The subject matter of the present invention is an aircraft propulsor assembly comprising a front engine attachment (60) comprising a cross beam (74) connected to the engine by converging first and second connecting rods (76, 82). The cross member (74) includes an upper extension (94) positioned at least partially facing a front transverse reinforcement (72) of the main structure (62) and connected to the main structure by at least one first coupling element (96), and a left or right extension (98, 100) positioned on either side of the upper extension (94), each side extension is connected to the first wing (102.1, 104.1) of the left or right corner member (98, 100) by at least one second fixing element (106), and the second wing (102.2, 10.4) of the left or right corner member (98, 100) is connected to the main structure (62) by at least a third coupling element (108).

    本发明的主题是一种飞行器推进器组件,其包括包含通过会聚的第一和第二连接杆(76、82)连接到发动机的横梁(74)的前发动机附接件(60)。该横梁(74)包括上延伸部(94),其至少部分地面对主结构(62)的前横向加强件(72)定位并且通过至少一个第一联接元件(96)连接到主结构,以及定位在上延伸部(94)的两侧的左侧或右侧延伸部(98、100),每个侧延伸部通过至少一个第二固定元件(106)连接到左或右角构件(98、100)的第一翼部(102.1、104.1),左或右角构件(98、100)的第二翼部(102.2、10.4)通过至少第三联接元件(108)连接到主结构(62)。


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    Title :

    Aircraft propeller assembly and aircraft comprising same


    Additional title:

    飞行器推进器组件及包括其的飞行器


    Contributors:
    GELIOT JEAN (author)

    Publication date :

    2022-12-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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