- 专利标题： AIR TURBINE STARTER WITH DECOUPLER
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申请号： US15180728申请日： 2016-06-13
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公开(公告)号： US20170356345A1公开(公告)日： 2017-12-14
- 发明人: Eliel Fresco Rodriguez , David Allan Dranschak , Shiloh Montegomery Emerson Meyers
- 申请人： GE AVIATION SYSTEMS, LLC
- 主分类号： F02C7/277
- IPC分类号： F02C7/277 ; F16D9/08 ; F02C7/36
摘要：
A method and decoupler for disengaging an output shaft from an engine in a back drive event with a backdrive decoupler. The backdrive decoupler includes a an output shaft, drive shaft, and a retention mechanism selectively coupling the output shaft to the drive shaft. In a backdrive event, the decoupler decouples the output shaft from the drive shaft.
公开/授权文献
- US10584640B2 Air turbine starter with decoupler 公开/授权日：2020-03-10
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