Alloy for roller bearing

Details Alloy for roller bearing Alloy for roller bearing

C - Chemistry, Metallurgy

22

C

C22C 38/24 (2006.01) C22C 38/22 (2006.01) F16C 19/00 (2006.01) B64C 25/36 (2006.01) C22C 38/46 (2006.01)

Patent

CA 2582185

An alloy for aircraft roller bearings containing: 0.45 to 1.0 wt. % carbon, max 2.0 wt. % manganese, max 1.0 wt. % silicon, 8.5 to 11.5 wt. % chromium, 1.0 to 4.5 wt. % molybdenum, 1.0 to 2.5 wt. % vanadium, max 2.0 wt. % tungsten, max 0.5 wt. % niobium, max 0.5 wt. % tantalum, max 3.0 wt. % nickel, max 0.5 wt. % cobalt, max 0.1 wt. % aluminum, max 0.01 wt. % nitrogen, and the balance being iron and impurities due to production.

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