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公开(公告)号：US09776713B2
公开(公告)日：2017-10-03
申请号：US14602190
申请日：2015-01-21
CPC分类号： B64C27/025 , B64C27/02 , B64F1/04 , B64F1/16
摘要： Off-board gyrocopter take-off systems and associated methods are disclosed. A representative method includes restraining a gyrocopter from vertical and lateral movement, pre-rotating a fixed-pitch lift rotor of the gyrocopter via a power source located off the gyrocopter, and releasing the gyrocopter for vertical movement to allow the gyrocopter to lift under a force provided by the lift rotor. Optionally, the method can further include interrupting or reducing power from the power source to the gyrocopter as a way to release the gyrocopter for vertical movement.
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2.发明授权公开(公告)号：US09586679B2
公开(公告)日：2017-03-07
申请号：US14818105
申请日：2015-08-04
申请人： Karen Cupp
摘要： A helicopter main rotor control system includes a trunnion head mountable to a rotatable helicopter mast wherein the trunnion head has a control bar pivot supported by the trunnion head and pivotal about an axis substantially at a right angle to the helicopter mast. A control bar extends through the control bar pivot at a right angle thereto, and a pair of opposing leaf hinges are pivotal about the control bar and centered about said trunnion head. Each leaf hinge has a hinge plate extending from the control bar and defines a rotor blade mount hole therethrough.
摘要翻译： 直升机主转子控制系统包括可安装到可旋转的直升机桅杆的耳轴头，其中耳轴头具有由耳轴头支撑的控制杆枢轴，并且围绕基本上与直升机桅杆成直角的轴线枢转。 控制杆以与其成直角的方式延伸穿过控制杆枢轴，并且一对相对的叶片铰链围绕控制杆枢转并围绕所述耳轴头居中。 每个叶铰链具有从控制杆延伸的铰链板并且限定通过其中的转子叶片安装孔。
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3.发明授权Apparatus and method for roll moment equalization at high advance ratios for rotary wing aircraft 有权用于旋转翼飞机的高提前比例的滚动力矩均衡装置和方法公开(公告)号：US09205919B1
公开(公告)日：2015-12-08
申请号：US13999366
申请日：2014-02-13
CPC分类号： B64C27/615 , B64C27/025 , B64C27/18 , B64C27/26 , B64C27/30 , B64C27/57 , B64C27/58 , B64C2027/7261
摘要： A method for equalizing rolling moments at high advance ratios is disclosed including impelling an aircraft in a forward direction at an airspeed by means of a thrust source and rotating a rotor of the aircraft at an angular velocity with respect to the airspeed effective to cause a positive total lift on each blade due to air flow over the blades in the retreating direction when the blade is moving in the retreating direction. The rotor includes an even number of blades placed at equal angular intervals around the rotor hub. One or both of cyclic pitch and rotor angle of attack are adjusted such that a rolling moment of the retreating blade due to reverse air flow is between 0.3 and 0.7 times a rolling moment on the advancing blade due to lift.
摘要翻译： 公开了一种用于以高提前比率均衡滚动力矩的方法，包括通过推力源在空速下向前推动飞行器，并以相对于空速的角速度旋转飞机的转子，以有效地引起正向 当叶片沿退回方向移动时，由于叶片在退回方向上的空气流过，在每个叶片上的总升力。 转子包括在转子毂周围以相等的角度间隔放置的偶数个叶片。 调节循环桨距和转子迎角的一个或两个，使得由于反向气流而导致的后退叶片的滚动力矩由于提升而在前进叶片上的滚动力矩的0.3至0.7倍之间。
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公开(公告)号：US09079659B2
公开(公告)日：2015-07-14
申请号：US13427696
申请日：2012-03-22
CPC分类号： B64C27/48 , B64C7/00 , B64C27/025 , B64C27/32
摘要： A fairing system may be assembled about a rotor of a rotorcraft to present an aerodynamically quasi-static region that rotates in an airstream, as well as certain extensions that sweep through the airstream as the rotor hub passes through the air. A spherical interface between the extensions on the rotor hub fairing and the base or root portion of each blade fairing provides three degrees of freedom permitting lead-lag, flapping, and blade pitch pivoting in the blade, while still maintaining an aerodynamic profile that will minimize drag.
