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US Patent 9016695 Gas turbine exhaust nozzle divergent flap seal

Patent 9016695 was granted and assigned to United Technologies on April, 2015 by the United States Patent and Trademark Office.

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Patent abstract

A seal assembly for a nozzle in a gas turbine engine includes a connector having a first hinge portion for attaching to the nozzle, a flat portion for sealing against a wall of the engine; and a first hinge for attaching the connector to the flat portion wherein the connector is adapted to rotate relative to the nozzle and the flat portion is adapted to rotate relative to the connector.

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