Diffuser pipe with axially-directed exit

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 11435079
APP PUB NO 20200393129A1
SERIAL NO

16440213

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Importance

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Abstract

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A compressor diffuser for a gas turbine engine includes diffuser pipes having a tubular body including a generally radial portion, a bend portion and a generally axial portion. The generally axial portion has an exit segment extending parallel to the center axis and terminating at a pipe outlet. The bend portion is disposed radially further from the center axis than the exit segment.

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Patent Owner(s)

Patent OwnerAddress
PRATT & WHITNEY CANADA CORP1000 MARIE VICTORIN BLVD LONGUEUIL QU J4G 1A1

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Duong, Hien Mississauga, CA 57 230

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