ANTRIEBSEINHEIT EINES LUFTFAHRZEUGS, DIE EINE VERBINDUNGSVERKLEIDUNG ZWISCHEN EINER GONDEL UND EINEM MAST EINES LUFTFAHRZEUGS UMFASST, DIE MIT EINER ENTFERNBAREN ABDECKUNG AUSGESTATTET IST, UND MIT EINER SOLCHEN ANTRIEBSEINHEIT AUSGESTATTETES LUFTFAHRZEUG

摘要

The subject of the invention is a propulsion unit of an aircraft comprising a junction fairing (30), ensuring continuity between a nacelle (18) and a mast (22), which comprises: - a fixed chassis (32), connected to the nacelle (18) and to the mast (22) by a connection system (34) configured to absorb possible deformations and / or misalignments between the nacelle (18) and the mast (22) in operation, which has a wall exterior (36) comprising an opening (38), - a cover (40), movable between a closed position in which the cover (40) closes the opening (38) and an open position in which the cover (40) releases at at least partially the opening (38), which has a panel (44), - the outer wall (36) of the fixed frame (32) and the panel (44) of the cover (40) having outer surfaces which form the aerodynamic surface junction fairing (30) .The invention also relates to an aircraft which comprises at least one such propulsion unit.