Heat resistant alloy and method of manufacture

Details Heat resistant alloy and method of manufacture Heat resistant alloy and method of manufacture

1979-02-14

1981-07-21

Dean, R.

Specialized metallurgical processes, compositions for use therei

Processes

Free metal or alloy reductant contains magnesium

75134F, 75171, C22C 1905

Patent

active

042796458

ABSTRACT:
In accordance with the invention there is provided an alloy having high hardness and wear resistance even at elevated temperatures, the alloy consisting essentially of from about 35% to 65% nickel, 15% to 25% chromium, 5% to 20% cobalt, 2% to 5% molybdenum, 1.5% to 4% titanium, 1% to 12% iron, 0.5% to 2% aluminum, 0.3% to 2% silicon, 0.7% to 2% carbon and 1% to 4% boron.

REFERENCES:
patent: 4108647 (1978-08-01), Shaw

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