The invention discloses a novel annular stable deceleration parachute. According to the novel annular stable deceleration parachute, an ellipsoidal parachute canopy after being sewed is adopted, the shape of the parachute canopy is ellipsoidal, one end of a topping rope is connected with a parachute top, the other end of the topping rope is connected with a parachute rope convergent point, and theparachute top is pulled down through the topping rope. By adoption of the scheme, the aerial stability of the stable brake parachute is improved, and the problems that paratroopers freely fall down for a long time and rotate automatically when the paratroopers jump high and open low during airborne landing can be solved.

    本发明公开了一种新型环状稳定减速伞,采用缝合后为椭球形的伞衣,伞衣的形状椭球形,牵顶绳一端连接伞顶,另一端与伞绳汇聚点相连,通过牵顶绳下拉伞顶。采用本发明的方案提高了稳定减速伞空中稳定性,可以解决伞兵空降高跳低开时,长时间自由坠落,伞兵自转的现象。


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    Titel :

    Novel annular stable brake parachute


    Weitere Titelangaben:

    新型环状稳定减速伞


    Beteiligte:
    SHAO CHAOJUN (Autor:in) / CHEN WU (Autor:in) / LI JUN (Autor:in) / HU SHOUWEN (Autor:in) / LYU ZHONG (Autor:in)

    Erscheinungsdatum :

    21.04.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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