Integrated strut and IGV configuration

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United States of America Patent

PATENT NO 10808556
SERIAL NO

16122295

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Abstract

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A strut and IGV configuration in a gas turbine engine positioned at an upstream of a rotor includes a plurality of radial struts, for example for bearing engine loads, and a plurality of inlet guide vanes positioned axially spaced apart from the struts. The number of inlet guide vanes is greater than the number of struts. The struts are circumferentially aligned with the inlet guide vanes.

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Patent Owner(s)

Patent OwnerAddress
PRATT & WHITNEY CANADA CORPLONGUEUIL

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Dutton, Ronald Guelph, CA 8 72
Yu, Hong Oakville, CA 273 2709

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