Bleed air systems for use with aircrafts and related methods

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United States of America Patent

PATENT NO 8967528
SERIAL NO

13357293

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Abstract

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Bleed air systems for use with aircrafts and related methods are disclosed. An example apparatus includes a turbo-compressor including a compressor having a compressor inlet fluidly coupled to a low-pressure compressor of the aircraft engine and a compressor outlet fluidly coupled to a first system of an aircraft. The turbo-compressor also includes a turbine inlet fluidly coupled to a high-pressure compressor of the aircraft engine and a turbine outlet fluidly coupled to a second system of the aircraft.

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Patent Owner(s)

Patent OwnerAddress
THE BOEING COMPANY100 NORTH RIVERSIDE PLAZA CHICAGO IL 60606-2016

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Ludlow, George A Kirkland, US 2 149
Mackin, Steve G Bellevue, US 57 1038

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