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
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