Flow deflector for aperture in gas turbine engine flowpath wall

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United States of America Patent

PATENT NO 11873737
SERIAL NO

17871582

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Importance

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Abstract

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A system is provided for a gas turbine engine. This gas turbine engine system includes a flowpath wall and a deflector. The flowpath wall includes a surface and an opening to a blind aperture. The surface forms a peripheral boundary of an internal engine flowpath. The opening is disposed in the surface. The blind aperture extends vertically into the flowpath wall from the opening. The deflector projects vertically out from the flowpath wall into the internal engine flowpath. The deflector is configured to deflect gas flowing within the internal engine flowpath over the opening.

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Patent Owner(s)

Patent OwnerAddress
PRATT & WHITNEY CANADA CORPLONGUEUIL

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Mirmohammadi, Ghoojdi Tahereh Sainte-Julie, CA 3 0

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