The invention discloses a parachute and an aircraft, and relates to the technical field of aircrafts, the parachute comprises a top panel and a plurality of parachute arms, one ends of the plurality of parachute arms are connected around the top panel, gaps are formed between the adjacent parachute arms at intervals, and the parachute arms are provided with air guide channels with two open ends along the length direction of the parachute arms. A plurality of parachute arms of the parachute are all provided with air guide channels, and the air guide channels are arranged in the length directions of the parachute arms; in the parachute opening process, the parachute arm firstly extends out of the parachute pack, a part of airflow reaches the top panel position along the air guide channel to inflate the top panel, the parachute arm and the top panel are synchronously inflated, the parachute arm is not prone to overturning and knotting, and the parachute can be normally used after being unfolded.

    本发明公开了一种降落伞及飞行器,涉及飞行器技术领域,降落伞包括顶幅及多个伞臂,多个所述伞臂的一端围绕所述顶幅连接,相邻的所述伞臂间隔形成有缝隙,所述伞臂沿其长度方向设置有两端开口的导气通道。降落伞包括的多个伞臂均设置有导气通道,且导气通道沿着各自伞臂的长度方向设置;在开伞的过程中,伞臂先从伞包伸出,一部分气流顺着导气通道到达顶幅位置,给顶幅充气,使得伞臂和顶幅同步充气,伞臂不易翻转打结,降落伞在展开后能够正常使用。


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    Title :

    Parachute and aircraft


    Additional title:

    一种降落伞及飞行器


    Contributors:
    GONG SONGJIE (author) / ZHANG YUHANG (author) / ZHANG XU (author)

    Publication date :

    2024-10-25


    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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