Particle tolerant turboshaft engine

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United States of America Patent

PATENT NO 9869250
SERIAL NO

14707208

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A gas turbine engine includes a core engine section which includes a compressor section and a core turbine section. The core engine is configured to rotate about a core axis. A drive turbine is configured to rotate about a drive turbine axis. A bypass passage connects an intake to the gas turbine engine directly with an exhaust of the drive turbine.

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Hanrahan, Paul R Farmington, US 61 171
Kupratis, Daniel Bernard Wallingford, US 195 1435

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