发明名称 Clutch system for rotary-wing aircraft with secondary thrust system
摘要 A aircraft, 10, includes a powerplant system, 26, operable to power a main rotor system , 12, and a secondary thrust system, 30, the secondary thrust system is selectively driven through operation of a clutch system, 34C, and a clutch system synchronization time corresponds to a response time of the powerplant systems, 26.
申请公布号 EP2615033(A2) 申请公布日期 2013.07.17
申请号 EP20120198637 申请日期 2012.12.20
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 LONG, CHARLES E.;NOREM, DEAN A.;WEYL, RAYMOND N.;REIMERS, RICKY D.
分类号 B64D35/04;B64C27/10;B64C27/12;B64C27/22 主分类号 B64D35/04
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