发明名称 Helicopter, rotor thereof, and control method thereof
摘要 A helicopter rotor include a blade, a rotor hub which supports the blade, and a lead-lag angle mechanism configured to change the lead-lag angle of the blade in synchronization with the rotation of the rotor hub. The lead-lag angle mechanism changes the lead-lag angle of the blade such that a circumferential speed of a blade tip of the blade (3) is slower on a forward side and faster on a backward side. The result is a helicopter, a helicopter rotor, and a control method of a helicopter that enable higher speed flight.
申请公布号 US8911209(B2) 申请公布日期 2014.12.16
申请号 US200912811295 申请日期 2009.01.09
申请人 Mitsubishi Heavy Industries, Ltd. 发明人 Nakao Masahiro
分类号 B64C27/635;B64C27/51;B64C27/54 主分类号 B64C27/635
代理机构 Wenderoth, Lind & Ponack, L.L.P. 代理人 Wenderoth, Lind & Ponack, L.L.P.
主权项 1. A helicopter rotor comprising: a blade; a rotor hub which supports said blade; and a lead-lag angle mechanism configured to change a lead-lag angle of said blade in synchronization with rotation of said rotor hub such that a lag angle is given to said blade on a first side of a helicopter movement direction, on which first side said blade is rotating in the movement direction, and a lead angle is given to said blade on a second side of the movement direction of said helicopter, on which second side said blade is rotating opposite to the movement direction, wherein: said blade comprises a spar having a spar tip-side portion and a spar hub-side portion hinged to each other by a lead-lag hinge; said lead-lag angle mechanism comprises a link mechanism that causes said spar tip-side portion to pivot about said lead-lag hinge with respect to said spar hub-side portion to give said blade the lag angle on the first side of the helicopter movement direction and the lead angle on the second side of the helicopter movement direction in synchronization with rotation of said rotor hub and in dependence upon a rotational position of said blade with respect to the helicopter movement direction; said blade includes a blade hub side portion positioned on a rotor hub side with respect to said lead-lag hinge; said spar hub side portion is arranged inside said blade hub side portion; said blade hub side portion includes a first rail; and said spar hub side portion includes a first roller which engage said first rail.
地址 Tokyo JP