High-temperature member for use in gas turbine

Details High-temperature member for use in gas turbine High-temperature member for use in gas turbine

C - Chemistry, Metallurgy

22

C

C22C 19/07 (2006.01) C22F 1/10 (2006.01) F01D 5/28 (2006.01)

Patent

CA 2419018

Disclosed herein is a high-temperature member for use in a gas turbine, the member being formed from a new wear-resistant alloy having good wear resistance as well as good ductility. the member was developed to prevent wear and damage that occur due to vibration while the turbine is running. The high-temperature member for use in a gas turbine is formed from a new cobalt-based wear-resistant alloy which is composed of a cobalt-chromium matrix and refractory metals, with the content of hard particles (such as carbide) reduced. The refractory metals promote work hardening, thereby improving wear resistance. The reduced content of hard particles contributes to good ductility.

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