发明名称 ROTATION OF DISENGAGED ROTOR
摘要 Embodiments of the invention include a vehicle including an engine and a rotor including a plurality of rotor blades in a path of exhaust from the engine. The vehicle includes a rotor control assembly configured to connect the rotor to a rotation force source to rotate the rotor and configured to rotate the rotor at a prescribed minimum rotation rate greater than zero based on at least one of disengaging the rotor from the rotation force source and receiving a control signal to disengage the rotor from the rotation force source. The rotor control assembly is designed to rotate the rotor at the prescribed minimum rotation rate based on at least one system attribute of the vehicle that is affected by a rotation rate of the rotor.
申请公布号 WO2016007403(A3) 申请公布日期 2016.03.03
申请号 WO2015US39181 申请日期 2015.07.06
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 DEVITO, ASHLEY;VOEGELI, HENRY E.;PANTALONE III, JOSEPH
分类号 B64C27/04;B64C27/12 主分类号 B64C27/04
代理机构 代理人
主权项
地址