Invention Grant
- Patent Title: Gas turbine engine with plural accessory air paths
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Application No.: US16264837Application Date: 2019-02-01
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Publication No.: US10787966B2Publication Date: 2020-09-29
- Inventor: Gabriel L. Suciu , Jesse M. Chandler
- 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.
- Main IPC: F02C7/18
- IPC: F02C7/18 ; F02C6/08 ; F02K3/062 ; F02K3/06 ; F01D25/12 ; F02C9/18 ; B64D13/06
Abstract:
A gas turbine engine has a first source of air to be delivered into a core of the engine, and a second source of air, distinct from the first source of air and including separately controlled first and second fans, each delivering air into respective first and second conduits connected to distinct auxiliary applications.
Public/Granted literature
- US20190162118A1 GAS TURBINE ENGINE WITH PLURAL ACCESSORY AIR PATHS Public/Granted day:2019-05-30
Information query
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