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US 5,509,781 AGranted
Compressor blade containment with composite stator vanes
AssigneeUnited Technologies Corporation
InventorsSamuel M. Boszor, Stuart A. Sanders
Life of this patent
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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.
Claims7
A gas turbine engine comprising stator blades located between compressor stages, characterized by:
- the stator blades including a composite shell of fibers laid-up over a core, said core comprising randomly oriented fibers selected to have an elongation velocity that exceeds the elongation velocity of said fibers in said composite shell and said shell comprising a binder bonded to said core.
A method of constructing stator vanes characterized by:
- laying a composite surface over a fiber core to form a vane skin, said surface comprising fibers in a binder that attaches to the core, the elongation velocity of fibers in the core being greater than the elongation velocity of the fibers in the composite surface and the fibers in the core being randomly oriented.
A stator vane characterized by:
- a core comprising at least four plies of T1000 in polyimide resin;
- and
- a shell, covering the core, comprising at least four plies of graphite and polyimide.
Dependencies are inferred from the claim text.