Multi-flow turbojet-engine i.e. turbofan engine, suspension for airplane, has rear fixation unit with connection unit that fixes case and strut, where rear and front fixation units respectively transmit vertical/lateral and torque efforts

摘要

The suspension has a front fixation unit (10) fixing a multi-flow turbojet-engine i.e. turbofan engine, and an attachment strut of an aircraft i.e. airplane, where the strut is in the form of a rectangular sectioned case. A rear fixation unit (20) has a triangular connection unit (21) that fixes a multi-flow turbojet-engine case and the strut of the aircraft using a single attachment point. The unit (20) transmits vertical and lateral efforts, and the unit (10) transmits efforts related to torque around an axis of the engine.