首页> 外国专利> Engine mounting structure for jet engine of aircraft, has rigid structure, whose back structure projects caisson toward back, and carries back wing attachment to retrieve exerting forces along vertical direction of mounting structure

Engine mounting structure for jet engine of aircraft, has rigid structure, whose back structure projects caisson toward back, and carries back wing attachment to retrieve exerting forces along vertical direction of mounting structure

机译:用于飞机的喷气发动机的发动机安装结构,具有刚性结构,其后部结构向后凸出沉箱,并进行后翼附接以沿安装结构的垂直方向恢复施加力

摘要

The mounting structure (4) has a rigid structure with a front longitudinal central caisson (22), and an anchoring unit for anchoring the structure (4) on a wing. The unit has a connection hinge (54) fixed to the caisson, and a back wing attachment located relative to lateral attachments. The structure has a back structure (21) with a transversal width reduced relative to that of the caisson, and projects the caisson towards the back. The back structure carries the back wing attachment to strictly retrieve exerting forces along a vertical direction of the mounting structure.
机译:安装结构(4)具有刚性结构,该刚性结构具有前纵向中央沉箱(22),以及用于将结构(4)锚固在机翼上的锚固单元。该单元具有固定至沉箱的连接铰链(54)和相对于侧向附件定位的后翼附件。该结构具有背面结构(21),该背面结构的横向宽度相对于沉箱的宽度减小,并将沉箱向后突出。背部结构带有后翼附件,可以严格地恢复沿安装结构垂直方向的作用力。

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