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    • 3. 发明申请
    • Electric Motor Powered Rotor Drive for Slowed Rotor Winged Aircraft
    • 用于减速转子翼型飞机的电动马达驱动转子驱动
    • US20130134264A1
    • 2013-05-30
    • US13445594
    • 2012-04-12
    • Jay W. Carter, JR.Jeffrey R. Lewis
    • Jay W. Carter, JR.Jeffrey R. Lewis
    • B64C27/22B64C9/00B64D35/00B64C27/26B64C27/28
    • B64C27/025B64D2027/026
    • A rotor aircraft has an engine, a propeller, wings, and a rotor. An electric motor is coupled to the rotor drive shaft for applying torque to the rotor drive shaft. The electric motor is sized to supply all of the torque to pre-rotate the rotor to a selected speed prior to liftoff of the aircraft. The wings are capable of providing substantially all of the lift required during forward flight at a cruise speed. The rotor being is capable of being trimmed to provide substantially zero lift and auto-rotate at cruise speed. Sensors sense flight conditions of the aircraft and provide signals to a controller that selectively causes the electric motor to cease applying torque to the rotor drive shaft during autorotation at cruise speed. The controller also causes the electric motor to apply torque to the rotor drive shaft if the sensors indicate additional rotor speed is needed.
    • 转子飞机有发动机,螺旋桨,机翼和转子。 电动机联接到转子驱动轴上以向转子驱动轴施加扭矩。 电动机的尺寸被设计成提供所有的扭矩以在飞机起飞之前将转子预旋转至选定的速度。 机翼能够以巡航速度提供在向前飞行期间所需的基本上所有的升力。 转子能够被修整以提供基本上的零升程并且以巡航速度自动旋转。 传感器感测飞行器的飞行状态,并向控制器提供信号,该控制器选择性地使电动机停止在巡航速度的自动转速期间向转子驱动轴施加扭矩。 如果传感器指示需要额外的转子速度,则控制器还使电动机向转子驱动轴施加扭矩。
    • 5. 发明授权
    • Automatic mechanical control of rotor blade collective pitch
    • 自动机械控制转子叶片集体间距
    • US07677492B1
    • 2010-03-16
    • US11280036
    • 2005-11-16
    • Jay W. Carter, Jr.Jeffrey R. Lewis
    • Jay W. Carter, Jr.Jeffrey R. Lewis
    • B64C27/00
    • B64C27/022B64C27/025
    • A rotary aircraft has a fuselage with wings and a rotor. The blades of the rotor are twistable about a pitch axis to vary collective pitch. A collective pitch shaft moves in an advancing direction to increase the collective pitch. Weights are mounted to the blades for outward movement along the blades in response to an increase in rotational speed of the blades. A linkage between each of the weights and the collective pitch shaft moves the collective pitch shaft in the advancing direction in response to an increase in rotational speed. A spring acting through a cam mechanism exerts a non linear force in opposition to the outward movement of the blades.
    • 旋转飞机具有机翼和转子的机身。 转子的叶片围绕俯仰轴线是可扭转的,以改变总体间距。 集体节距轴在前进方向上移动以增加集体节距。 响应于叶片的转速的增加,重量被安装到叶片上以沿叶片向外运动。 每个重物和集体节距轴之间的联动响应于转速的增加而使总倾斜轴沿前进方向移动。 通过凸轮机构作用的弹簧相对于叶片向外的运动产生非线性力。