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US Patent 10208676 Gas turbine engine dual sealing cylindrical variable bleed valve

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Contents

Is a
Patent
Patent

Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10208676
Date of Patent
February 19, 2019
Patent Application Number
15083392
Date Filed
March 29, 2016
Patent Citations Received
‌
US Patent 12085027 Compressor bleed for gas turbine engine
0
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US Patent 11912425 Aircraft propulsion unit
0
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US Patent 11940816 Aircraft control system and method
0
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US Patent 11479146 Battery thermal management system and method
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US Patent 11230384 Vehicle cabin thermal management system and method
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US Patent 11548407 Battery thermal management system and method
‌
US Patent 11560968 Bleed valve with reduced noise
‌
US Patent 11560235 Aircraft propulsion unit
...
Patent Primary Examiner
‌
Craig Kim
Patent abstract

Axially adjacent annular booster bleed aft and forward plenums with annular common wall therebetween extend radially outwardly from transition duct. Variable bleed valve includes bleed valve door in bleed inlet in transition duct, attached to rotatable valve body rotatable about axis of rotation, operable to open and close bleed inlet to aft plenum. Rotatable plenum door clocked or circumferentially spaced apart from variable bleed valve door and attached to rotatable valve body, operable to close and open up and control flow through an inter plenum aperture in common wall. Aft and forward bleed exhaust ducts extend from booster bleed aft and forward plenums to bypass flow path. One or more heat exchanger, such as from thermal management system, may be disposed in the bleed exhaust ducts. Heat exchangers may be used for cooling oil for power gear box and/or engine bearings, air conditioning, or variable frequency generator.

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