ROTARY WING AIRCRAFT AND METHOD OF CONTROLLING A ROTARY WING AIRCRAFT
摘要
A method of controlling a rotary wing aircraft includes accelerating the aircraft in a fore direction independently of cyclic control of the main rotor and pitch of the aircraft.
申请公布号
WO2016053777(A2)
申请公布日期
2016.04.07
申请号
WO2015US52142
申请日期
2015.09.25
申请人
SIKORSKY AIRCRAFT CORPORATION
发明人
EADIE, WILLIAM J.;WEINER, STEVEN D.;BREDENBECK, KEVIN L.
