Strut for a gas turbine engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8784051
APP PUB NO 20090324400A1
SERIAL NO

12164565

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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The strut is for use in a gas turbine engine has body, typically having an airfoil shape, having a leading edge and a trailing edge. The leading edge has at least one gas inlet in direct fluid communication with at least one outlet located in the trailing edge through which gas may be redirected from the leading edge to the trailing edge through the strut for injection back into a wake region downstream of the strut.

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Patent Owner(s)

  • PRATT & WHITNEY CANADA CORP.

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Findlay, Jonathon Peter Edmonton, CA 3 28
Marini, Remo Montreal, CA 24 452
Vlasic, Edward Beaconsfield, CA 18 558

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