Improvements relating to nickel-chromium alloys

An alloy resistant to creep and to corrosion at high temperatures contains Cr 4-12 per cent, Ti 3.5-8 per cent, Al 0.9-5 per cent, the combined contents of Al and Ti being 4.5-10 per cent, and the balance, except for impurities and residual deoxidants, being Ni. The alloy may also contain Co less th...

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Hauptverfasser: BETTERIDGE WALTER, FRANKLIN ARTHUR WILLIAM, SMITH RONALD ALFRED
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creator BETTERIDGE WALTER
FRANKLIN ARTHUR WILLIAM
SMITH RONALD ALFRED
description An alloy resistant to creep and to corrosion at high temperatures contains Cr 4-12 per cent, Ti 3.5-8 per cent, Al 0.9-5 per cent, the combined contents of Al and Ti being 4.5-10 per cent, and the balance, except for impurities and residual deoxidants, being Ni. The alloy may also contain Co less than 10 per cent, Zr up to 0.2 per cent, B up to 0.01 per cent, C up to 0.25 per cent, Fe up to 10 per cent, W up to 5, per cent Mo up to 5 per cent, Mn up to 1 per cent, Si up to 1.5 per cent, Nb or Ta up to 1 per cent. The alloy may be subjected to a heat treatment comprising solution heating at 1050-1250 DEG C., intermediate heating at 750-1100 DEG C. and finally precipitation hardening at 650-850 DEG C. Specification 583,162 is referred to.
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The alloy may also contain Co less than 10 per cent, Zr up to 0.2 per cent, B up to 0.01 per cent, C up to 0.25 per cent, Fe up to 10 per cent, W up to 5, per cent Mo up to 5 per cent, Mn up to 1 per cent, Si up to 1.5 per cent, Nb or Ta up to 1 per cent. The alloy may be subjected to a heat treatment comprising solution heating at 1050-1250 DEG C., intermediate heating at 750-1100 DEG C. and finally precipitation hardening at 650-850 DEG C. 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The alloy may also contain Co less than 10 per cent, Zr up to 0.2 per cent, B up to 0.01 per cent, C up to 0.25 per cent, Fe up to 10 per cent, W up to 5, per cent Mo up to 5 per cent, Mn up to 1 per cent, Si up to 1.5 per cent, Nb or Ta up to 1 per cent. The alloy may be subjected to a heat treatment comprising solution heating at 1050-1250 DEG C., intermediate heating at 750-1100 DEG C. and finally precipitation hardening at 650-850 DEG C. 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subjects ALLOYS
CHEMISTRY
FERROUS OR NON-FERROUS ALLOYS
METALLURGY
TREATMENT OF ALLOYS OR NON-FERROUS METALS
title Improvements relating to nickel-chromium alloys
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