High Speed Engine Reduction Gearboxes

申请号 US15709548 申请日 2017-09-20 公开(公告)号 US20180087639A1 公开(公告)日 2018-03-29
申请人 Bell Helicopter Textron Inc.; 发明人 Scott David Poster; Walter Riley; Gary Cope; Charles Hubert Speller, JR.;
摘要 An engine reduction gear system includes at least two self-contained, independent engine reduction gearboxes, each capable of connecting to an aircraft engine. Each of the engine reduction gearboxes provides redundant, reduced speed to a main rotor gearbox via a shaft.
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