Patent ID: 11952964
Assignee: SAFRAN NACELLES
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 10:
11. A propulsion unit for an aircraft, the propulsion unit comprising:
a turbojet engine; and
a nacelle supporting said turbojet engine, said nacelle comprises a cascade thrust reverser device comprising a cowl, wherein the cowl is movable between a retracted position providing an aerodynamic continuity of the nacelle for an operation of the nacelle in direct jet mode and between a deployed position defining an annular passage in the nacelle for an operation of the nacelle in reverse jet mode, wherein said propulsion unit comprises a sealing assembly according to claim 10, wherein the seal comprises a sealing body supported by the bead of said seal, said sealing body being in contact with a deflection edge of the turbojet engine.