy and the direct reason 80A works in a valve. Hardness for the fully heat-treated condition is typically quoted as <b>\u2265300 HV<\/b> as a specification minimum and around <b>38 HRC<\/b> in machining references \u2014 <b>always state the scale<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Notch impact<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">EN 10269 minimum is <b>ISO-V \u226520 J at 20 \u00b0C<\/b>, with about <b>22 J<\/b> published as typical. <b>That is a low figure and it should not surprise anyone<\/b>: a \u03b3\u2032-hardened alloy is not a toughness alloy. <b>Do not use 80A in a structural part exposed to impact loading.<\/b> One published fatigue strength of <b>370 MPa<\/b> exists but is <b>single-source with no cycle count or R ratio stated \u2014 do not use it as a design input<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Creep and Rupture Strength (EN 10302 route) \u2014 MPa<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>500 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Creep limit Rp1.0: <b>10\u2074 h 624<\/b> \u00b7 <b>10\u2075 h 530<\/b> \u2014 Rupture Rm: <b>10\u2074 h 745<\/b> \u00b7 <b>10\u2075 h 587<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>550 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Rp1.0: <b>10\u2074 h 523<\/b> \u00b7 <b>10\u2075 h 390<\/b> \u2014 Rm: <b>10\u2074 h 582<\/b> \u00b7 <b>10\u2075 h 416<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>600 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rp1.0: <b>10\u2074 h 398<\/b> \u00b7 <b>10\u2075 h 257<\/b> \u2014 Rm: <b>10\u2074 h 433<\/b> \u00b7 <b>10\u2075 h 272<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>650 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Rp1.0: <b>10\u2074 h 275<\/b> \u00b7 <b>10\u2075 h 149<\/b> \u2014 Rm: <b>10\u2074 h 300<\/b> \u00b7 <b>10\u2075 h 157<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>700 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rp1.0: <b>10\u2074 h 183<\/b> \u00b7 <b>10\u2075 h 72<\/b> \u2014 Rm: <b>10\u2074 h 186<\/b> \u00b7 <b>10\u2075 h 75<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>750 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Rp1.0: <b>10\u2074 h 106<\/b> \u00b7 <b>10\u2075 h 33<\/b> \u2014 Rm: <b>10\u2074 h 114<\/b> \u00b7 <b>10\u2075 h 37<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>800 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rp1.0: <b>10\u2074 h 58<\/b> \u00b7 <b>10\u2075 h 16<\/b> \u2014 Rm: <b>10\u2074 h 70<\/b> \u00b7 <b>10\u2075 h 20<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b6\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Physical Properties<\/h4>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Physical Properties \u00b7 Nimonic 80A (N07080)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Density<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>8.19 g\/cm\u00b3<\/b> (0.296 lb\/in\u00b3) \u2014 the most widely published value. <b>Conflict:<\/b> one producer publishes <b>8.2<\/b>, another <b>8.17 g\/cm\u00b3<\/b>. <b>The difference is negligible; use 8.19<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Melting range<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>1320\u20131370 \u00b0C<\/b> (one producer) \u00b7 <b>1320\u20131365 \u00b0C<\/b> (majority). <b>A single \u201cmelting point 1365 \u00b0C\u201d is wrong<\/b> \u2014 the alloy has a solidus-liquidus range<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Modulus of elasticity \u2014 CONFLICTING<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Published values: 216 GPa \u00b7 222 GPa \u00b7 190\u2013200 GPa \u00b7 190 GPa.<\/b> <b>That is a 17 % spread and it cannot be ignored.<\/b> The most detailed source (the producer that publishes a full temperature table) gives <b>216 GPa at 20 \u00b0C<\/b> and <b>that is the value used here<\/b>; but for a spring or a bolt preload calculation, <b>have the modulus measured on the heat<\/b>. With temperature: <b>100 \u00b0C 212 \u00b7 200 \u00b0C 208 \u00b7 300 \u00b0C 202 \u00b7 400 \u00b0C 196 \u00b7 500 \u00b0C 189 \u00b7 600 \u00b0C 179 \u00b7 700 \u00b0C 161 \u00b7 800 \u00b0C 130 GPa<\/b>. <b>The 19 % drop in a single 100 \u00b0C step from 700 to 800 \u00b0C is the physical signature of \u03b3\u2032 coarsening and dissolution.<\/b> Shear modulus is quoted as <b>85 GPa<\/b> \u2014 <b>single source<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Thermal conductivity<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>20 \u00b0C: 11.2 W\/m\u00b7K<\/b>. With temperature: 100 \u00b0C 12.6 \u00b7 200 \u00b0C 14.4 \u00b7 300 \u00b0C 16.1 \u00b7 400 \u00b0C 17.8 \u00b7 500 \u00b0C 19.4 \u00b7 600 \u00b0C 20.8 \u00b7 700 \u00b0C 22.3 \u00b7 800 \u00b0C 24.5 \u00b7 900 \u00b0C 26.5 \u00b7 <b>1000 \u00b0C 28.4 W\/m\u00b7K<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Mean coefficient of thermal expansion<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>20\u2013100 \u00b0C: 12.7 \u00d7 10\u207b\u2076\/K<\/b>. Then: 20\u2013200 \u00b0C 13.3 \u00b7 20\u2013300 \u00b0C 13.7 \u00b7 20\u2013400 \u00b0C 14.1 \u00b7 20\u2013500 \u00b0C 