An integrated pylon structure for a propulsion system is suitable for one end to be connected to an aircraft wing and the other end to be connected to an aircraft engine. The pylon structure includes a pylon box section (110) formed from an upper and a lower bean, a frame (100) and a side wall panel. The pylon structure has a thrust reverser hood connection structure, provided on the side wall and connected with a nacelle thrust reverser hood having a front fixed hood (301) and a rear movable hood (302). A guide rail allows the rear movable hood to slide and open relative to the pylon box section. The engine thrust reverser hood is directly connected to the side wall of the pylon box section and a guide rail on the side wall guides the opening of the thrust reverser hood.


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    Titel :

    Integrated pylon structure for propulsion system


    Beteiligte:
    WU GUANGHUI (Autor:in) / HAN KECEN (Autor:in) / ZHOU LIANGDAO (Autor:in) / YU QIFENG (Autor:in) / LIN GUOZHENG (Autor:in) / ZHANG HONGJIE (Autor:in) / ZHANG SHIBIAO (Autor:in) / WENG HAOJIE (Autor:in) / GUO HAISHA (Autor:in) / ZHANG PENGFEI (Autor:in)

    Erscheinungsdatum :

    2018-01-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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