| 摘要 |
FIELD: engines and pumps.SUBSTANCE: invention relates to aircraft turbojet suspension assembly (3) including pylon (1) and bars (13a, 13b) to react the load from turbojet (3) connected with said pylon (1).EFFECT: assembly equipped with means (19, 25) separated from pylon (1) for heat isolation of bars (13a, 13b) from turbojet (3).9 cl, 8 dwg |