14.4 \u00b7 20\u2013600 \u00b0C 15.0 \u00b7 20\u2013700 \u00b0C 15.5 \u00b7 20\u2013800 \u00b0C 16.2 \u00b7 20\u2013900 \u00b0C 17.1 \u00b7 <b>20\u20131000 \u00b0C 18.1 \u00d7 10\u207b\u2076\/K<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Electrical resistivity<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>20 \u00b0C: 1.24 \u00b5\u03a9\u00b7m<\/b> (= <b>124 \u00b5\u03a9\u00b7cm<\/b> = 1.24 \u03a9\u00b7mm\u00b2\/m). <b>Common error:<\/b> at least one publisher prints <b>12.4 \u00b5\u03a9\u00b7m<\/b> \u2014 <b>a factor of ten<\/b>. The correct figure is 1.24 \u00b5\u03a9\u00b7m<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>The commercially meaningful point<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>11.2 W\/m\u00b7K<\/b> at room temperature is roughly a quarter of carbon steel and about 70 % of <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-316l\/\">316L<\/a>. <b>In an exhaust valve that is a DISADVANTAGE:<\/b> heat in the valve head flows slowly down the stem to the guide, so the head runs hotter. <b>That is precisely why heavily loaded valves use sodium-filled stems<\/b> \u2014 to compensate for the alloy&#8217;s low conductivity. Knowing this when you quote an 80A valve is what gets you taken seriously technically<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b7\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Heat Treatment and Thermal Stability \u2014 THERE ARE TWO SEPARATE ROUTES<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>There is no single \u201cstandard heat treatment\u201d for 80A, and this is the most critical information on the page.<\/b> The alloy is processed by two different routes for two different jobs: the <b>creep route<\/b> (turbines, bolting, long-term static load) and the <b>valve route<\/b> (endurance-strength driven). <b>Same chemistry, different part.<\/b><\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Route 1 \u2014 the CREEP route (ASTM B637 \u00b7 turbine, bolting, static load)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Step 1 \u2014 Solution anneal<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>1066 \u00b1 14 \u00b0C (1950 \u00b1 25 \u00b0F), 8 hours, air cool.<\/b> The European route gives the same thing as a band: <b>1050\u20131080 \u00b0C, 8 hours, air cool<\/b>. <b>The two do not conflict<\/b> \u2014 1066 \u00b0C sits in the middle of 1050\u20131080. Purpose: dissolve \u03b3\u2032 and the soluble carbides, remove dislocations, set the grain size. <b>Note:<\/b> at least one publisher writes \u201c1040 \u00b0C followed by water quench\u201d, which <b>contradicts majority practice<\/b>; 80A&#8217;s \u03b3\u2032 kinetics are slow enough for air cooling, and quenching risks distortion in thin sections<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Step 2 \u2014 Stabilising anneal<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>849 \u00b1 14 \u00b0C (1560 \u00b1 25 \u00b0F), 24 hours, air cool.<\/b> European route: <b>840\u2013860 \u00b0C, 24 hours, air cool<\/b>. <b>This step cannot be skipped and its purpose is widely misunderstood.<\/b> Those 24 hours are not there to precipitate \u03b3\u2032; they are there to <b>precipitate M\u2082\u2083C\u2086 carbides at the grain boundaries in a controlled way<\/b>. Those carbides block grain-boundary sliding and deliver <b>creep-rupture ductility<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Step 3 \u2014 Ageing (precipitation hardening)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>699 \u00b1 14 \u00b0C (1290 \u00b1 25 \u00b0F), 16 hours, air cool.<\/b> European route: <b>690\u2013710 \u00b0C, 16 hours, air cool<\/b>. Trade shorthand: <b>\u201c700 \u00b0C \/ 16 h\u201d<\/b>. The bulk of the \u03b3\u2032 precipitates here and so does the bulk of the strength<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Why three steps<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>An 80A aged in a single step gives the same tensile strength but not the creep-rupture ductility.<\/b> The grain-boundary microstructure (carbides) and the intragranular microstructure (\u03b3\u2032) have to be built separately. <b>A heat treater who short-cuts gives you material that passes the tensile test and fails the rupture test<\/b> \u2014 and B637&#8217;s acceptance criterion is the rupture test<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Route 2 \u2014 the VALVE route (endurance and fatigue driven)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>The whole difference is in Step 1<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Solution anneal at 1010\u20131050 \u00b0C<\/b> \u2014 roughly <b>40 \u00b0C lower<\/b> than the standard route&#8217;s 1050\u20131080 \u00b0C. In the producer&#8217;s own words: \u201cfor applications where the <b>endurance strength<\/b> is in focus instead of the creep resistance (e.g. valves), the solution annealing should occur in the temperature range from 1010 \u00b0C to 1050 \u00b0C\u201d<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Why lower<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Grain size.