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    • 4. 发明授权
    • Stabilizer
    • 稳定剂
    • US08622336B2
    • 2014-01-07
    • US13150790
    • 2011-06-01
    • Hanno BrennerChristoph KesslerWolfgang Kreitmair-Steck
    • Hanno BrennerChristoph KesslerWolfgang Kreitmair-Steck
    • B64C11/00
    • B64D1/22B64C27/04
    • A rotary aircraft which carries a hanging sling load on at least one support cable, benefits from a stabilizer which generates control signals R to be applied or modulated onto the flight control of the aircraft. At least one sling load pendulum motion detecting unit provides the stabilizer with data on the pendulum motion of the sling load. Additionally, the stabilizer is set up with a working range determination unit S3 for determining the space where free movement is possible in which the rotary aircraft with sling load can move without collision. The stabilizer generates control signals R in dependency of the determined pendulum motion of the sling load and the determined working range.
    • 在至少一个支撑电缆上承载吊吊负载的旋转飞机受益于产生要应用或调制到飞行器的飞行控制上的控制信号R的稳定器。 至少一个吊装载荷摆动运动检测单元为吊具提供有关吊索载荷的摆动运动的数据。 此外,稳定器设置有工作范围确定单元S3,用于确定具有悬挂载荷的旋转飞行器可以在没有碰撞的情况下移动的空间。 稳定器根据确定的吊架载荷的摆动和所确定的作业范围产生控制信号R.
    • 5. 发明授权
    • Helicopter rotor control system with individual blade control
    • 直升机转子控制系统,具有独立的叶片控制
    • US08201771B2
    • 2012-06-19
    • US12986664
    • 2011-01-07
    • Christoph KesslerDaniel Furst
    • Christoph KesslerDaniel Furst
    • B64C27/54
    • B64C27/001B64C2027/7216Y02T50/34
    • A method of controlling rotor pitch in a helicopter comprising the steps of: generating at least one blade dynamics signal representing at least one dynamic force acting on at least one of a rotor blade rotating assembly and a helicopter non-rotating assembly, the rotor blade rotating assembly including a plurality of rotor blades and a pitch actuator for each rotor blade; extracting information representing the at least one dynamic force; generating a dynamic force compensation output representing a compensation for at least a portion of the at least one dynamic force; receiving flight control signals directing flight of the helicopter from flight controls of the helicopter; generating from the flight control signals and the dynamic force compensation output a compensated pitch control signal for each blade of the rotor blade rotating assembly, and providing a compensated pitch control signal to compensate for a portion of the at least one dynamic force.
    • 一种在直升机中控制转子节距的方法,包括以下步骤:产生至少一个叶片动力学信号,其表示作用于至少一个转子叶片旋转组件和直升机非旋转组件中的至少一个的动力,转子叶片旋转 组件包括多个转子叶片和每个转子叶片的俯仰致动器; 提取表示所述至少一个动态力的信息; 产生表示对所述至少一个动态力的至少一部分的补偿的动态力补偿输出; 接收飞行控制信号,指挥直升机飞行从直升机的飞行控制; 从飞行控制信号产生并且动态力补偿输出用于转子叶片旋转组件的每个叶片的补偿俯仰控制信号,以及提供经补偿的桨距控制信号以补偿至少一个动态力的一部分。
    • 10. 发明申请
    • Stabilizer
    • 稳定剂
    • US20110303783A1
    • 2011-12-15
    • US13150790
    • 2011-06-01
    • Hanno BrennerChristoph KesslerWolfgang Kreitmair-Steck
    • Hanno BrennerChristoph KesslerWolfgang Kreitmair-Steck
    • G05D1/02B64C27/00G05D1/10
    • B64D1/22B64C27/04
    • The invention relates to a stabilizer for rotary wing aircraft 11 which carry a hanging sling load 12 in the direction of the ground on at least one support cable 13, and were the stabilizer is set up to generate control signals R to be applied or modulated onto the flight control of the rotorcraft 11 and set up with at least one sling load pendulum motion detecting unit 2 for detecting the pendulum motion 15, 21, 41 of the sling load 12. Additionally, the stabilizer is set up with a working range determination unit S3 for determining the space where free movement is possible in which a rotorcraft 11 with sling load 12 can move without collision and the stabilizer is set up to generate the control signals R in dependency of the determined pendulum motion 15, 31, 41 of the sling load 12 and in dependency of the of the determined working range.
    • 本发明涉及一种用于旋转飞行器11的稳定器,其在至少一个支撑缆索13上沿地面方向承载悬挂吊索12,并且设置稳定器以产生要施加或调制到 旋翼航空器11的飞行控制,并设置有至少一个吊索载荷摆动检测单元2,用于检测吊索载荷12的摆动运动15,21,41。另外,稳定器设置有工作范围确定单元 S3,用于确定具有悬挂负载12的旋翼航空器11可以在没有碰撞的情况下可自由运动的空间,并且稳定器被设置为根据确定的吊架运动15,31,41产生控制信号R. 负载12并依赖于确定的工作范围。