公开(公告)号：US08844880B1

公开(公告)日：2014-09-30

申请号：US13199671

申请日：2011-09-07

申请人： McGregor Lee Corliss

发明人： McGregor Lee Corliss

IPC分类号： B64C27/56 ,  B64C13/04

CPC分类号： B64C27/32 ,  B64C13/12 ,  B64C27/025 ,  B64C27/18 ,  B64C27/26 ,  B64C27/48 ,  B64C27/56 ,  B64C27/605 ,  B64C27/72 ,  B64C2027/4736 ,  B64D31/04 ,  F16C33/667 ,  Y10T74/20612

摘要： A heliplane operates with a fixed wing at high velocities, and particularly at high advance ratios, while using a rotary wing maintained in motion at all speeds. At high advance ratios, the rotor wing eventually may be rotated primarily to maintain its stability, rather than depending upon the majority of lift. Meanwhile, a collective pitch control is provided and located between pilot and copilot. A single control provides control of both collective pitch and throttle by both pilots. One pilot will have to operate the control with the left hand, while the other may use their right hand. Nevertheless, both throttles push away from the pilot, regardless of which one is in control of the aircraft, while a single collective lever is relied upon.

摘要翻译： 一个直升机以高速度，特别是高进给速率的固定机翼操作，同时使用在所有速度下保持运动的旋翼。 在高提前比例下，转子翼最终可以主要旋转以保持其稳定性，而不是依赖于大部分升力。 同时，提供集体俯仰控制，位于飞行员和副驾驶之间。 单个控制提供两个飞行员对集体俯仰和油门的控制。 一名飞行员必须用左手操纵控制，而另一名可以使用右手。 尽管如此，无论是哪一个控制着飞机，两个节流阀都从飞行员上推，而依靠单一的集体杠杆。