发明名称 SINGLE COLLECTIVE STICK FOR A ROTARY WING AIRCRAFT
摘要 An aircraft is provided including an airframe, an extending tail, and a counter rotating, coaxial main rotor assembly including an upper rotor assembly and a lower rotor assembly. A translational thrust system positioned at the extending tail, the translational thrust system providing translational thrust to the airframe. A cockpit in the airframe, the cockpit including two seats and a single collective control input positioned between the two seats.
申请公布号 WO2016054215(A1) 申请公布日期 2016.04.07
申请号 WO2015US53229 申请日期 2015.09.30
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 BREDENBECK, KEVIN L.;FELL, WILLIAM;ELLER, EREZ
分类号 B64C13/50 主分类号 B64C13/50
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