Bleed structure for a bleed passage in a gas turbine engine

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United States of America Patent

PATENT NO 8528344
APP PUB NO 20100199633A1
SERIAL NO

12752284

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Abstract

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A bleed structure for a bleed passage in a gas turbine engine includes a first wall portion defining a first side of an opening for the passage, and a second wall portion defining a second side, opposite the first side of the opening. The first and second wall portions end at different positions in an extension direction of the opening.

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Patent Owner(s)

Patent OwnerAddress
VOLVO AERO CORPORATIONS-461 81 TROLLHATTAN

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Mårtensson, Hans Trollhättan, SE 10 39
Nilsson, Martin Göteborg, SE 34 202

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