The invention relates to an aircraft pylon comprising a main structure (28) and a pipe section (44) having an internal duct (46) positioned inside at least one structural pipe (30, 32, 34) of the main structure (28). This solution makes it possible to reduce congestion outside the structural tubes of the main structure, making it easier to integrate other equipment into the pylon, and may help improve the aerodynamic performance of the pylon by reducing the cross-section of the pylon. The invention also relates to an aircraft comprising at least one such pylon.

    本发明涉及一种飞行器吊挂架,其包括主结构(28)和管段(44),所述管段具有定位在所述主结构(28)的至少一个结构管件(30,32,34)内部的内部管道(46)。这种解决方案使得可以减少所述主结构的结构管件外的拥挤,使得更容易将其他设备集成到所述吊挂架内,并且可以通过减小所述吊挂架的截面来帮助改善所述吊挂架的空气动力学性能。本发明还涉及一种包括至少一个这种吊挂架的飞行器。


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    Titel :

    Aircraft hanging frame and aircraft comprising same


    Weitere Titelangaben:

    飞行器吊挂架和包括其的飞行器


    Beteiligte:
    OLDE THEOPHILE (Autor:in) / CZAPRA LIONEL (Autor:in) / LABARTHE CHRISTOPHE (Autor:in)

    Erscheinungsdatum :

    2022-09-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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