The invention designs an autonomous maneuvering taper sleeve for soft aerial refueling. An aerial refueling taper sleeve is transformed, an aerodynamic principle at a high speed is utilized, and the stress condition of the taper sleeve is changed by changing the shape of an umbrella cover, so that the taper sleeve generates controllable movement within a certain range under the action of an aerodynamic force, and the applicability of the taper sleeve in different environments is improved; the taper sleeve can resist interference of complex airflow, the taper sleeve is kept at an ideal positionall the time in the refueling process stably, and the aerial refueling success rate is increased; and maneuvering of the taper sleeve within a certain range can be achieved, the refueling mode that the taper sleeve autonomously and flexibly finishes butt joint with an oil receiver aircraft is achieved, and a safer refueling mode is provided for aerial refueling.

    本发明设计一种用于软式空中加油的自主机动锥套,通过对空中加油锥套的改造,利用高速下的空气动力学原理,通过改变伞面形态,从而改变锥套的受力情况,使其在气动力的作用下产生一定范围内的可控运动,增加了锥套的在不同环境下的适用性;使锥套能够抵抗复杂气流的干扰,保持其加油过程中一直稳定在理想位置,增加了空中加油成功率;并且能够实现锥套在一定范围内的机动,实现锥套向受油机自主机动完成对接的加油方式,为空中加油提供了一种更安全的加油方式。


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    Titel :

    Autonomous maneuvering taper sleeve for soft aerial refueling


    Weitere Titelangaben:

    一种用于软式空中加油的自主机动锥套


    Beteiligte:
    MENG ZHONGJIE (Autor:in) / GUO GUANGGUANG (Autor:in) / HUANG PANFENG (Autor:in) / ZHANG YIZHAI (Autor:in)

    Erscheinungsdatum :

    02.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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