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SPECIFICATION Alloy 80A is available in Bar, Extruded Section, Tube, Plate, Sheet and Wire. Similar Specification UNS N07080, NA 20, BS 3076, HR1, HR201, HR401, HR601 ASTM B637, Werkstoff Nr. 2.4631 and 2.4952, AFNOR NC 20TA, NIMONIC Alloy 80A, MSRR 7095 and MSRR 7011, AECMA Pr EN 2188, 2189, 2190, 2191, 2396 and 2397, VAT80A,
RESISTANCE TO OXIDATION and CORROSION Alloy 80A is a nickel-chromium alloy similar to alloy 75 but made precipitation hardenable by additions of aluminium and titanium. The alloy has good corrosion and oxidation resistance and high tensile and creep-rupture properties at temperatures to 815ºC (1500ºF). Used for gas-turbine components (blades, rings, discs), bolts, tube supports in nuclear generators, exhaust valves in internal combustion engines.
MECHANICAL PROPERTIES Alloy 80A
(This material was Precipitation Hardened)
Many sizes and forms available Alloy 80A Bar Alloy 80A Extruded Section Alloy 80A Tube Alloy 80A Plate Alloy 80A Sheet Alloy 80A Wire Disclaimer Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.
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