According to an aircraft test flight tail wiping monitoring method, a tail wiping protection wheel is arranged on the rear side of the abdomen of an aircraft, an observation window is formed in the abdomen of the aircraft, a laser range finder and a camera are arranged in the observation window, and the laser range finder and the camera are connected with a test flight tail wiping monitor and a displayer; when the aircraft is in test flight, the laser range finder detects the distance between the belly of the aircraft and the ground to form a ranging signal and transmit the ranging signal to the test flight tail wiping monitor; the camera observes the relation between the tail wiping protection wheel and the ground for forming an image signal and transmits the image signal to the test fly tail wiping monitor; the tail wiping monitor calculates and processes the received ranging signals and the image signals to form state information of the abdomen of the airplane and the ground, and the state information is displayed through the displayer.

    一种飞机试飞擦尾监控方法,在飞机的腹部后侧设有擦尾保护轮,在飞机腹部设有观测窗,该观测窗内设有激光测距器和摄像头,激光测距器和摄像头与试飞擦尾监控器以及显示器连接;飞机试飞时,激光测距器探测飞机腹部与地面的距离,形成测距信号传输给试飞擦尾监控器;所述的摄像头观测擦尾保护轮与地面关系,形成影像信号传输给试飞擦尾监控器;擦尾监控器将收到的测距信号和影像信号进行计算处理形成飞机腹部与地面的状态信息,并将该状态信息通过显示器显示。


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    Title :

    Aircraft test flight tail wiping monitoring method


    Additional title:

    一种飞机试飞擦尾监控方法


    Contributors:
    LUO ZHIPENG (author) / SUN YI (author) / WANG QINGHUA (author) / HE WANG (author)

    Publication date :

    2021-09-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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