System for attaching an engine to the structure of an aircraft, such as a sail wing aircraft

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.

2. The attachment system according to claim 1 , wherein the angle of inclination of an axis of the shaft is about 45° relative to the Y direction and about 45° relative to the Z direction.

3. The attachment system according to one of claims 1 or 2 , further comprising:

at least one rear engine attachment point which bears the forces along the Y direction and along the Z direction.

4. The attachment system according to one of claims 1 or 2 , wherein a rear fastening is made up of two radial rods at about 45°, which are symmetrical in relation to a vertical plane passing through the longitudinal axis of the engine.

5. The attachment system according to one of claims 1 or 2 , further comprising:

a left-hand fixing swivel joint and a right-hand fixing swivel joint, each mounted externally on a flange which is firmly fixed to the engine housing, where each swivel joint is internally fitted on the shaft which is inclined relative to the Y direction and to the Z direction, where the shaft is firmly fixed on the first frame.

6. The attachment system according to one of claims 1 or 2 , further comprising:

an attachment point fitted with free play and which is designed to bear the engine forces in the event of failure of any of the principal engine attachment points.

7. The attachment system according to one of claims 1 or 2 , wherein the aircraft is a sail wing aircraft.

8. The attachment system according to one of claims 1 or 2 , wherein a longitudinal axis of the engine is disposed between the upper beam and a wing surface of the aircraft.

9. 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, wherein the top portion of the first frame is opposite the bottom portion of the first frame;

a second frame disposed aft of the first frame, the second frame firmly fixed to a median part of the upper beam;

at least one fastening firmly fixed to the first frame, the at least one fastening including a first aperture therethrough;

at least one flange firmly fixed to an engine housing, the at least one flange including a second aperture therethrough; and

at least one shaft disposed through the first aperture and the second aperture,

wherein the shaft is inclined relative to a transverse axis of the engine and a vertical axis of the engine so as to bear forces in a longitudinal direction of the engine and bear forces inclined relative to the transverse axis of the engine and the vertical axis of the engine.

10. The attachment system of claim 9 , further comprising:

at least one swivel joint including a third aperture therethrough, the at least one shaft disposed through the third aperture.

11. The attachment system of claim 9 , wherein the at least one shaft comprises a solid shaft and a tubular shaft, the solid shaft disposed through an inner diameter of the tubular shaft.

12. The attachment system of claim 9 , further comprising:

at least one ring disposed on the at least one shaft, thereby retaining the shaft in the first aperture and the second aperture, and thereby fastening the at least one fastening to the at least one flange.