The invention belongs to the technical field of rotor aerodynamic design, and discloses a reversible hidden armed helicopter short wing. The short wing comprises a telescopic connecting beam, a transition section, a connecting shaft, a short wing body, a locking mechanism and a three-axis hydraulic electric cylinder. During normal training and cruising flight, the short wings are closed to be attached to the helicopter body to form a part of the helicopter body structure, and the helicopter is changed into a structure without short wings, is streamlined in appearance and is smooth and flat. When the helicopter enters a fighting mode, the locking mechanism is opened, the three-axis hydraulic electric cylinder enables the short wing of the helicopter to turn over upwards by 90 degrees aroundthe fixed shaft, and when the short wing is placed in the horizontal state of the helicopter body, weapon ammunition below the ammunition hanging hook can attack an enemy target under the control ofa pilot. And after the attack task is finished, the short wings are quickly folded and the helicopter quickly leaves the battlefield.

    本发明属于旋翼气动设计技术领域,公开了一种可翻转隐藏式武装直升机短翼。包括:可伸缩连接梁、过渡段、连接轴、短翼本体、锁闭机构、三轴液压电动缸;正常训练及巡航飞行时,将短翼闭合至与机身贴合,构成了机身结构的一部分,直升机变成了无短翼结构,外形呈流线型且光滑平整。当直升机进入战斗模式,打开锁闭机构,三轴液压电动缸将直升机短翼向上绕固定轴翻转90°,将短翼置于机身水平状态时,挂弹钩下方的武器弹药可通过飞行员的控制对敌方目标进行攻击。攻击任务结束后,快速收起短翼,迅速脱离战场。


    Access

    Download


    Export, share and cite



    Title :

    Reversible hidden armed helicopter short wing


    Additional title:

    一种可翻转隐藏式武装直升机短翼


    Contributors:
    LIU GUANG (author) / CHEN WEIXING (author) / WANG WENTAO (author) / CHEN YAOFENG (author) / CHEN HUAN (author)

    Publication date :

    2021-01-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    The Armed Forces Helicopter Repair Facility

    Emerald Group Publishing | 1978


    Novel helicopter stub wing and helicopter

    XU WEI / CHEN HONGYU / XU JINPENG et al. | European Patent Office | 2021

    Free access

    Project AIR87: Armed Reconnaissence helicopter HUMS Requirements

    Millar, M. / Harris, M. P. / Defence Science and Technology Organisation | British Library Conference Proceedings | 2001



    Wing-adjustment controlled helicopter

    YU DAICHUAN | European Patent Office | 2015

    Free access