摘要翻译： 可以围绕旋翼航空器的转子组装整流罩系统，以呈现在气流中旋转的空气动力学准静态区域，以及当转子毂经过空气时扫过气流的某些延伸部分。 转子轮毂整流罩上的延伸部分与每个叶片整流罩的基部或根部之间的球形接口提供了三个自由度，允许在叶片中进行超前滞后，振动和叶片俯仰摆动，同时仍保持空气动力学特性将使 拖动。
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公开(公告)号：US20150142219A1
公开(公告)日：2015-05-21
申请号：US14288957
申请日：2014-05-28
IPC分类号： B64C27/02
CPC分类号： B64C27/027 , B64C27/025 , B64C27/18 , B64C27/26 , B64C27/82 , B64C2027/8272
摘要： Apparatus and methods for controlling yaw of a rotorcraft in the event of one or both of low airspeed and engine failure are disclosed. A yaw propulsion device, such as an air jet or a fan may be used. A pneumatic fan may be driven by compressed air released into a channel surrounding an outer portion of the fan. Power for the yaw propulsion device and other system may be provided by a hydraulic pump and/or generator engaging the rotor. Low speed yaw control may be provided by auxiliary rudders positioned within the stream tube of a prop. The auxiliary rudders may one or both of fold down and disengage from rudder controls when not in use. Apparatus for generating horizontal lift imbalance induced a tail boom positioned within the downwash of a rotor may also be used, including compressed air vents or lateral or trailing edge flaps.
摘要翻译： 公开了在低空速和发动机故障中的一个或两个情况下控制旋翼航空器的偏航的装置和方法。 可以使用偏航推进装置，例如空气喷射器或风扇。 气动风扇可以被释放到围绕风扇外部的通道的压缩空气驱动。 用于偏航推进装置和其它系统的动力可由与转子接合的液压泵和/或发电机提供。 低速偏航控制可以由位于支柱的流管内的辅助方向舵提供。 辅助方向舵可以在不使用时向下折叠并与方向舵控制器脱离。 用于产生水平升降机不平衡的装置也可以使用定位在转子的下冲液内的尾臂，包括压缩空气通风口或横向或后缘翼片。
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公开(公告)号：US09022313B2
公开(公告)日：2015-05-05
申请号：US13335541
申请日：2011-12-22
CPC分类号： B64C27/615 , B64C27/025 , B64C27/18 , B64C27/26 , B64C27/30 , B64C27/57 , B64C27/58 , B64C2027/7261
摘要： A method and apparatus for enabling high speed flight in a rotorcraft are disclosed. The method may include executing a flight with a rotorcraft. The flight may include a first portion and second portion ordered sequentially. During the first portion, the rotorcraft may be flown with the rotor exclusively in autorotation. Once sufficient airspeed is obtained, the flight may transition to the second portion. Wherein, substantially all of the weight of the rotorcraft may be supported by one or more fixed wing surfaces of the rotorcraft. Thus, during the second portion, the rotor may be completely unloaded. To keep the rotor stable by turning, the rotor may be powered during the second portion by an engine of the rotorcraft by way of a prerotation system.
摘要翻译： 公开了一种用于在旋翼航空器中实现高速飞行的方法和装置。 该方法可以包括执行具有旋翼航空器的飞行。 飞行可以包括顺序排列的第一部分和第二部分。 在第一部分期间，旋翼航空器可以独自在自转中与转子一起飞行。 一旦获得足够的空速，飞行可以转变到第二部分。 其中，旋翼航空器的基本上所有的重量可以由旋翼航空器的一个或多个固定翼面支撑。 因此，在第二部分期间，转子可以完全卸载。 为了通过转动来保持转子稳定，转子可以在第二部分期间由旋转飞机的发动机通过预旋转系统供电。
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7.发明授权Solid lubricated blade pitch control system for use within a compressed airstream of a reaction driven rotorcraft 有权固体润滑叶片桨距控制系统，用于反应驱动旋翼航空器的压缩空气流中公开(公告)号：US08991748B1
公开(公告)日：2015-03-31
申请号：US13373406
申请日：2011-11-14
IPC分类号： B64C27/605 , B64C27/18 , F16C33/10 , B64C27/02 , F16C33/66
CPC分类号： B64C27/605 , B64C27/025 , B64C27/18 , B64C27/32 , F16C33/1095 , F16C33/6696 , F16C2326/43
摘要： A rotor system is disclosed for a reactive drive rotary wing aircraft. Apparatus and methods are disclosed for maintaining the rigidity of the rotor and eliminating play between flight controls and the rotor by mounting swashplate actuators to a flange rigidly secured to the mast. Methods are disclosed for modulating the temperature of oil pumped over one or more of the mast bearing, swashplate bearing, and spindle bearing. The temperature of air passively or actively drawn through rotor may also be modulated to maintain bearing temperature within a predetermined range. Structures for reducing pressure losses and drag on components due to air flow through the rotor are also disclosed. A rotor facilitating thermal management by oil and air flow is also disclosed. Surfaces interfacing between the swashplate and the mast and between control rods and the swashplate or pitch horn may bear a solid lubricant layer.
