Gas turbine engine and composite parts

C - Chemistry – Metallurgy – 04 – B

Patent

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25/135, 261/6

C04B 35/80 (2006.01)

Patent

CA 1230621

Abstract High strength, fracture tough, high temperature oxidatively stable, gas turbine engine core engine components are described made of silicon carbide fiber reinforced ceramic matrix or silicon carbide fiber reinforced glass matrix material. A gas turbine engine containing core engine components as above described is also disclosed.

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