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United States of America Patent

PATENT NO 9790803
SERIAL NO

14185962

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A rotor assembly for a gas turbine engine includes a plurality of blades including a root portion and an airfoil portion. The rotor includes a plurality of slots that receive the root portion of a corresponding blade. The rotor includes an annular groove for a first and second retaining ring. The retaining rings are received within a common annular groove for holding each of the plurality of blades within the slots of the rotor.

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First Claim

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Anderson, Carney R East Haddam, US 19 88
Tomeo, Peter V Middletown, US 16 70

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