摘要翻译： 公开了一种用于无功驱动旋翼飞机的转子系统。 公开了用于维持转子的刚性并且通过将斜盘致动器安装到刚性地固定到桅杆的凸缘上来消除飞行控制器和转子之间的作用的装置和方法。 公开了用于调节泵送在一个或多个桅杆轴承，斜盘轴承和主轴轴承上的油的温度的方法。 无源或主动地通过转子吸入的空气的温度也可被调制以将轴承温度保持在预定范围内。 还公开了用于减少由于通过转子的气流引起的部件上的压力损失和阻力的结构。 还公开了通过油和空气流促进热管理的转子。 在斜盘和桅杆之间以及控制杆和斜盘或桨距角之间的表面可以承载固体润滑剂层。
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8.发明申请AUTOMATIC PITCH CHANGE ROTARY WING ROTOR SYSTEM AND METHOD OF ROTOR CONTROL 审中-公开自动换刀转子转子转子系统及转子控制方法公开(公告)号：US20140263821A1
公开(公告)日：2014-09-18
申请号：US13836190
申请日：2013-03-15
申请人： Karen Cupp
IPC分类号： B64C27/57
摘要： A helicopter main rotor control system includes a trunnion head mountable to a rotatable helicopter mast wherein the trunnion head has a control bar pivot supported by the trunnion head and pivotal about an axis substantially at a right angle to the helicopter mast. A control bar extends through the control bar pivot at a right angle thereto, and a pair of opposing leaf hinges are pivotal about the control bar and centered about said trunnion head. Each leaf hinge has a hinge plate extending from the control bar and defines a rotor blade mount hole therethrough.
摘要翻译： 直升机主转子控制系统包括可安装到可旋转的直升机桅杆的耳轴头，其中耳轴头具有由耳轴头支撑的控制杆枢轴，并且围绕基本上与直升机桅杆成直角的轴线枢转。 控制杆以与其成直角的方式延伸穿过控制杆枢轴，并且一对相对的叶片铰链围绕控制杆枢转并围绕所述耳轴头居中。 每个叶铰链具有从控制杆延伸的铰链板并且限定通过其中的转子叶片安装孔。
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公开(公告)号：US08752786B2
公开(公告)日：2014-06-17
申请号：US13545904
申请日：2012-07-10
IPC分类号： B64C27/82
CPC分类号： B64C27/027 , B64C27/025 , B64C27/18 , B64C27/26 , B64C27/82 , B64C2027/8272
摘要： Apparatus and methods for controlling yaw of a rotorcraft in the event of one or both of low airspeed and engine failure are disclosed. A yaw propulsion device, such as an air jet or a fan may be used. A pneumatic fan may be driven by compressed air released into a channel surrounding an outer portion of the fan. Power for the yaw propulsion device and other system may be provided by a hydraulic pump and/or generator engaging the rotor. Low speed yaw control may be provided by auxiliary rudders positioned within the stream tube of a prop. The auxiliary rudders may one or both of fold down and disengage from rudder controls when not in use. Apparatus for generating horizontal lift imbalance induced a tail boom positioned within the downwash of a rotor may also be used, including compressed air vents or lateral or trailing edge flaps.
摘要翻译： 公开了在低空速和发动机故障中的一个或两个情况下控制旋翼航空器的偏航的装置和方法。 可以使用偏航推进装置，例如空气喷射器或风扇。 气动风扇可以被释放到围绕风扇外部的通道的压缩空气驱动。 用于偏航推进装置和其它系统的动力可由与转子接合的液压泵和/或发电机提供。 低速偏航控制可以由位于支柱的流管内的辅助方向舵提供。 辅助方向舵可以在不使用时向下折叠并与方向舵控制器脱离。 用于产生水平升降机不平衡的装置也可以使用定位在转子的下冲液内的尾臂，包括压缩空气通风口或横向或后缘翼片。
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公开(公告)号：US08690100B2
公开(公告)日：2014-04-08
申请号：US13393909
申请日：2010-09-02
申请人： Otmar Birkner
发明人： Otmar Birkner
IPC分类号： B64C27/00
CPC分类号： B64C27/025
摘要： A gyrocopter includes a motor, a rotor head and a torque transmission device for transmitting torque of the motor to the rotor head. The torque transmission device includes a pneumatic coupling.
摘要翻译： 陀螺仪包括马达，转子头和用于将马达的转矩传递到转子头的扭矩传递装置。 扭矩传递装置包括气动联轴器。
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