Patent ID: 8196859
Filing Date: 2012-06-12
Classification: B64C,B64D

Abstract:
1. A system for attaching an engine onto a structure of an aircraft comprising: an upper beam having a front end; a first frame disposed above a wing surface of the aircraft, the first frame having a bottom portion fitted to the structure of the aircraft, the front end of the upper beam firmly fixed to a top portion of the first frame; and a second frame disposed aft of the first frame, the second frame firmly fixed to a median part of the upper beam, wherein: the top portion of the first frame is opposite the bottom portion of the first frame, the engine is positioned beneath the upper beam, the system is orientated in relation to a longitudinal axis X, a transverse axis Y, and a vertical axis Z, two front engine attachment points are arranged symmetrically on either side of the vertical median plane of the engine, and said attachment points include a shaft which is inclined relative to the Y direction and to the Z direction so as to bear the forces along the longitudinal direction and forces inclined relative to the Z direction and the Y direction.