ACOUSTIC SIGNATURE VARIATION OF AIRCRAFT UTILIZING A CLUTCH
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 including a propeller is positioned at the extending tail. The translational thrust system provides translational thrust to the airframe. A drive system is configured to operate both the main rotor system and the translational thrust system. The drive system includes a clutch configured to selectively couple or decouple the propeller from the drive system.
申请公布号
WO2016053408(A1)
申请公布日期
2016.04.07
申请号
WO2015US36354
申请日期
2015.06.18
申请人
SIKORSKY AIRCRAFT CORPORATION
发明人
GARCIA, TODD, A.;EADIE, WILLIAM, J.;STILLE, BRANDON, L.