| 摘要 |
FIELD: aircraft engineering. ^ SUBSTANCE: engine assembly unit comprises turbojet engine, pylon and multiple engine attachment elements arranged between pylon and turbojet engine. In compliance with this invention, multiple engine suspension elements comprise element (6a) that takes up only those forces that act along turbojet engine crosswise axis (Y). Note here that said element (6a) comprises intermediate metal fastener (46) coupled with first metal fastener (40) attached to pylon with the help of two ball pins (48) arranged along vertical axis (Z), and pin (56) arranged along axis (X) and coupled with aforesaid intermediate metal fastener. Said pin is fitted with clearance along axis (X) on second metal fastener (58) jointed to turbojet engine. ^ EFFECT: optimum distribution of loads taking transmitted from turbojet engine to pylon structure. ^ 7 cl, 4 dwg |
