The present invention relates to a front engine attachment system for an engine of an aircraft and an aircraft, the front engine attachment system comprising: an engine boom (104) with a nose (110) having a main mother frame (111) and a cylindrical receptacle; a primary link (162) fixed to the engine (102) by a secondary articulated connection about a secondary axis (12a); a primary shaft (165) which enables a primary articulated connection of a primary link (162) in the primary mother frame (111) about a primary axis (10), the primary axis (10) and the secondary axis (12a) being on the same vertical plane; and an outer cylinder having a vertical axis, a first end of which is fixed in the cylindrical housing and a second end of which is mounted relative to the front cover (103) by an annular linear connection. The vertical volume of such a front engine attachment system is reduced as the front engine attachment is integrated to the engine boom.

    本发明涉及用于飞行器的发动机的前发动机附接系统及飞行器,该前发动机附接系统包括:发动机吊杆(104),该发动机吊杆(104)带有具有主母架(111)和圆柱形容置部的鼻部(110);主连杆(162),该主连杆(162)通过绕次轴线(12a)的次铰接连接固定至发动机(102);主轴(165),该主轴(165)实现绕主轴线(10)的在主母架(111)中的主连杆(162)的主铰接连接,其中,主轴线(10)和次轴线(12a)在同一竖直平面上;以及具有竖直轴线的外圆筒,其第一端部固定在圆柱形容置部中,并且其第二端部通过环形线性连接相对于前罩(103)安装。由于前发动机附接件集成至发动机吊杆,这样的前发动机附接系统的垂直体积减小。


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    Titel :

    Front engine attachment system for engine of aircraft and aircraft


    Weitere Titelangaben:

    用于飞行器的发动机的前发动机附接系统及飞行器


    Beteiligte:
    BERJOT MICHAEL (Autor:in) / LANCIO R ¨ (Autor:in) / MI (Autor:in)

    Erscheinungsdatum :

    31.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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