Invention Grant
- Patent Title: Multi-mode heat rejection system for a gas turbine engine
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Application No.: US16867155Application Date: 2020-05-05
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Publication No.: US11378009B2Publication Date: 2022-07-05
- Inventor: Gary D. Roberge
- 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: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C7/14
- IPC: F02C7/14 ; F02C9/20 ; F02C7/18 ; F02K3/06 ; F02C9/16
Abstract:
A turbine engine includes a duct defining an annular passage, at least two heat exchangers arranged within the annular passage and spaced circumferentially apart, a passage between the at least two heat exchangers, and a forward flow control device operable for controlling airflow through the passages.
Information query
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