TURBOJET ENGINE NACELLE COMPRISING A UNIT ASSEMBLY CAPABLE OF MOVING ALONG A GUIDE ASSEMBLY
The present invention relates to an assembly comprising at least one nacelle (1) unit assembly (9) for a turbojet engine, capable of moving relative to a fixed structure along at least one associated guide element (15), said guide assembly comprising: - at least one guiding element (17, 20) secured to the fixed structure; - at least one guided element (19) secured to the unit assembly, shaped to move along the guiding element; - at least one contact surface (21, 25) common to said guiding and guided elements.