Invention Application
- Patent Title: GAS TURBINE ENGINE AND METHOD TO COOL A GAS TURBINE ENGINE CASE ASSEMBLY
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Application No.: US15185820Application Date: 2016-06-17
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Publication No.: US20170363003A1Publication Date: 2017-12-21
- Inventor: Joseph D. Evetts , William J. Riordan , Federico Papa
- Applicant: United Technologies Corporation
- Main IPC: F02C7/12
- IPC: F02C7/12 ; B64D29/00 ; F02C3/04 ; F02C9/18 ; F01D25/24

Abstract:
A method of cooling a gas turbine engine case assembly includes moving a fan air valve that is operatively connected to a pre-cooler having a bypass inlet that is configured to receive bypass air that bypasses a gas turbine engine core to facilitate a provision of bypass air through a fan air valve inlet to the bypass inlet to a first open position, in response to a core compartment temperature being greater than a target core compartment temperature. The method further includes bleeding the bypass air through a bypass outlet of the pre-cooler into a core compartment.
Information query
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