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公开(公告)号：US20150314857A1
公开(公告)日：2015-11-05
申请号：US14701032
申请日：2015-04-30
发明人： Igor Cherepinsky , Harshad S. Sane
CPC分类号： B64C13/04 , B64C13/503 , B64C27/56 , B64D11/0689
摘要： A system and method for controlling a trajectory of a vehicle includes a crew seat with first and second inceptors mounted to a portion of the crew seat; a processor with memory having instructions stored thereon that cause the system to: receive signals indicative of a trajectory for the vehicle; receive signals indicative of a deviation in a trajectory of the vehicle; and transmit signals for controlling a flight path of the vehicle. A second inceptor is configured for selecting one or more menus on a user display and being configured to interact with a fly-by-wire control system for transmitting signals indicative of movement of flight surface of the vehicle. The crew seat is configured to be located on the vehicle, in a control station remotely located from the vehicle, or in a second vehicle remotely located from the vehicle.
摘要翻译： 用于控制车辆轨迹的系统和方法包括：乘员座椅，其具有安装在乘员座椅的一部分上的第一和第二受体; 具有存储器的存储器的处理器，其上存储有指令，其使得所述系统：接收指示所述车辆的轨迹的信号; 接收指示车辆轨迹偏离的信号; 并发送用于控制车辆的飞行路径的信号。 第二受体器被配置用于在用户显示器上选择一个或多个菜单，并且被配置为与用于传输指示车辆的飞行表面的运动的信号的线控飞控制系统交互。 船员座椅被配置为位于车辆上，远离车辆的控制站中，或位于远离车辆的第二车辆中。
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公开(公告)号：US09156546B2
公开(公告)日：2015-10-13
申请号：US12046356
申请日：2008-03-11
摘要： The system contains the active inceptor having mobility in a first direction. A feedback mechanism is in communication with the active inceptor. The mechanism provides a variable level of force to the active inceptor in the first direction. A programmable device communicates with the feedback mechanism. The programmable device controls the level of force provided to the active inceptor from the feedback mechanism. The programmable device is capable of recognizing and distinguishing between regimes wherein the operator is physically engaging the inceptor (“hands-on” state) and when the operator is “hands-off” the inceptor. The programmable device limits the maximum rate of displacement of an active inceptor to a specified safe and effective value regardless of changes in forces applied by the variable force feel feedback mechanism. The limit on rate of change of active inceptor position is varied based on the recognized “hands-on” or “hands-off” state and the type of tactile cue to satisfy otherwise conflicting requirements for failure robustness and effective tactile cueing during highly dynamic operations.
摘要翻译： 该系统包含在第一方向上具有迁移率的活性受体。 反馈机制与主动接收器通信。 该机制向第一方向的活动受体提供可变的力水平。 可编程设备与反馈机制通信。 可编程设备控制从反馈机制提供给主动接收器的力的水平。 可编程设备能够识别和区分操作者在物理上接合受体（“动手”状态）和操作者“接触”受体时的方式。 可编程设备将活动受体的最大位移速率限制在指定的安全有效值上，而不管由可变力感觉反馈机制施加的力的变化。 活动受体位置变化率的限制因识别的“动手”或“手动”状态以及触觉提示的类型而变化，以满足在高动态操作期间对故障鲁棒性和有效触觉提示的另外冲突的要求 。
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公开(公告)号：US09073631B1
公开(公告)日：2015-07-07
申请号：US13199678
申请日：2011-09-07
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 rotorcraft is disclosed. The rotorcraft may include an airframe, at least one engine connected to the airframe, and a rotor connected to the airframe. The rotor may include a hub, a rotor blade, and a feathering spindle connecting the rotor blade to the hub. The rotorcraft may further include a flow of oil passing proximate the feathering spindle. The flow of oil may cool the feathering spindle during take off and landing of the rotorcraft. Additionally, the flow of oil may heat the feathering spindle during travel of the rotorcraft at altitude.
