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IMPROVED MEANS FOR TRANSMITTING EFFORTS, AGENCY BETWEEN AN AIRCRAFT ENGINE AND ITS ATTACHING MATERIAL

机译:飞机发动机及其连接材料之间的传递力,传递力的改进方法

摘要

In order to impart to the flexibility with a means of transmission of forces which are intended to be interposed between an aircraft engine and an attachment strut, while allowing it to transmit the loads that are extremely high, the invention relates to a terminal part (100) of this transmission means, including: - a second member for the passage of the forces (46), forming a second force path; - a first member of the passage of the forces (52, 52 ′), more flexible than the second and forming a first path of the forces (50b) and comprising a wall (52a) in the form of an arc; - an axis of the transmission of forces (60) integrated in the first path of the forces (50b) and passing through the second member (46) with a set of passage (66) so as to be integrated into the second path of the forces only when a deformation of the wall in the form of an arc (52a) is sufficient to take up the clearance of the passage (66).
机译:为了通过旨在被施加在飞机发动机和附接支柱之间的力的传递手段来赋予灵活性,同时允许其传递极高的载荷,本发明涉及一种终端部分(100 ),该传动装置包括:-用于使力(46)通过的第二构件,形成第二力路径; -力(52、52')通过的第一构件,比第二个构件更柔韧并且形成力(50b)的第一路径,并包括呈弧形的壁(52a); -整合在力(50b)的第一路径中并通过一组通道(66)穿过第二构件(46)的力(60)的传输轴,以便整合到第二力(50b)的第二路径中仅当壁的弧形变形(52a)足以占据通道(66)的间隙时,才施加力。

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