<\/b> A lower solution temperature leaves <b>finer grain<\/b>. Fine grain <b>raises fatigue strength and room-temperature yield<\/b>; coarse grain raises <b>creep resistance<\/b>. <b>The two cannot be optimised at the same time<\/b> \u2014 one of the most basic trade-offs in metallurgy, and in 80A it is written straight into the heat treatment instruction<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>The commercial consequence<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Bar processed for turbine bolting is NOT the right material for a valve<\/b>, and the reverse is equally true. The chemistry on the certificate looks the same and the mechanical values may look similar, <b>but the fatigue life is different<\/b>. <b>Write \u201cvalve route\u201d or \u201ccreep route\u201d into the order.<\/b> A supplier who asks you this question is a supplier who knows the alloy. <b>Note:<\/b> a separate route is published for cold-rolled sheet \u2014 <b>1150 \u00b0C for 2\u20133 minutes, fluidised-bed quench, then ageing at 750 \u00b0C<\/b> \u2014 <b>single source<\/b>, and completely different from the bar route (minutes, not hours). <b>Confirm it separately if you are buying sheet<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Hot and Cold Working<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Hot forming range<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>1200 \u2192 1050 \u00b0C<\/b> (the producer&#8217;s optimum band); another publisher gives the wider <b>1050\u20131200 \u00b0C<\/b>, and <b>982\u20131176 \u00b0C<\/b> is published for forging (single source). <b>A 150 \u00b0C window is narrow:<\/b> below 1050 \u00b0C the alloy work-hardens rapidly and cracks, above 1200 \u00b0C there is grain coarsening and burning risk. <b>Budget frequent reheats<\/b> \u2014 noticeably more than for a stainless forging job, and <b>re-apply the full heat treatment cycle after all hot forming<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Thermal stability \u2014 where 80A degrades<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>80A is not expected to show an embrittling ordering reaction or a \u201cwindow to avoid\u201d of the kind seen in solid-solution alloys.<\/b> There is one degradation mechanism and it is simple: <b>\u03b3\u2032 COARSENS and eventually DISSOLVES.<\/b> By Ostwald ripening the large \u03b3\u2032 particles consume the small ones, the spacing between them opens up, and dislocations begin to loop rather than cut \u2014 <b>the alloy softens<\/b>. The process becomes measurable above about <b>700 \u00b0C<\/b> and reaches a commercially unacceptable rate around <b>815 \u00b0C<\/b>. <b>The physical measurement is the modulus:<\/b> 161 GPa at 700 \u00b0C, <b>130 GPa at 800 \u00b0C<\/b> \u2014 19 % lost in a single 100 \u00b0C step. <b>The rule is single: do not exceed 815 \u00b0C under load, and design long-term service from the creep table.<\/b> Numerical data on 80A&#8217;s loss of ductility and toughness after tens of thousands of hours of exposure <b>could not be independently verified<\/b> \u2014 for a critical application ask the producer for post-exposure data.<\/p>\n<h4 id=\"dm-b8\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Welding \u2014 Strain-Age Cracking Is the Most Important Warning on This Page<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>80A is a \u03b3\u2032-hardened alloy, and for welding that means one thing: the risk of STRAIN-AGE CRACKING (reheat cracking).<\/b> A fabricator who does not understand this risk produces parts that crack after welding \u2014 and the cracks usually appear not during welding but <b>on the heating ramp of the post-weld heat treatment<\/b>.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Welding \u00b7 Nimonic 80A (N07080)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>The mechanism \u2014 understand this first<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">After welding the part carries <b>residual stress<\/b>. When it is heated through the \u03b3\u2032 precipitation band (roughly 600\u2013800 \u00b0C), <b>\u03b3\u2032 precipitates rapidly and hardens the matrix<\/b>. The hardened matrix can no longer accommodate the residual stress by <b>plastic deformation<\/b>; the stress concentrates at the <b>grain boundaries<\/b> and an <b>intergranular crack<\/b> opens in the HAZ. <b>The moment the crack opens is the moment the furnace is ramping towards 700 \u00b0C<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>The number that governs susceptibility: Al + Ti<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">The classic rule in the literature is that <b>\u03b3\u2032 alloys with Al + Ti above roughly 3\u20134 % are susceptible to strain-age cracking<\/b>. 80A&#8217;s specification band is <b>Al + Ti = 2.8\u20134.5 %<\/b> \u2014 <b>the alloy sits squarely inside that band and heats near the top of it are plainly susceptible<\/b>. For comparison: <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-718\/\">718<\/a> hardens with niobium (\u03b3\u2033) and precipitates very slowly \u2014 <b>which is why 718 counts as weldable and 80A does not<\/b>. <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/waspaloy\/\">Waspaloy<\/a> is more susceptible still<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>THE GOLDEN RULE<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Weld 80A ONLY in the solution-annealed condition. Do not weld aged material.