The invention discloses a gyro type rotary stability augmentation air refueling taper sleeve, which relates to the technical field of air refueling, and is characterized in that the refueling taper sleeve comprises a refueling hose connected with a refueling machine and a taper sleeve joint connected to the end part of the refueling hose, and an oil transportation channel is arranged on the taper sleeve joint in a penetrating manner; an air flow cover and a mass block located in the air flow cover are wrapped outside the oil conveying channel, an air inlet and an air outlet are formed in the air flow cover, the mass block is rotationally connected to the oil conveying channel through a bearing, a plurality of blades are distributed on the mass block in the circumferential direction, the end of the oil conveying channel is connected with an umbrella rib located outside the air flow cover, and the umbrella rib is connected with the air flow cover. And the umbrella ribs are coated with an umbrella canopy. According to the gyro type rotary stability augmentation air refueling taper sleeve, the phenomena of irregular swinging and rotation of a hose taper sleeve system in the air refueling butt joint process can be restrained, the efficiency and progress of taper sleeve butt joint are improved, and accidents are reduced.

    本发明公开了一种陀螺式旋转增稳空中加油锥套,涉及空中加油技术领域,其技术方案要点是:所述加油锥套包括与加油机连接的加油软管和连接在加油软管端部的锥套接头,所述锥套接头上穿设有输油通道,所述输油通道外包覆有气流罩和位于气流罩内的质量块,所述气流罩上开设有进气口和出气口,所述质量块通过轴承转动连接在输油通道上,所述质量块上周向分布有多个叶片,所述输油通道的端部连接有位于气流罩外的伞骨,所述伞骨外包覆有伞衣。该陀螺式旋转增稳空中加油锥套可以抑制空中加油对接过程中软管锥套系统出现的无规则飘摆和旋转现象,提高锥套对接的效率和进度,减少意外事故的发生。


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    Titel :

    Gyroscope type rotary stability augmentation air refueling taper sleeve


    Weitere Titelangaben:

    一种陀螺式旋转增稳空中加油锥套


    Beteiligte:
    HUANG JIANGTAO (Autor:in) / CHEN QISHENG (Autor:in) / SHAN ENGUANG (Autor:in) / WANG CHUNYANG (Autor:in) / TAN XIAO (Autor:in) / ZHU ZHE (Autor:in) / TANG JIGANG (Autor:in) / HU BIN (Autor:in) / WANG YINZHU (Autor:in) / DU XIN (Autor:in)

    Erscheinungsdatum :

    2023-03-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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