The invention relates to an engine attachment system for an aircraft and a method for attaching an engine. The engine attachment system includes a strut box. The strut box includes a longitudinal axis, a forward portion extending along the longitudinal axis, and a rearward portion extending from the forward portion along the longitudinal axis. The engine attachment system includes a front attachment device coupled to a front portion of the strut box and coupleable to a front spar of the wing. The engine attachment system includes a rear attachment device coupled to a rear portion of the strut box and coupleable to a rear spar of the wing. The rear portion of the strut box is positioned below the wing when the strut box is coupled to the wing by the front and rear attachment means. The strut box may be coupled to the engine.

    本发明涉及用于飞机的发动机附接系统和用于附接发动机的方法。发动机附接系统包括支柱箱。支柱箱包括纵向轴线、沿纵向轴线延伸的前部和沿纵向轴线从前部延伸的后部。发动机附接系统包括联接到支柱箱的前部并且可联接到机翼的前翼梁的前附接装置。发动机附接系统包括联接到支柱箱的后部并且可联接到机翼的后翼梁的后附接装置。当支柱箱通过前附接装置和后附接装置联接到机翼时,支柱箱的后部定位在机翼下方。支柱箱可联接到发动机。


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    Titel :

    ENGINE ATTACHMENT SYSTEM FOR AIRCRAFT AND METHOD FOR ATTACHING AN ENGINE


    Weitere Titelangaben:

    用于飞机的发动机附接系统和用于附接发动机的方法


    Beteiligte:
    L D TORKINSON (Autor:in) / POWELL DANIEL THOMAS (Autor:in) / SCHAEFER KURT K (Autor:in) / PALMA DARIO (Autor:in) / STEVENS KERRY (Autor:in)

    Erscheinungsdatum :

    2023-10-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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