C - Chemistry – Metallurgy – 04 – B
Patent
C - Chemistry, Metallurgy
04
B
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.
447018
Brennan John J.
Prewo Karl M.
Ogilvy Renault
United Technologies Corporation
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