Invention Grant
- Patent Title: Integrated thermal system for a gas turbine engine
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Application No.: US14729800Application Date: 2015-06-03
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Publication No.: US09797311B2Publication Date: 2017-10-24
- Inventor: Gabriel L. Suciu , Allan R. Penda , Brian D. Merry , Christopher M. Dye , Nathan Snape
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C7/18
- IPC: F02C7/18 ; F02C7/14 ; F02C7/08

Abstract:
A thermal system for a gas turbine engine includes a bypass flow duct and a compressor flow duct which meets with the bypass flow duct at an intersection. A valve is located within the intersection and is movable between a first position and a second position. First position is operable to selectively communicate fan bypass flow from the bypass flow duct and block the compressor flow duct. The second position is operable to selectively block the bypass flow duct and communicate bleed flow through the compressor flow duct.
Public/Granted literature
- US20150267617A1 INTEGRATED THERMAL SYSTEM FOR A GAS TURBINE ENGINE Public/Granted day:2015-09-24
Information query
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