| 摘要 |
FIELD: aviation technique. ^ SUBSTANCE: the fastening assembly of an aviation engine of a flying vehicle has a pylon with a pair of lugs, a front and a back suspension brackets. One of them is fulfilled in the shape of a cross-arm hinged on the engine and hinged to the pair of lugs of the pylon. At that the assembly has a loading compensator fulfilled in the form of a rod hinged between one of the lug of the pylon and the cross-arm, and the hinged joints of the cross-arm with the lug of the pylon and with the rod of the loading compensator are made in the shape of ball and socket joints. ^ EFFECT: increases reliability, serviceable life and reduces the weight of the pylon-cross-arm system. ^ 5 dwg |
