Patent ID: 8141817
Filing Date: 2012-03-27
Classification: B64D

Abstract:
1. A turbojet suspended from an aircraft mast, the turbojet comprising the mast comprising a structural strut assembly of elongated shape, wherein said strut assembly is attached upstream rigidly to the outer shroud of the intermediate casing by a front attachment comprising a means for transmitting axial and lateral forces and downstream by a rear attachment to said exhaust casing, the front attachment of the strut assembly receives forces in an axial direction parallel to the axis XX, in a vertical direction which is perpendicular to the axial direction, in a transverse direction which is perpendicular to both the axial direction and the vertical direction, and receives a moment about the axial direction, and wherein the front attachment includes a horizontal plate in a plane defined by the axial and transverse directions which rests on a base secured to the outer shroud of the intermediate casing, a shear pin which extends in the vertical direction and transverses the plate and the base, and a pair of link rods in a V-shape, first ends of the link rods presenting an apex of the V-shape being attached by a fitting to the outer shroud of the intermediate casing.