<\/b> Aged material already has a hardened matrix and lacks the ductility to absorb weld stress. <b>If a repair weld is to be made on a valve or a bolt, a full solution anneal must come first<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Post-weld heat treatment \u2014 MANDATORY<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Published repair procedure: <b>solution anneal 1065\u20131095 \u00b0C, 8 hours, air cool \u2192 age 685\u2013715 \u00b0C, 16 hours, air cool<\/b>. <b>That is a repeat of the entire standard cycle<\/b>, not a \u201cstress relief\u201d. <b>THERE IS NO SUCH THING as a simple stress-relief anneal on 80A<\/b> \u2014 those temperatures are already the ageing temperatures<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Sequence of operations<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Machine BEFORE ageing, after the solution anneal.<\/b> Two reasons: solution-annealed material machines far more easily, and small dimensional changes during ageing do not spoil the final size. <b>Sequence: solution anneal \u2192 weld \u2192 solution anneal \u2192 machine \u2192 age.<\/b> <b>Attach the thermocouple to the PART, not to the furnace<\/b> \u2014 inside a 699 \u00b1 14 \u00b0C window, trusting furnace air temperature means missing the ageing treatment in a heavy section<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Filler metal \u2014 two routes<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>(a) Matching filler:<\/b> wire drawn from the same alloy; the weld metal ages too and the joint loses no strength. <b>No AWS classification could be verified<\/b>; it is bought to company specification. <b>(b) Non-matching filler:<\/b> <b>ENiCrFe-3<\/b> and <b>ERNiCr-3 \/ ENiCr19Nb<\/b> type Ni-Cr-Nb consumables are reported in repair practice. <b>These cannot be aged<\/b> \u2014 the weld metal stays soft. <b>Choose this knowingly in a load-carrying joint and tell the customer in writing<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">What actually goes wrong<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>1. Welding aged material.<\/b> The most frequent and most expensive mistake. The part may not crack during welding; the crack appears <b>during post-weld heat treatment or on the first thermal cycle<\/b>. <b>A pre-weld solution anneal is not negotiable.<\/b><br \/><b>2. Applying a \u201cstress-relief anneal\u201d.<\/b> On 80A a \u201cstress relief\u201d at 600\u2013750 \u00b0C <b>is exactly the ageing cycle<\/b> \u2014 it does not relieve stress, it hardens the matrix and triggers the crack. <b>Either a full solution anneal is performed, or nothing is.<\/b><br \/><b>3. A load-carrying joint made with the wrong filler.<\/b> A joint made with ENiCrFe-3 leaves <b>weld metal markedly weaker than the parent<\/b> after ageing. Acceptable for a repair; <b>not for a design joint<\/b>.<br \/><b>4. Trusting the sentence \u201c80A is a weldable alloy\u201d.<\/b> Some distributor pages print it with no conditions attached. <b>The truth is: 80A can be welded in the right condition and with the right heat treatment cycle; if those conditions are not met, it cracks.<\/b><\/p>\n<h4 id=\"dm-b9\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Machining<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>A caveat that must be stated plainly:<\/b> the parameters below are <b>starting values compiled from secondary sources<\/b>, not the producer&#8217;s own 80A-specific table. <b>Verify them with your own trials.<\/b> The producer&#8217;s qualitative rule is clear: <b>select a lower cutting speed and keep the tool engaged in the cut at all times<\/b>.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Starting Parameters (secondary source \u00b7 aged condition, about 38 HRC)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Turning<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>40\u201355 m\/min (130\u2013180 sfm)<\/b> \u00b7 very hard substrate, <b>PVD-coated<\/b> carbide \u00b7 ground inserts \u00b7 <b>positive rake 13\u00b0\u201318\u00b0<\/b> \u00b7 hone 0.02\u20130.05 mm \u00b7 land width 0.10\u20130.20 mm<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Milling \u00b7 drilling<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>30\u201340 m\/min (100\u2013130 sfm)<\/b> \u00b7 semi-hard substrate, PVD-coated carbide. <b>CBN<\/b> inserts can raise cutting speed <b>2\u20134 times<\/b> over carbide at higher tool cost<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Governing rules<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>A positive, sharp cutting edge is mandatory.<\/b> The alloy work-hardens fast: <b>rigid clamping, constant feed, never dwell, never rub<\/b> \u2014 a stalled feed burnishes the surface and the next pass has to cut through a work-hardened skin. <b>Flood, high-pressure coolant.