Patent ID: 9562274
Date: 2017-02-07
CPC Classifications: C21D

Claim:
1. A method of making an ultra-high strength stainless steel alloy suitable in the manufacture of aircraft landing gear comprising the steps of: (a) providing an alloy comprising 0 to 0.06% carbon (C); 12.0 to 18% chromium (Cr); 18.0 to 31.0% cobalt (Co); 0 to 8% molybdenum (Mo); 0.5 to 5.0% nickel (Ni); 0 to 0.5% titanium (Ti); 0 to 1.0% niobium (Nb); 0 to 0.5% vanadium (V); 0 to 16% tungsten (W); balance iron (Fe) and incidental deoxidizers and impurities; (b) austenitizing the alloy; (c) cooling the austenitized alloy to room temperature; and (d) tempering the austenitized and cooled alloy, wherein step (d) is performed after step (c) without any further processing being conducted in between.