Invention Grant
- Patent Title: Thermal management system for gas turbine engine
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Application No.: US14533611Application Date: 2014-11-05
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Publication No.: US09863318B2Publication Date: 2018-01-09
- Inventor: Michael Joseph Murphy
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F02C7/14 ; F01D17/08 ; F01D17/14 ; F02K3/075 ; F02C9/18 ; F01D25/12 ; F02C7/18

Abstract:
A method of thermal management for a gas turbine engine comprising selectively positioning a valve to communicate a bypass flow into either an Environmental Control System (ECS) pre-cooler or an Air Oil Cooler (AOC) “peaker” through a common inlet.
Public/Granted literature
- US20150052907A1 THERMAL MANAGEMENT SYSTEM FOR GAS TURBINE ENGINE Public/Granted day:2015-02-26
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