The present invention relates to a paraglider with improved flight stability. According to an embodiment of the present invention, disclosed is the paraglider with improved flight stability in which a left main suspension line connected to a left riser distributes and transmits a load generated on a right side of a canopy, and as a right main suspension line connected to a right riser distributes and receives the load generated on the left side of the canopy, force is evenly distributed to left and right sides during riser-up for take-off, and deformation that occurs in the canopy is reduced when rotating left and right during flight. The paraglider includes a canopy, a harness, multiple lines, multiple left risers and right risers, and left and right control lines.

    본 발명은 비행 안정감이 향상된 패러글라이더에 관한 것이다. 본 발명의 실시예에 따르면, 좌측 라이저에 연결되는 좌측 메인 산줄이 캐노피의 우측부에 발생된 하중을 분산하여 전달받고 우측 라이저에 연결되는 우측 메인 산줄이 캐노피의 좌측부에 발생된 하중을 분산하여 전달받도록 구성됨으로써, 이륙을 위한 라이저업 시에 좌우측으로 균등하게 힘을 분산시키고, 비행 중에 좌우 방향으로 회전 시에 캐노피에 발생하는 변형을 저감하도록 하는 비행 안정감이 향상된 패러글라이더가 개시된다.


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    Titel :

    Paraglider with improved flight stability


    Weitere Titelangaben:

    비행 안정감이 향상된 패러글라이더


    Beteiligte:
    LEE JIHUN (Autor:in)

    Erscheinungsdatum :

    12.05.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

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



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