Damper for a turbine rotor assembly

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 9347325
APP PUB NO 20140119916A1
SERIAL NO

13665453

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A damper for a turbine rotor assembly of a gas turbine engine may include a forward plate with a forward face and an aft face, and an aft plate with a forward face and an aft face. The aft face of the forward plate may be connected to the forward face of the aft plate with a longitudinal structure. An area of the aft plate in a plane transverse to the longitudinal structure may be greater than an area of the forward plate in the plane transverse to the longitudinal structure. The damper may also include a pocket on the forward face of the forward plate.

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Patent Owner(s)

  • SOLAR TURBINES INCORPORATED

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Faulder, Leslie John San Diego, US 10 88
Tarczy, Jeffrey Eugene San Diego, US 5 56

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