| 摘要 |
The invention concerns an engine fastener of a mounting system designed to b e interposed between a rigid structure of an attachment strut of an aircraft engine and engine, the fastener comprising a main body (130), a control bar mounted articulating on the main body via a pivot bolt (144), as well as two thrust load absorbing link rods each provided with one end connected on the control bar, the main body consisting of a first main bracket (132a) and a second main bracket (132b) superimposed on the first. The invention is characterized in that the pivot bolt (144) consists of a first portion (144a ) and a second portion (144b), the first portion being made in one single piec e with the first bracket and the second portion being made in one single piece with the second bracket. Moreover, the brackets (132a, 132b) define an abutting surface (166) capable of limiting the rotation of the control bar (146). |
