Stator vane seal arrangement for a gas turbine engine
AssigneePratt & Whitney Canada Corp.
InventorsTibor Urac, Bernadette Mason
Life of this patent
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AssigneePratt & Whitney Canada Corp.
InventorsTibor Urac, Bernadette Mason
Estimating the term…
A seal spacer for a gas turbine engine to provide sealing between a casing wall and a stator vane of the engine. The seal spacer comprises a circumferential body having a slot defined therethrough and configured to receive the stator vane therein. The circumferential body is configured to be disposed between and space apart the engine casing wall from a head of the stator vane when the vane is inserted in the slot and the vane is inserted in the opening in the casing wall. The circumferential body includes a support positioned to be engage and provide a gap between the casing wall and the head when the seal spacer is installed therebetween, and an elastomeric seal portion positioned to engage and compressingly provide sealing the casing wall and the head when the seal spacer is installed therebetween to seal the gap.
A seal spacer for a gas turbine engine, for providing sealing between a casing wall of the engine and a stator vane inserted into a corresponding opening provided in the casing wall of the engine, the seal spacer comprising:
A stator vane assembly for a gas turbine engine, the gas turbine engine comprising an annular casing wall portion defining a duct and having a plurality of openings circumferentially defined therein, the stator vane assembly comprising:
A method for sealing a gap defined between a casing wall and a head of a stator vane of a gas turbine engine, the method comprising:
Dependencies are inferred from the claim text.