Stator vane assembly for a gas turbine engine

Details Stator vane assembly for a gas turbine engine Stator vane assembly for a gas turbine engine

2006-04-11

2006-04-11

Look, Edward K. (Department: 3745)

Rotary kinetic fluid motors or pumps

Including thermal expansion joint

Radially sliding

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: 2005/0008486 (2005-01-01), Malmborg

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