摘要翻译： 公开了一种旋翼飞机。 旋翼航空器可以包括机身，连接到机身的至少一个发动机和连接到机身的转子。 转子可以包括轮毂，转子叶片和将转子叶片连接到轮毂的羽化主轴。 旋翼航空器还可以包括靠近羽化主轴的油流。 在旋转飞机起飞和着陆期间，油流可以冷却羽化主轴。 此外，油流可以在旋翼飞机高度行进期间加热羽化主轴。
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公开(公告)号：US09033284B2
公开(公告)日：2015-05-19
申请号：US13682165
申请日：2012-11-20
摘要： An inceptor is provided including a control stick mounted to a seat. The control stick is movable about at least a first axis. A fly-by-wire inceptor control system is housed within a portion of the seat. The inceptor control system is configured to provide input signal indicative of movement of the control stick to a flight control system.
摘要翻译： 提供了一种受体，包括安装在座椅上的控制棒。 控制杆可以围绕至少第一轴线移动。 线控式感应器控制系统容纳在座椅的一部分内。 所述受体控制系统被配置为提供指示所述控制棒向飞行控制系统的运动的输入信号。
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公开(公告)号：US08973863B1
公开(公告)日：2015-03-10
申请号：US13199705
申请日：2011-09-07
IPC分类号： B64C27/48 , B64C27/18 , B64C27/72 , B64C27/02 , B64C27/473
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： The rotorcraft may include an airframe, at least one engine connected to the airframe, and a rotor connected to the airframe. The rotor may include a hub, a rotor blade, and a feathering spindle connected to the hub. The rotor blade may have a root and a tip and form a conduit extending in the radial 5 direction from the root to the tip. The root may comprise a wall forming a hollow circular cylinder. The hollow circular cylinder may form a portion of the conduit. A plurality of bolts may be distributed circumferential within the wall of the root. The plurality of bolts may extend in the radial direction from the wall of the root to secure the rotor blade to the feathering 10 spindle.
摘要翻译： 旋翼航空器可以包括机身，连接到机身的至少一个发动机和连接到机身的转子。 转子可以包括轮毂，转子叶片和连接到轮毂的羽化主轴。 转子叶片可以具有根部和尖端并且形成从径向5方向从根部延伸到尖端的导管。 根部可以包括形成中空圆柱体的壁。 中空圆柱体可以形成导管的一部分。 多个螺栓可以在根部的壁内周向分布。 多个螺栓可以从根部的壁沿径向方向延伸，以将转子叶片固定到羽化10主轴上。
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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
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。
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57.发明申请CONTROL MEMBER PROVIDED WITH A BLADE COLLECTIVE PITCH LEVER AND YAW CONTROL MEANS, AND AN AIRCRAFT 有权控制构件用叶片集合式倾斜杆和伞形控制装置提供，以及飞机公开(公告)号：US20140263850A1
公开(公告)日：2014-09-18
申请号：US14165712
申请日：2014-01-28
申请人： AIRBUS HELICOPTERS
IPC分类号： B64C27/56
摘要： A control member (10) having a collective pitch lever (20) extending from a first end (21) to a second end (22). Said control member (10) has a handle (30) for controlling a yaw movement control device, said handle (30) being secured to an inner ring (40) that is guided to pivot about a second axis (AXLAC) by an outer ring (50) secured to said second end (22), said inner ring (40) being constrained to move together with said outer ring (50) and the lever (20) in pivoting about said first axis (AXCOL).
