The invention relates to the technical field of aircraft landing platform manufacturing, in particular to a vibration correction type propeller aircraft self-gravity positioning landing platform. Comprising an aircraft and a parking platform, a landing positioning part is arranged at the bottom of the aircraft, a falling guiding concave part is arranged on the parking platform corresponding to the landing positioning part, a concave cavity of the falling guiding concave part is integrally in an inverted cone shape with an opening in the upper end, and a vibration generator is arranged on the parking platform; the system further comprises a detection control system. And when the aircraft lands on the parking platform and deviates from the preset positioning position, the detection control system sends a starting instruction to the vibration generator driver until the aircraft reaches the preset position. The situation that the aircraft cannot be positioned to the preset position after landing can be avoided.

    本发明涉及飞行器降落平台制造技术领域,具体涉及一种振动纠偏型螺旋桨飞行器自重力定位降落平台。包括飞行器和停机台,所述飞行器底部设有降落定位部,对应所述降落定位部,所述停机台上设有导落凹部,所述导落凹部的凹腔整体呈上端开口的倒置锥形,所述停机台上设有振动发生器;还包括检测控制系统;当所述飞行器降落在停机台上且偏离预设定位位置时,所述检测控制系统向所述振动发生器驱动器发出启动指令,直至所述飞行器到达预设位置。能够避免飞行器降落后无法定位至预设位置。


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    Titel :

    Vibration correction type propeller aircraft self-gravity positioning landing platform


    Weitere Titelangaben:

    一种振动纠偏型螺旋桨飞行器自重力定位降落平台


    Beteiligte:
    DU JIANAN (Autor:in) / CHENG LIANG (Autor:in) / YAN KAI (Autor:in) / DONG RUNRU (Autor:in)

    Erscheinungsdatum :

    2023-08-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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    Freier Zugriff


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    Caldwell, F.W. | Engineering Index Backfile | 1937


    Aircraft landing gear positioning concerning abnormal landing cases

    Lee, Hsing-Juin / Chiou, Cheng-Yi | AIAA | 1994