Material system for high temperature jet engine operation

Details Material system for high temperature jet engine operation Material system for high temperature jet engine operation

B - Operations, Transporting

32

B

13/7

B32B 15/00 (2006.01) B32B 15/01 (2006.01) C23C 30/00 (2006.01)

Patent

CA 2009599

RD-18,980 3/30/89 MATERIAL SYSTEM FOR HIGH TEMPERATURE JET ENGINE OPERATION ABSTRACT OF THE DISCLOSURE A materials system is provided which is adapted for use in jet engines operable at higher temperature and at lower density than possible with nickel base superalloys. A range of niobium base alloys is combined with a range of protective metallic coatings to provide a material system which permits a wide variety of alloy properties and performance characteristics to be combined in structural components of jet engines.

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