Patent ID: 8215580
Filing Date: 2012-07-10
Classification: B64D

Abstract:
1. A suspension for suspending a multi-flow turbojet engine provided with an intermediate casing and an exhaust casing from a pylon that can be attached to the structure of an aircraft, comprising: a forward attachment device attaching a hub of the intermediate casing to the pylon; a rear attachment device attaching the exhaust casing to the pylon; and a connection device rigidly connecting the intermediate casing to the pylon, wherein the rear attachment device includes an actuator which varies a vertical distance between the exhaust casing and the pylon to compensate for variations in diameter of the exhaust casing so as to keep an axis of the exhaust casing coaxial with an axis of the intermediate casing through the various phases of flight of the aircraft, a first end of the actuator is secured to the pylon and a second end of the actuator, movable relative to the first end in a vertical direction, is connected to the rear attachment device.