Gas turbine engine and composite parts

Stock material or miscellaneous articles – Composite – Of inorganic material

Patent

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Details

428698, 428107, 428114, 428112, 428294, 428367, 428902, B32B 502, B32B 508, B32B 1508

Patent

active

047389028

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.

REFERENCES:
patent: 4324843 (1982-04-01), Brennan et al.
patent: 4341826 (1982-07-01), Prewo et al.

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