Stator vane assembly for a gas turbine engine

Rotary kinetic fluid motors or pumps – Including thermal expansion joint – Radially sliding

Reexamination Certificate

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Details

C415S191000

Reexamination Certificate

active

07025563

ABSTRACT:
A low-pressure compressor exit stator assembly for a gas turbine includes a multiple of vanes mounted between a full hoop outer shroud and an inner shroud. The outer shroud and inner shroud are mounted to the intermediate case structure. A seal is located between the outer shroud and a bleed duct structure to accommodate thermal growth mismatch.

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patent: 6139264 (2000-10-01), Schilling
patent: 6347508 (2002-02-01), Smallwood et al.
patent: 6607355 (2003-08-01), Cunha et al.
patent: 2005/0008486 (2005-01-01), Malmborg

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