摘要翻译： 具有从第一端（21）延伸到第二端（22）的集体俯仰杆（20）的控制构件（10）。 所述控制构件（10）具有用于控制偏航运动控制装置的手柄（30），所述手柄（30）固定到内环（40），所述内环被引导以通过外环绕着第二轴线（AXLAC）枢转 （50）固定到所述第二端（22），所述内环（40）被限制为与所述外环（50）和所述杠杆（20）一起围绕所述第一轴线（AXCOL）枢转。
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58.发明授权Device for piloting a vehicle and method for the motorised assistance and control of such a piloting device 有权用于驾驶车辆的装置和用于机动辅助和控制这种驾驶装置的方法公开(公告)号：US08548651B2
公开(公告)日：2013-10-01
申请号：US12859819
申请日：2010-08-20
申请人： Cedric Antraygue
发明人： Cedric Antraygue
CPC分类号： B64C27/68 , B63H21/213 , B64C27/56
摘要： The invention relates to a piloting device comprising a piloting component (10) which is connected to at least one steering component (13), at least one force sensor (17) which measures the forces imparted into the kinematic chain (12) by said piloting component (10), a logic circuit (23) which is adapted to develop a speed reference signal according to a predetermined function of said force signals, and a circuit for controlling at least one parallel actuator (14) as regards speed.It extends to a method for the motorised assistance and control of a device of this kind and to an aircraft comprising a device of this kind.
摘要翻译： 本发明涉及一种引导装置，其包括连接到至少一个转向部件（13）的引导部件（10），至少一个力传感器（17），其通过所述引导来测量施加到运动链（12）中的力 组件（10），适于根据所述力信号的预定功能产生速度参考信号的逻辑电路（23），以及用于在速度方面控制至少一个并行致动器（14）的电路。 它涉及一种用于对这种装置的机动化辅助和控制的方法以及包括这种装置的飞机。
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公开(公告)号：US20130087660A1
公开(公告)日：2013-04-11
申请号：US13691927
申请日：2012-12-03
申请人： Eurocopter
IPC分类号： B64C27/68
摘要： A device for assisting the piloting of a rotorcraft, the rotorcraft having a flight control (10) for controlling a rotor (20, 21) via at least one linkage (35. An additional force is generated by at least one piloting assistance means (100) mechanically linked to the linkage (35. The additional force is a function of the position of the flight control (10) and of an instantaneous force as measured on the linkage (35).
摘要翻译： 一种用于辅助驾驶飞行器的驾驶的装置，旋翼飞机具有用于经由至少一个联动装置（35）控制转子（20,21）的飞行控制装置（10）。由至少一个引导辅助装置（100 ）与机构连接（35）。附加力是飞行控制器（10）的位置和在连杆机构（35）上测量的瞬时力的函数。
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60.发明授权Variable ratio crank for a manual flight control linkage of a rotary wing aircraft 有权用于旋翼飞机的手动飞行控制联动的可变比曲柄公开(公告)号：US08196857B2
公开(公告)日：2012-06-12
申请号：US12791216
申请日：2010-06-01
申请人： Bernard Gemmati , Romuald Biest , Carine Mirman
发明人： Bernard Gemmati , Romuald Biest , Carine Mirman
IPC分类号： B64C27/32
摘要： The present invention relates to a bellcrank (40) for a flight-attitude-changing linkage (27, 25A, 28A) of the variable gain type. The linkage (27, 25A, 28A) connects a manual flight control device of a rotary wing aircraft (1), e.g. a hybrid helicopter, to at least one airfoil of said aircraft (1) suitable for causing a change in flight attitude. Said bellcrank (40) includes first and second sliders (50, 52). Said first slider (50) is connected to a movable portion (57, 61) of a setpoint flight-attitude-changing linkage (24) that delivers a setpoint, with movements of said linkage causing the gain of said variable-gain linkage (27, 25A, 28A) to be adjusted, which gain is proportional to the position of said movable portion (57, 61).
摘要翻译： 本发明涉及一种用于可变增益型飞行姿态改变联动装置（27,25A，28A）的曲拐（40）。 连杆机构（27,2AA，28A）连接旋翼机（1）的手动飞行控制装置， 一种混合式直升机，适用于适于引起飞行姿态改变的所述飞机（1）的至少一个翼型。 所述曲拐（40）包括第一和第二滑块（50,52）。 所述第一滑块（50）连接到传递设定点的设定点飞行姿态改变联动装置（24）的可移动部分（57,61），所述联动装置的运动导致所述可变增益联动装置（27）的增益 ，25A，28A），该增益与所述可动部分（57,61）的位置成比例。
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