The invention discloses an active controllable stability augmentation taper sleeve for soft air refueling. The active controllable stability augmentation taper sleeve comprises an oil conveying pipe, a taper sleeve body, a stabilizing umbrella, an adjusting sleeve and a driving module. The adjusting sleeve can be freely expanded and shrunk, and the inner wall is a hollow cylinder with two open ends; the taper sleeve is sleeved with the adjusting sleeve, the stabilizing umbrella is arranged at the tail of the taper sleeve, and the taper sleeve is adjusted through the driving module to do eccentric motion. The adjusting sleeve is controlled to move eccentrically, large control force is generated, deflection decoupling of two degrees of freedom around the axis of the taper sleeve can be conducted at the same time, controllability and control force are greatly improved, disturbance force caused by the head wave effect in the air refueling process can be effectively resisted, and the stability of the device is improved. And the instability of a taper sleeve hose system caused by the head wave effect of an oil receiving head and moderate turbulence disturbance in the air refueling docking process is obviously improved.

    本发明公开了一种用于软式空中加油的主动可控增稳锥套,包括输油管、锥套、稳定伞、调整套和驱动模块;调整套能够自由扩大活缩小,内壁呈两端开口的空心圆柱体状;调整套套在锥套外,稳定伞设置在锥套尾部,通过驱动模块调整锥套进行偏心运动。本发明通过操控调整套偏心运动,产生很大的控制力,绕锥套轴线两个自由度的偏转解耦并且可以同时进行,大大的提高了可控性和控制力,能够有效抵抗空中加油过程中头波效应所引起的扰动力,对由空中加油对接过程中受油机头波效应和中度紊流扰动引起的锥套软管系统的不稳定有显著的改善。


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    Titel :

    Active controllable stability augmentation taper sleeve for soft air refueling


    Weitere Titelangaben:

    一种用于软式空中加油的主动可控增稳锥套


    Beteiligte:
    ZOU GUIYUN (Autor:in) / LIANG ZIFENG (Autor:in) / LIU XUEQIANG (Autor:in) / CHENG JIANGFENG (Autor:in)

    Erscheinungsdatum :

    04.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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