<\/b> On condition: solution-annealed material machines more easily and loads the tool less, while the aged condition gives the better surface finish \u2014 <b>the producer publishes both facts and leaves the choice to you<\/b>. In practice, roughing annealed and finishing aged works best in most shops. <b>Sulpho-chlorinated tapping compound must be removed completely before any heat treatment or welding<\/b> \u2014 residual sulphur causes hot cracking<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b10\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Corrosion \u2014 Where It Is Good, and WHERE IT FAILS<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>80A is a high-temperature oxidation alloy. It is NOT an aqueous corrosion alloy.<\/b> This distinction is the most frequently violated part of the page, because the alloy&#8217;s <b>18\u201321 % chromium<\/b> makes it look like something better than a stainless steel. <b>It is not: there is no molybdenum, no nitrogen, no copper.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Where it is good \u2014 high-temperature oxidation<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">80A forms a tightly adherent, protective scale based on <b>Cr\u2082O\u2083 (chromium oxide)<\/b>. <b>The published scaling-resistance limit is 1000 \u00b0C.<\/b> Wear studies report a layered oxide developing in the sequence <b>Cr\u2082O\u2083 \/ TiO\u2082 \/ Al\u2082O\u2083 \/ substrate<\/b> at the interface \u2014 so titanium and aluminium do more than form \u03b3\u2032, they also work beneath the scale. Against iron-base heat-resisting steels of the same chromium this is a clear advantage: the nickel matrix gives <b>fast re-passivation<\/b> when the scale cracks and reduces spalling under thermal cycling.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Where it is good \u2014 the exhaust-gas environment (the real application)<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>This is 80A&#8217;s commercial reason to exist.<\/b> Producer data states that the alloy has <b>proven its resistance to vanadium pentoxide (V\u2082O\u2085), sodium compounds and sulphur compounds as an exhaust valve in heavy-oil-fired engines<\/b>. That trio is the classic valve-killer of heavy-fuel marine and stationary diesels:<br \/><b>Vanadium pentoxide<\/b> is a low-melting oxide (melting around 675 \u00b0C) which in the molten state <b>dissolves and fluxes away<\/b> the protective Cr\u2082O\u2083 scale \u2014 the classic catastrophic oxidation mechanism.<br \/><b>Sodium sulphate (Na\u2082SO\u2084)<\/b>, formed from sodium in marine air and sulphur in the fuel, drives <b>hot corrosion<\/b>.<br \/><b>80A survives this environment because of its high chromium<\/b> \u2014 the stronger but lower-chromium members of the \u03b3\u2032 family, for example <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-x750\/\">X-750<\/a> at 14\u201317 % Cr, do not substitute for it here. <b>This is the strongest technical argument you have when selling 80A.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">WHERE IT FAILS \u2014 1: aqueous corrosion<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>80A contains NO molybdenum.<\/b> That single fact explains every one of its aqueous weaknesses. Molybdenum is the element that prevents local breakdown of the passive film (pitting and crevice corrosion) in chloride-bearing media. Calculated roughly, with Mo = 0 and N \u2248 0 the alloy&#8217;s pitting resistance equivalent is <b>only its chromium: about 18\u201321<\/b> \u2014 below <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-316l\/\">316L<\/a> (about 24) and not comparable with <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-f53\/\">2507 super duplex<\/a> or <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/hastelloy-c-276\/\">C-276<\/a>.<br \/><b>Practical consequences:<\/b> <b>do not use it<\/b> in seawater. <b>Do not use it<\/b> in chloride process solutions. <b>Do not use it<\/b> in reducing acids (HCl, H\u2082SO\u2084) \u2014 that is where <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/hastelloy-b-3\/\">B-3<\/a> and <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/hastelloy-c-276\/\">C-276<\/a> live. <b>No published aqueous corrosion rate tables for 80A could be found, and that is not a gap but a message: producers do not sell this alloy for that duty.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">WHERE IT FAILS \u2014 2: reducing, sulphidising atmospheres<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>This is the classic weakness of high-nickel alloys, and 80A is about 75 % nickel.<\/b> In a reducing atmosphere low in oxygen and rich in sulphur \u2014 incomplete combustion products, sulphurous process gases, petrochemical regeneration environments \u2014 the protective Cr\u2082O\u2083 scale cannot remain stable and <b>nickel sulphide forms<\/b>. <b>The Ni\u2013Ni\u2083S\u2082 eutectic is widely reported in the general literature to melt at about 645 \u00b0C<\/b> \u2014 that is a <b>liquid phase<\/b> far below valve temperature. The liquid sulphide penetrates along grain boundaries and <b>destroys the alloy from the inside<\/b>; the damage is fast and irreversible.