Rotor blade retention system for a gas turbine engine

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United States of America Patent

PATENT NO 11519278
APP PUB NO 20220282626A1
SERIAL NO

17193064

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A rotor blade retention system for a gas turbine engine includes a rotor blade connection component defining a slot, with the rotor blade connection component including a first set of electric leads. Furthermore, the rotor blade retention system includes a rotor blade having a root section received within the slot, with the rotor blade further including a second set of electric leads. In this respect, the first and second sets of electric leads are electrically coupled together to permit electric current to be supplied to the rotor blade.

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Patent Owner(s)

  • GENERAL ELECTRIC COMPANY

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Kray, Nicholas Joseph Mason, US 170 733
Kryj-Kos, Elzbieta Liberty Township, US 9 9

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