首页> 外国专利> AIRCRAFT ENGINE ATTACHMENT COMPRISING INCLINED FIXING ELEMENTS, AIRCRAFT COMPRISING SAID ENGINE ATTACHMENT AND METHOD FOR FIXING AN ENGINE TO AN AIRCRAFT MATTING USING THE SAME

AIRCRAFT ENGINE ATTACHMENT COMPRISING INCLINED FIXING ELEMENTS, AIRCRAFT COMPRISING SAID ENGINE ATTACHMENT AND METHOD FOR FIXING AN ENGINE TO AN AIRCRAFT MATTING USING THE SAME

机译:包括倾斜固定元件的飞机发动机附件,包括所述常规引擎附件的飞机以及使用该模块将发动机固定到飞机垫上的方法

摘要

The invention relates to a motor attachment (50) configured to connect an engine and an aircraft mast (54), said engine attachment (50) comprising: - a first yoke (56) having two wings (72, 72 ') parallel to each other, - a connecting piece (52) positioned between the flanges (72, 72') of the first yoke (56) and connected to the first yoke (56) by a first connecting system (58) - fastening elements (80.1 to 80.4), connecting the first yoke (56) and the mast (54), including first and second fastening elements (80.1, 80.2) positioned between the flanges (72, 72 ') of the first yoke (56) which is inclined at an angle of between 10 and 45 ° so that it can be put in place and removed in the presence of the connecting piece (52) connected to the first yoke (56) by the first system link (58), the inclined fasteners having lateral forces. According to the invention, the connecting piece (52) and the first yoke (56) are connected by the first connecting system before the engine is fixed to the mast. The engine is attached to the mast by installing the fasteners (80.1 to 80.4).
机译:本发明涉及构造成连接发动机和飞机桅杆(54)的电动机附件(50),所述发动机附件(50)包括:-第一轭架(56),其具有平行于每个的两个翼(72、72')。其他,-连接件(52),位于第一轭(56)的凸缘(72、72')之间,并通过第一连接系统(58)连接到第一轭(56)-紧固元件(80.1至80.4) ),连接第一轭架(56)和桅杆(54),包括位于第一轭架(56)的凸缘(72,72')之间的第一和第二紧固元件(80.1,80.2),该第一和第二紧固元件以一定角度倾斜倾斜角在10°至45°之间,以便在存在通过第一系统连接件(58)连接到第一轭(56)的连接件(52)存在的情况下将其放置就位,并且倾斜紧固件具有侧向力。根据本发明,在将发动机固定在桅杆上之前,利用第一连接系统将连接片(52)和第一轭铁(56)连接。通过安装紧固件(80.1至80.4)将发动机固定在桅杆上。

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