公开(公告)号：US20150246725A1

公开(公告)日：2015-09-03

申请号：US14308326

申请日：2014-06-18

申请人： Nolan Joseph Reilly

发明人： Nolan Joseph Reilly

IPC分类号： B64C27/605 ,  B64C11/32

CPC分类号： B64C27/605 ,  B64C11/32 ,  B64C15/02 ,  B64C27/24 ,  B64C27/82 ,  B64C2027/8236 ,  B64C2027/8245

摘要： A method of aircraft propulsion and control more specific to rotorcraft propulsion and control using forward, neutral and aft thrust in addition to forward/aft thrust coupling from the propulsive tail assembly through cyclic and collective pitch of the non-flapping, ridged propeller/fan blades and/or from a turbojet/turbofan vectored thrust system. The cyclic blade pitch induces a drive shaft bending moment that is used to provide aircraft directional control and also provides anti-torque control for a single rotor head helicopter. The forward/reverse collective thrust actuator, phase lag elevator effect cyclic actuator and phase lag rudder/anti-torque effect cyclic actuator do not require complex control mixing. The vectored thrust system also provides aircraft directional control and anti-torque control individually or combined with the propeller/fan assembly. This assembly eliminates the requirement of rudder or elevator control on a fixed wing aircraft and the requirement of a tail rotor on a conventional helicopter while increasing speed and maneuverability. A slowed or stopped ridged X-wing rotorcraft hub with a modified circular arc airfoil would not require cyclic/collective control.

摘要翻译： 一种飞行器推进和控制的方法，其特别是旋翼航空器的推进和控制，除了从推进尾部组件通过非颤动，脊状螺旋桨/风扇叶片的循环和集合间距之外，使用前进，中立和后推力 和/或来自涡轮喷气发动机/涡轮风扇向量推力系统。 循环叶片间距引起用于提供飞行器方向控制的驱动轴弯矩，并且还为单个转子头直升机提供抗扭矩控制。 前进/后退集体推力执行器，相位滞后电梯效应循环执行器和相滞后舵/反转矩效应循环执行器不需要复杂的控制混合。 向量推力系统还单独提供飞机方向控制和抗扭矩控制，或与螺旋桨/风扇组件组合。 该组件消除了对固定翼飞机上的方向舵或电梯控制的要求以及在常规直升机上的尾部转子的要求，同时提高了速度和机动性。 具有改进的圆弧翼型的减速或停止的脊状X翼旋翼航空器轮毂不需要循环/集体控制。