<br \/><b>Caution \u2014 do not conflate two separate claims.<\/b> Producer data says 80A resists the <b>sulphur compounds in exhaust gas<\/b>; that environment is <b>oxidising<\/b> (large excess air) and the Cr\u2082O\u2083 scale is stable. It does <b>not<\/b> follow that the same alloy will survive in a <b>reducing sulphidising<\/b> process atmosphere. <b>A quotation that misses this distinction ends in a field failure.<\/b> For such an environment look at higher-chromium, lower-nickel choices such as <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/incoloy-800h\/\">800H<\/a> or <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-601\/\">601<\/a> \u2014 and still have the sulphur partial pressure evaluated.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">WHERE IT FAILS \u2014 3: mechanical collapse above 815 \u00b0C<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>This is not a corrosion failure, but in the field it looks like one.<\/b> Above 815 \u00b0C the \u03b3\u2032 coarsens and dissolves; the part <b>begins to creep<\/b>, the valve head distorts, the seat face loses contact and <b>hot gas leakage starts<\/b>. The escaping gas burns the seat (guttering) and the failure report calls it \u201ccorrosion\u201d. <b>The real cause is excess temperature.<\/b> Look at the creep table: <b>the 10\u2075 h rupture strength at 800 \u00b0C is 20 MPa<\/b> \u2014 engineering-wise, close to zero.<\/p>\n<h4 id=\"dm-b11\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Frequently Asked Questions<\/h4>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Our exhaust valve is 21-4N (1.4882). Is it worth paying to move to Nimonic 80A?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The answer depends entirely on the real valve-head temperature and the loading regime, and deciding without measuring those two numbers is burning money.<\/b><br \/><b>Both sit in the same standard.<\/b> EN 10090 covers <b>1.4882 \/ X50CrMnNiNbN21-9<\/b> and <b>2.4952 \/ NiCr20TiAl<\/b> alike, and both are delivered in the <b>+AT+P<\/b> condition. There is no standards difference; they are <b>two rungs of the same ladder<\/b>.<br \/><b>What 21-4N does:<\/b> an austenitic matrix stabilised with manganese and nitrogen, plus niobium carbides and nitrides. It is sufficient for an ordinary petrol engine&#8217;s exhaust valve and costs <b>an order of magnitude less per kilogram<\/b>. Its weakness is that as temperature rises it <b>loses hot hardness and fatigue strength quickly<\/b>; its matrix is supported by solid solution and dispersed carbides, not by a coherent precipitate.<br \/><b>What 80A does:<\/b> \u03b3\u2032 \u2014 Ni\u2083(Ti,Al) \u2014 keeps the yield strength <b>remarkably flat<\/b> against temperature: a room-temperature yield of about 600 MPa is <b>still about 500 MPa at 600 \u00b0C<\/b>. Add <b>18\u201321 % chromium<\/b> and you also get resistance to vanadium, sodium and sulphur compounds, which the producer publishes as proven in heavy-fuel engines.<br \/><b>So the decision rule:<\/b> if your valve-head temperature is inside the comfortable range of the austenitic steel and your failures are wear or seating related, <b>moving to 80A will not fix your problem, only make it expensive<\/b>. But if your failures look like <b>head distortion, seat face loss, gas leakage (guttering) or stem fracture<\/b> \u2014 that is, <b>hot-strength and fatigue failures<\/b> \u2014 80A makes a real, measurable difference. <b>Turbocharged high-output engines and heavy-fuel diesels historically moved to 80A for exactly this reason.<\/b><br \/><b>One final warning:<\/b> if you do move, specify the <b>valve-route heat treatment<\/b> (solution anneal 1010\u20131050 \u00b0C), not the creep route. 80A delivered on the wrong route will not give you the fatigue life you paid for.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">The datasheet says \u201cmaximum operating temperature 1000 \u00b0C\u201d. Can we use it at 900 \u00b0C?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>No. And this is the most common and most expensive misreading of 80A.<\/b><br \/><b>1000 \u00b0C is an OXIDATION number, not a STRENGTH number.<\/b> The producer&#8217;s wording is \u201c<b>resistance to scaling up to 1000 \u00b0C<\/b>\u201d \u2014 meaning the surface is not rapidly consumed at that temperature. The same producer publishes the <b>maximum service temperature under load as 815 \u00b0C (1500 \u00b0F)<\/b>.<br \/><b>Look at the numbers.<\/b> The EN 10302 route creep data gives a <b>10\u2075 h rupture strength of 75 MPa at 700 \u00b0C<\/b>, <b>37 MPa at 750 \u00b0C<\/b> and <b>20 MPa at 800 \u00b0C<\/b>. The curve is not published beyond 800 \u00b0C \u2014 <b>because there is no meaningful strength left to publish<\/b>. At 900 \u00b0C \u03b3\u2032 is largely dissolved and the alloy behaves like a \u03b3\u2032-free nichrome, i.e. at the level of <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-600\/\">alloy 600<\/a> or Nimonic 75. <b>Everything you paid extra for buys you nothing there.