- 专利标题： GAS TURBINE ENGINE WITH PLURAL ACCESSORY AIR PATHS
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申请号： US16264837申请日： 2019-02-01
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公开(公告)号： US20190162118A1公开(公告)日： 2019-05-30
- 发明人: Gabriel L. Suciu , Jesse M. Chandler
- 申请人： United Technologies Corporation
- 主分类号： F02C7/18
- IPC分类号： F02C7/18 ; F02K3/06 ; F02K3/062 ; F02C9/18 ; F01D25/12 ; F02C6/08
摘要：
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.
公开/授权文献
- US10787966B2 Gas turbine engine with plural accessory air paths 公开/授权日：2020-09-29
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