Disclosed is an integrated pylon structure for a propulsion system, wherein it 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 comprises a pylon box section (110) formed from an upper and a lower beam, a frame (100) and a side wall panel (102). The pylon structure further comprises a thrust reverser hood connection structure, provided on the side wall and connected with a nacelle thrust reverser hood comprising a front fixed hood (301) and a rear movable hood (302). The thrust reverser hood connection structure comprises at least one guide rail used for guiding the rear movable hood to make the rear movable hood 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 the opening of the thrust reverser hood is guided by means of the guide rail on the side wall, thus a guide rail beam is eliminated, which saves on space while meeting the installation requirements of an engine and reduces the weight of the entire propulsion system.


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    Title :

    INTEGRATED PYLON STRUCTURE FOR PROPULSION SYSTEM


    Additional title:

    INTEGRIERTE PYLONENSTRUKTUR FÜR ANTRIEBSSYSTEM
    STRUCTURE DE MÂT INTÉGRÉE POUR SYSTÈME DE PROPULSION


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

    Publication date :

    2018-01-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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