Patent ID: 7971826

Claim:
An aircraft engine assembly comprising: an engine; an engine suspension pylon, the pylon comprising a rigid structure comprising a box and a mounting system inserted between the engine and the rigid structure, the mounting system comprising an aft engine suspension; and a heat exchanger system comprising an exchanger to which a hot fluid inlet, a cold air inlet, a first outlet communicating with the hot fluid inlet, and at least one second outlet communicating with the cold air inlet are connected, each second outlet from the heat exchanger system being located between the box and the engine; wherein each second outlet is located aft from the aft engine suspension; and wherein the rigid structure of the suspension pylon further comprises a structural block fixed on the box between the box and the engine, the structural block comprising an attachment interface of the aft engine suspension, the second outlet from the heat exchanger system being provided on a second outlet pipe connected to the exchanger and passing through the structural block.