Patent ID: 7555894

Claim:
A swiveling exhaust nozzle for an aircraft engine, comprising pivoting means for pivoting the nozzle about at least one transverse pivoting axis on an external engine case and displacement means for displacing the nozzle about said transverse pivoting axis, wherein the pivoting means comprise two diametrically opposed coaxial pivots outside the nozzle, at least one of which is connected to the external engine case by an elastically deformable one-piece articulation, and wherein said transverse pivoting axis passes through said elastically deformable one-piece articulation; wherein each elastically deformable articulation comprises two elastically deformable blocks which are diametrically opposed with respect to the transverse pivoting axis and are each mounted between the pivot and a case element, one end of the blocks being rotationally fixed to the case element and their other end being rotationally fixed to the pivot.