Compressor blade containment with composite stator vanes

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Specific casing or vane material

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Details

2988971, 416229A, 416230, 416241A, F01D 904

Patent

active

056054416

ABSTRACT:
Stator vanes located between compressor stages in a gas turbine engine are fabricated with a composite outer shell made of graphite fibers in an epoxy binder that is laid-up over a core of felt-like material selected to have an elongation velocity that is greater than the elongation velocity of the shell.

REFERENCES:
patent: 5439353 (1995-08-01), Cook et al.
patent: 5509781 (1996-04-01), Boszor et al.

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