<\/b><br \/><b>Physical confirmation:<\/b> modulus of elasticity 161 GPa at 700 \u00b0C and <b>130 GPa at 800 \u00b0C<\/b> \u2014 19 % lost in a single 100 \u00b0C step. That is a direct measurement of the collapse of \u03b3\u2032.<br \/><b>What to do at 900 \u00b0C:<\/b> if the load is low and the requirement is really oxidation resistance, solid-solution alloys such as <b>Nimonic 75<\/b> or <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/inconel-601\/\">alloy 601<\/a> are already sufficient and <b>far cheaper<\/b>. If the load is high you need <b>Nimonic 90<\/b> (cobalt-bearing, rupture strength published to about 920 \u00b0C) or a cobalt-base alloy. <b>What you must not do is convert an oxidation number into a design temperature.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">The certificate says W.Nr. 2.4631 but we ordered 2.4952. Do we reject it?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Not automatically \u2014 but this is a case where you must check the chemistry table line by line.<\/b><br \/><b>First the fact:<\/b> <b>2.4952 and 2.4631 name the same alloy<\/b>, and the overwhelming majority of producers publish them <b>together, without distinction<\/b> \u2014 a German producer, a French mill and several distributors print the two numbers side by side. <b>They are not two different alloys.<\/b><br \/><b>Then the caveat:<\/b> <b>no authoritative statement distinguishing the two numbers could be found.<\/b> The only observable pattern is this: <b>2.4952<\/b> is quoted together with the <b>EN 10090 \/ EN 10269 \/ EN 10302 \/ DIN 17742<\/b> table (<b>Al 1.0\u20131.8 % \u00b7 Fe \u22641.5 % \u00b7 Co \u22641.0 % \u00b7 C \u22650.04 %<\/b>), while <b>2.4631<\/b> is commonly quoted together with the <b>N07080 \/ NA20 \/ ASTM B637<\/b> band (<b>Al 0.50\u20131.80 % \u00b7 Fe \u22643.0 %<\/b>). <b>That is an observation, not a proven rule<\/b>, and it is presented as such on this page.<br \/><b>What to do is simple:<\/b> look not at the number but at the <b>actual values on the analysis certificate<\/b>. Is aluminium below 1.0 %? Is iron above 1.5 %? Is carbon below 0.04 %? <b>The answers to those three questions tell you whether you meet the EN specification you ordered far more reliably than the number at the top of the page.<\/b> If all three are inside the EN band, the number is a labelling matter and you can ask the supplier to correct it. <b>If any one of them falls outside, the material is not compliant no matter what number is printed.<\/b><br \/><b>Write this into the order:<\/b> \u201cNiCr20TiAl, W.Nr. 2.4952, <b>to the EN 10269 chemistry table<\/b>\u201d \u2014 so that which band governs is never a matter for debate.<\/p>\n<h4 id=\"dm-b12\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Common Datasheet Errors and Traps \u2014 Check Before You Order<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>1. Yield and tensile strength swapped.<\/b> A widely mirrored 80A page prints <b>\u201cyield 1000 MPa, tensile 621 MPa\u201d<\/b>. <b>Yield cannot exceed tensile.<\/b> The truth is the reverse: 621 MPa corresponds to the yield (about 90 ksi, the ASTM B637 minimum) and 1000 MPa to the tensile. <b>Reject on sight any table where yield exceeds tensile.<\/b><br \/><b>2. A factor-of-ten error in electrical resistivity.<\/b> At least one publisher prints <b>12.4 \u00b5\u03a9\u00b7m<\/b>. The correct figure is <b>1.24 \u00b5\u03a9\u00b7m = 124 \u00b5\u03a9\u00b7cm = 1.24 \u03a9\u00b7mm\u00b2\/m<\/b>. In a heating-element or current-carrying calculation that error is off by ten times.<br \/><b>3. \u201cTensile 145 ksi \/ 1000 MPa minimum per ASTM B637.\u201d<\/b> <b>WRONG.<\/b> <b>The B637 minimum is 135 ksi \/ 930 MPa.<\/b> The 1000 MPa figure comes from the <b>floor of the EN 10269 band<\/b> or from the <b>BS HR 1 \/ MSRR route<\/b>. No standard contains a table combining the two systems in one row.<br \/><b>4. \u201cSolution annealed: Rp0.2 600 MPa.\u201d<\/b> One producer labels its table that way, but those values are <b>almost identical to ASTM B637&#8217;s FULLY HEAT TREATED minima<\/b>. An 80A with no \u03b3\u2032 precipitated is not expected to yield at 600 MPa. <b>If you are buying un-aged material, have it tested on the heat.<\/b><br \/><b>5. Three different cobalt limits.<\/b> <b>Cobalt is NOT LISTED in the ASTM B637 N07080 row<\/b>; the EN route says <b>\u22641.0 %<\/b> and BS\/commercial practice <b>\u22642.0 %<\/b>. In nuclear work that difference is directly an activation question. <b>Put it in the order.<\/b><br \/><b>6. Nimonic 90&#8217;s chemistry printed as 80A.<\/b> <b>Any 80A table showing Co 15\u201321 % is WRONG<\/b> \u2014 that is Nimonic 90 (N07090 \/ 2.4632). In 80A cobalt is an impurity ceiling, not an alloying element. Similarly, research literature sometimes describes 80A as \u201cnichrome plus Ti\/Al\u201d using a nominal containing <b>Fe 5.0 %<\/b>; <b>that exceeds even the ASTM ceiling of 3.0 %<\/b> and is three times the EN ceiling of 1.5 %. <b>Do not use it as a purchasing limit.<\/b><br \/><b>7. BS HR numbers confused with product form.