ROTOR DRIVE AND CONTROL SYSTEM FOR A HIGH SPEED ROTARY WING AIRCRAFT
摘要
A drive system for a high speed rotary-wing aircraft includes a combiner gearbox in meshing engagement with a main gearbox. The combiner gearbox is driven by one or more engines such that a main rotor system and a translational thrust system are driven thereby. The engine drives the combiner gearbox and thus the main gearbox through an overrunning clutch. The drive system permits the main rotor system RPM to be controlled by offloading power to the translational thrust system during a high speed flight profile.
申请公布号
WO2007084171(A2)
申请公布日期
2007.07.26
申请号
WO2006US16640
申请日期
2006.04.28
申请人
SIKORSKY AIRCRAFT CORPORATION
发明人
COTTON, BRYAN, S.;TULLY, THOMAS, J., JR.;GMIRYA, YURIY, Z.