MECHANICAL FLIGHT CONTROL AUXILIARY POWER ASSIST SYSTEM
摘要
A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and a booster means for connecting the upstream portion to the downstream portion. The booster means may comprise dual concentric valve actuators and/or a variety of system load limiting features.
申请公布号
WO2006137908(A2)
申请公布日期
2006.12.28
申请号
WO2005US36714
申请日期
2005.10.13
申请人
BELL HELICOPTER TEXTRON INC.;SHULTZ, PETER, M.;FENNY, CARLOS, A.;WALKER, TODD;ARJUNAN, SAM
发明人
SHULTZ, PETER, M.;FENNY, CARLOS, A.;WALKER, TODD;ARJUNAN, SAM