<\/b> The correct mapping is: <b>BS HR 1 = rod\/bar<\/b>, <b>BS HR 201 = plate\/sheet\/strip<\/b>, <b>BS HR 401 = pipe\/tube<\/b>, <b>BS HR 601 = forgings<\/b>. If a distributor page says \u201cBS HR 601\u201d and sells plate, either the number or the product is wrong.<br \/><b>8. \u201cMaximum operating temperature 1000 \u00b0C.\u201d<\/b> That figure is the <b>scaling resistance<\/b> limit. <b>The maximum service temperature under load is 815 \u00b0C.<\/b> A third number, <b>about 550 \u00b0C<\/b>, is the <b>relaxation<\/b> limit some wire and spring makers publish. <b>Three different numbers, three different meanings \u2014 label each one.<\/b><br \/><b>9. Writing a single \u201cheat treatment\u201d.<\/b> 80A has <b>two routes<\/b>: the creep route (solution anneal <b>1050\u20131080 \u00b0C<\/b>) and the <b>valve route<\/b> (solution anneal <b>1010\u20131050 \u00b0C<\/b>). Any recipe that <b>omits the 849 \u00b0C \/ 24 h stabilising step<\/b> is incomplete. <b>A separate sheet route (1150 \u00b0C \/ 2\u20133 minutes) is published and must not be confused with the bar route.<\/b> Note too that majority practice and the ASTM route call for <b>air cooling<\/b>, while a single source writes \u201cwater quench\u201d.<br \/><b>10. Saying \u201c80A welds easily\u201d.<\/b> With Al + Ti = <b>2.8\u20134.5 %<\/b> the alloy sits in the <b>strain-age cracking risk band<\/b>. Welding is done only in the solution-annealed condition and <b>the full post-weld heat treatment cycle is mandatory<\/b>. <b>A simple stress-relief anneal is not an option.<\/b><br \/><b>11. Implying NACE MR0175 compliance.<\/b> <b>Listing of N07080 in ISO 15156-3 Annex A could not be verified<\/b> and the alloy contains no molybdenum. <b>Never make that declaration.<\/b><br \/><b>12. Treating 2.4952 and 2.4631 as two different alloys.<\/b> They are the same alloy. <b>But the chemistry bands published alongside the two numbers are not identical<\/b> \u2014 look at the Al, Fe and C values on the certificate, not at the number.<\/p>\n<p><!-- \/dm-zengin --><\/p>\n<p><!-- dm-ld --><script type=\"application\/ld+json\">{\"@context\":\"https:\/\/schema.org\",\"@type\":\"WebPage\",\"name\":\"Nimonic 80A\",\"url\":\"https:\/\/www.defencemetal.com\/index.php\/en\/nimonic-80a\/\",\"inLanguage\":\"en\",\"description\":\"Nimonic 80A (UNS N07080 \/ W.Nr. 2.4952 and 2.4631 \/ EN chemical name NiCr20TiAl \/ AFNOR NC 20 TA \/ BS NA20) is a precipitation-hardenable (age-hardenable) nickel-chromium alloy made by adding 1.8\u20132.7 % titanium and 1.0\u20131.8 % aluminium to a nominal 20 % chromium, balance nickel matrix.\",\"isPartOf\":{\"@type\":\"WebSite\",\"name\":\"Defence Metal\",\"url\":\"https:\/\/www.defencemetal.com\/\"},\"publisher\":{\"@type\":\"Organization\",\"name\":\"Defence Metal\",\"url\":\"https:\/\/www.defencemetal.com\/\"},\"mainEntity\":{\"@type\":\"DefinedTerm\",\"name\":\"Nimonic 80A\",\"description\":\"Nimonic 80A (UNS N07080 \/ W.Nr. 2.4952 and 2.4631 \/ EN chemical name NiCr20TiAl \/ AFNOR NC 20 TA \/ BS NA20) is a precipitation-hardenable (age-hardenable) nickel-chromium alloy made by adding 1.8\u20132.7 % titanium and 1.0\u20131.8 % aluminium to a nominal 20 % chromium, balance nickel matrix.\",\"inDefinedTermSet\":{\"@type\":\"DefinedTermSet\",\"name\":\"Defence Metal - metals and alloys\",\"url\":\"https:\/\/www.defencemetal.com\/\"},\"alternateName\":[\"UNS N07080\",\"W.Nr. 2.4952\"],\"identifier\":[{\"@type\":\"PropertyValue\",\"propertyID\":\"UNS\",\"value\":\"N07080\"},{\"@type\":\"PropertyValue\",\"propertyID\":\"Werkstoffnummer\",\"value\":\"2.4952\"}]}}<\/script><!-- \/dm-ld --><\/p>\n","protected":false},"excerpt":{"rendered":"<p>Nimonic 80A \/ UNS N07080 \/ ASTM B637 DEFENCE METAL Nimonic 80A UNS N07080 \u00b7 W.Nr. 2.4952 and 2.4631 \u00b7 NiCr20TiAl \u00b7 18.0-21.0% Cr \u2013 1.8-2.7% Ti \u2013 1.0-1.8% Al \u2013 balance Ni. Strengthening comes from the \u03b3\u2032 (Ni\u2083(Al,Ti)) precipitate formed by titanium and aluminium; the alloy contains no niobium. Not to be confused with &hellip; <\/p>\n<p class=\"link-more\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/nimonic-80a\/\" class=\"more-link\"><span class=\"screen-reader-text\"> &#8220;Nimonic 80A \/ ASTM B637&#8221;<\/span>devam\u0131n\u0131 oku<\/a><\/p>\n","protected":false},"author":1,"featured_media":0,"parent":3526,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_yoast_wpseo_title":"NIMONIC 80A \/ UNS N07080 \/ AMS 4378 \/ AMS 5829 | Defence Metal","_yoast_wpseo_metadesc":"Nimonic 80A (UNS N07080) \u2014 AMS 4378 \/ AMS 5829. Age-hardened nickel superalloy holding its strength at 650-850 \u00b0C. NACE MR0175 approved.","inspiro_hide_title":false,"inspiro_hide_featured_image":false,"footnotes":""},"dm_sektor":[10,12,13,18,15],"class_list":["post-3545","page","type-page","status-publish","hentry"],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v28.5 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>NIMONIC 80A \/ UNS N07080 \/ AMS 4378 \/ AMS 5829 | Defence Metal<\/title>\n<meta name=\"description\" content=\"Nimonic 80A (UNS N07080) \u2014 AMS 4378 \/ AMS 5829. Age-hardened nickel superalloy holding its strength at 650-850 \u00b0C. 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