Ultrahigh-purity dimensionally stable INVAR 36
AssigneeThe United States of America as represented by the Administrator of the National Aeronautics and Space Administration
InventorsWitold M. Sokolowski, Marc S. Lane, Cheng H. Hsieh, Timothy P. O'Donnell
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Abstract
An INVAR 36 material having long-term dimensional stability is produced by sintering a blend of powders of nickel and iron under pressure in an inert atmosphere to form an alloy containing less than 0.01 parts of carbon and less than 0.1 part aggregate and preferably 0.01 part individually of Mn, Si, P, S, and Al impurities. The sintered alloy is heat treated and slowly and uniformly cooled to form a material having a coefficient of thermal expansion of less than 1 ppm/.degree.C. and a temporal stability of less than 1 ppm/year.
Claims5
A method of forming an alloy of iron and nickel having long term dimensional stability comprising the steps of:
- blending powders of nickel and iron in the proportions of 36 parts of Ni.+-.1.0 parts, remainder Fe, having an impurities content below 1 part and containing less than 0.01 parts of carbon to form an intimate mixture;
- sintering the mixture in a hydrogen atmosphere under pressure to form an alloy in which the total carbon in the alloy does not exceed 0.01 parts and Mn, Si, P, S and Al impurities do not individually and collectively exceed 0.01 parts;
- heat treating the alloy to a first temperature of 1375.degree. F. to 1475.degree. F. in an inert atmosphere and holding the alloy at the first temperature for 10 to 60 minutes for each inch of section thickness of the alloy;
- then uniformly furnace cooling the alloy at a rate not to exceed 100.degree. F./hour to a temperature of about 300.degree. F. and then air cooling the alloy to room temperature;
- then heating the alloy to a second temperature of from 500.degree. F. to 700.degree. F. in a protective atmosphere and holding the alloy at the second temperature for at least one-half hour and then furnace cooling the alloy at a rate not to exceed 100.degree. F. per hour to 300.degree. F. and then air cooling the alloy to room temperature;
- then heating the alloy to a third temperature of from 150.degree. F. to 300.degree. F. in a protective atmosphere, holding the alloy at the third temperature for at least 24 hours and air cooling the alloy to room temperature;
- and
- recovering an alloy having a coefficient of thermal expansion at -50.degree. C. to 50.degree. C. of less than 1 ppm/.degree.C./year and a temporal stability of less than 1 ppm/year at 27.5.degree. C.
Dependencies are inferred from the claim text.