The invention relates to a front engine attachment system (150) for an engine (102), having: an engine pylon (104) having a nose (110) with a male collet (111) and a cylindrical post; two links (162a-162b) fastened to the engine (102) about a second axis (12) by means of a second ball joint connection; a first shaft (165) establishing a first spherical joint connection of the link (162a-b) around the first axis (10) to the male collet piece (111), where the first axis (10) and the second axis (12) are in the same vertical plane, and where the cylindrical column is mounted so as to be movable relative to the front housing (103) via an annular linear connection. Such a front engine attachment system has a reduced vertical volume because the front engine attachment is incorporated in the engine pylon.

    本发明涉及一种用于发动机(102)的前发动机附接件系统(150),其具有:发动机挂架(104),该发动机挂架具有鼻部(110),该鼻部具有阳夹头件(111)和圆柱形柱;两个联结件(162a‑162b),它们通过第二球形接头连接部绕第二轴线(12)紧固到发动机(102);第一轴(165),其建立绕第一轴线(10)的联结件(162a‑b)到阳夹头件(111)的第一球形接头连接部,其中,第一轴线(10)和第二轴线(12)在同一竖直平面中,并且其中,圆柱形柱安装成能够经由环形线性连接部相对于前壳体(103)运动。这种前发动机附接件系统具有减小的竖直体积,因为前发动机附接件结合在发动机挂架中。


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    Titel :

    Front engine attachment system intended for aircraft engine and having compact structure


    Weitere Titelangaben:

    拟用于飞行器发动机并具有紧凑结构的前发动机附接件系统


    Beteiligte:

    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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