The invention discloses a soft air refueling and oil receiving device capable of relieving butt joint impact. The soft air refueling and oil receiving device comprises an oil receiving conical head, a butt joint hose, an oil conveying pipe and an oil tank. The oil receiving conical head is inserted into an oil filling conical sleeve of an oil receiving aircraft; the oil receiving conical head is connected with the oil conveying pipe through a butt joint hose; the oil conveying pipe communicates with the oil tank; a connecting rod transmission assembly is mounted on the oil receiving conical head and the oil conveying pipe; the connecting rod transmission assembly is in transmission connection with the driving assembly; the driving assembly is fixedly installed on a side wing of the oiling machine. Through matched adjustment of the connecting rod transmission assembly and the driving assembly, the oil receiving conical head generates a buffering effect at the too high butt joint speed, the impact speed of the oil receiving conical head on the oil filling conical pipe is reduced, the whipping phenomenon caused by excessive looseness of the conical pipe is avoided, and meanwhile, in order to ensure that the oil receiving device can be in normal butt joint and has certain rigidity, the oil receiving device is not prone to falling off. Within a certain range, the oil receiving device ensures that impact force can push open a valve on the oil filling taper pipe to achieve air oil filling.

    本发明公开一种减缓对接冲击的软式空中加油受油装置,包括:受油锥头,对接软管,输油管和油箱;受油锥头插入受油飞机的加油锥套内;受油锥头通过对接软管与输油管相连接;输油管与油箱连通;受油锥头和输油管上安装有连杆传动组件;连杆传动组件与驱动组件传动连接;驱动组件固定安装于加油机的侧翼。本发明通过连杆传动组件与驱动组件的配合调节,使在过高对接速度下受油锥头产生缓冲效果,降低受油锥头对加油锥管的冲击速度,避免锥管过度松弛诱发鞭甩现象,同时为保证受油装置能进行正常对接,受油装置具有一定的刚度,在一定范围内受油装置保证冲击力能顶开加油锥管上的活门实现空中加油。


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    Titel :

    Soft air refueling and oil receiving device capable of relieving butt joint impact


    Weitere Titelangaben:

    一种减缓对接冲击的软式空中加油受油装置


    Beteiligte:
    ZHAO ZHENJUN (Autor:in) / TAN XINGYU (Autor:in) / ZHAO ZHANWEI (Autor:in) / SHI KUNKUN (Autor:in) / HOU XINGXING (Autor:in)

    Erscheinungsdatum :

    16.05.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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