Patent ID: 8366038

Claim:
A front attachment device for fastening a turbojet engine to an aircraft fixing strut, the attachment device being adapted to absorb turbojet engine thrust loads, wherein the attachment device comprises: a top bracket; a lower bracket; primary attachments operably coupling the top bracket to the lower bracket, each of the primary attachments presenting a primary attachment axis; and secondary attachments adapted to connect the lower bracket to the turbojet engine, each of the secondary attachments presenting a secondary attachment axis, wherein an absorbing thrust load vector extends along a longitudinal axis of the turbojet engine resulting from a first convergence point of primary vectors passing through the primary attachments coincident with the primary attachment axis, and a second convergence point of secondary vectors passing through the secondary attachments coincident with the secondary attachment axis, such that the absorbing thrust load vector is adapted to transmit the turbojet engine thrust loads to the aircraft fixing strut.