A process for producing static components for a gas turbine...

Details A process for producing static components for a gas turbine... A process for producing static components for a gas turbine...

C - Chemistry, Metallurgy

22

C

C22C 19/00 (2006.01) B22F 1/00 (2006.01) B22F 3/12 (2006.01) B22F 5/00 (2006.01) C22C 19/05 (2006.01) F01D 9/00 (2006.01) F01D 25/24 (2006.01) F23R 3/60 (2006.01)

Patent

CA 2588626

Static components for a gas turbine engine formed from a metal injection molding process. The static components are made from an alloy in the group consisting of Inconel 625, Inconel 718, MAR-M 247 or any nickel, cobalt or nickel-iron superalloy and have a density less than 99% of a theoretical possible density for the alloy.

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