Intermediate casing for turbojet, has fixing ring for assembling intermediate casing with thrust reverser casing, where fixing ring includes radial annular leg, and heat exchanger is partly fixed to radial annular leg

摘要

The casing has a fixing ring (10) for assembling the intermediate casing with a thrust reverser casing. The fixing ring includes a radial annular leg (10b), where a heat exchanger (12) is partly fixed to the radial annular leg. The heat exchanger includes an axial upstream end and an axial downstream end, where the axial downstream end of the heat exchanger is fixed at the radial annular leg of the fixing ring. A locking strip (16) cooperates with the annular leg, where the axial downstream end of the heat exchanger is placed between the annular leg and the locking strip.