Invention Grant
- Patent Title: Gas turbine engine and method to cool a gas turbine engine case assembly
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Application No.: US16812807Application Date: 2020-03-09
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Publication No.: US11149641B2Publication Date: 2021-10-19
- Inventor: Joseph D. Evetts , William J. Riordan , Federico Papa
- Applicant: Raytheon Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F02C7/12
- IPC: F02C7/12 ; F02C7/18 ; F02C6/08 ; B64D29/00 ; F01D25/24 ; F02C3/04 ; F02C9/18 ; B64D13/08 ; F01D11/24

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.
Public/Granted literature
- US20200208576A1 GAS TURBINE ENGINE AND METHOD TO COOL A GAS TURBINE ENGINE CASE ASSEMBLY Public/Granted day:2020-07-02
Information query
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