Fan exhaust nozzle for turbofan engine

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United States of America Patent

PATENT NO 8561384
APP PUB NO 20110014045A1
SERIAL NO

12893042

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Abstract

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The cross sectional flow area of a fan discharge nozzle on one side of a central plane of an associated gas turbine engine power plant is greater than the corresponding flow area of the fan discharge nozzle on an opposite side of the central plane to compensate for the blockage of fan airflow by a pylon.

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
McCall, John Andover, US 32 116

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