Invention Grant
- Patent Title: Gas turbine engine diffuser cooling and mixing arrangement
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Application No.: US14913922Application Date: 2014-07-18
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Publication No.: US10677161B2Publication Date: 2020-06-09
- Inventor: Christopher B. Lyons , Albert K. Cheung
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- International Application: PCT/US2014/047143 WO 20140718
- International Announcement: WO2015/030948 WO 20150305
- Main IPC: F02C6/08
- IPC: F02C6/08 ; F01D5/08 ; F01D25/12 ; F02C7/18 ; F04D29/54 ; F02C6/06 ; F01D9/06

Abstract:
A diffuser for a gas turbine engine includes a diffuser housing that has a circumferential array of hollow struts that provide a cavity. The diffuser housing includes inlet and outlet apertures that are in fluid communication with the cavity. An opening on a trailing end of the struts is in fluid communication with the cavity. The diffuser housing is configured to introduce a fluid through the inlet aperture and receive a core flow through the opening. The fluid and core flow exit through the outlet aperture.
Public/Granted literature
- US20160201688A1 GAS TURBINE ENGINE DIFFUSER COOLING AND MIXING ARRANGEMENT Public/Granted day:2016-07-14
Information query
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