Compressor temperature control system and method

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United States of America Patent

PATENT NO 10829226
APP PUB NO 20170341757A1
SERIAL NO

15595154

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Abstract

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A compressor temperature control system and method for an aircraft air cycle machine is presented. The system prevents overheating of the compressor using a low limit valve positioned between a turbine outlet and a bleed air source. The low limit valve directs the air to an air cycle machine, or bypasses the machine, in regards at least in part to the air temperature measured in the cabin supply duct.

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Patent Owner(s)

Patent OwnerAddress
TEXTRON AVIATION RHODE ISLAND INC40 WESTMINSTER STREET PROVIDENCE RI 02903

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Thompson, Clinton Lee Wichita, US 5 7
Weber, Scott William Goddard, US 3 5

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