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    • 1. 发明申请
    • AIRCRAFT WITH A CONTROL DEVICE
    • 具有控制装置的飞机
    • US20130035808A1
    • 2013-02-07
    • US13525282
    • 2012-06-16
    • Burkhard GÖLLINGFrank HAUCKEMatthias BAUERWolfgang NITSCHEInken PELTZER
    • Burkhard GÖLLINGFrank HAUCKEMatthias BAUERWolfgang NITSCHEInken PELTZER
    • B64C13/16B64C9/00B64C21/00B64C13/24
    • B64C23/005B64C9/16B64C9/38B64C13/18B64C21/04B64C29/0025Y02T50/166
    • An aircraft with aerofoils including a main wing and a control flap that includes an adjustment flap. The aircraft includes an actuator for the control flap, as well as a sensor device for acquiring the position of the control flap, an arrangement of flow-influencing devices for influencing the fluid that flows over a segment of the main wing, and flow-state sensor devices for measuring the flow state. The aircraft includes a flight control device connected to the sensor device for acquiring the position of the control flap and to the flow-state sensor devices, and connected to the actuator and flow-influencing devices for transmitting actuating commands, and a flight-state sensor device connected to the flight control device for transmitting flight states. The flight control device includes a function that selects the flow-influencing devices that are operated for optimising local lift coefficients on the aerofoil, depending on the flight state.
    • 具有机翼的飞机包括主翼和包括调节翼片的控制翼片。 飞机包括用于控制翼片的致动器,以及用于获取控制翼片的位置的传感器装置,用于影响流过主翼片段的流体的流动影响装置的布置,以及流动状态 用于测量流动状态的传感器装置。 飞机包括连接到传感器装置的飞行控制装置,用于获取控制翼片和流动状态传感器装置的位置,并连接到用于传送致动指令的致动器和流量影响装置,以及飞行状态传感器 连接到飞行控制装置的装置用于传送飞行状态。 飞行控制装置包括根据飞行状态选择用于优化机翼上的局部升力系数的流量影响装置的功能。