The invention discloses a complete machine parachute device which comprises a main parachute, a canopy sleeve, a traction rocket and a rocket slow descent parachute, and the canopy sleeve is in a long strip shape and is provided with a containing cavity used for containing the main parachute; parachute ropes of the rocket slow descending parachute are connected to one end of the parachute canopy sleeve, and the traction rocket is connected with a parachute fabric of the rocket slow descending parachute. The main parachute, the canopy sleeve, the traction rocket and the rocket slow descent parachute are arranged in a mounting cavity of the aircraft, and the traction rocket is used for pulling the canopy sleeve out of the aircraft from the mounting cavity; a first turning cover and a first elastic ferrule are arranged on the canopy sleeve; and a first air hole is formed in the first turning cover. The safety of personnel can be guaranteed, meanwhile, it can be guaranteed that the main parachute is rapidly and smoothly unfolded, and therefore the use safety can be improved.

    本发明公开了一种整机降落伞装置,包括主降落伞、伞衣套、牵引火箭以及火箭缓降降落伞,所述伞衣套为长条形,并设置有用于供主降落伞容纳的容纳腔;所述火箭缓降降落伞的伞绳连接于所述伞衣套的一端,所述牵引火箭与所述火箭缓降降落伞伞面相连;所述主降落伞、伞衣套、牵引火箭、火箭缓降降落伞设置于飞机的安装腔内,所述牵引火箭用于将伞衣套从安装腔牵引至飞机外;所述伞衣套上设置有第一翻盖、以及第一弹性套圈;所述第一翻盖上设置有第一气孔。本发明可保障人员安全的同时,并可确保主降落伞快速、顺利展开,从而可提高使用安全性。


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    Title :

    Complete machine parachute device


    Additional title:

    一种整机降落伞装置


    Contributors:
    XIE QIHAO (author) / ZHANG CAIXIA (author) / WANG CAIYI (author)

    Publication date :

    2023-11-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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