A propulsive assembly of an aircraft comprises a junction fairing, ensuring a continuity between a nacelle and a pylon, which comprises a fixed frame, linked to the nacelle and/or to the pylon by a link system configured to absorb any deformations and/or misalignments between the nacelle and the pylon in operation, which has an outer wall comprising an opening, a cowl, mobile between a closed position in which the cowl blocks the opening, and an open position in which the cowl at least partially frees the opening, which has a panel, the outer wall of the fixed frame and the panel of the cowl having outer surfaces which form the aerodynamic surface of the junction fairing. An aircraft is also provided which comprises at least one such propulsive assembly.
ENSEMBLE PROPULSIF D'UN AÉRONEF COMPRENANT UN CARÉNAGE DE JONCTION ENTRE UNE NACELLE ET UN MÂT DE L AÉRONEF ÉQUIPÉ D'UN CAPOT AMOVIBLE ET AÉRONEF ÉQUIPÉ DUDIT ENSEMBLE PROPULSIF
PROPULSION ASSEMBLY OF AN AIRCRAFT COMPRISING A CONNECTING FAIRING BETWEEN A NACELLE AND A PYLON OF THE AIRCRAFT PROVIDED WITH A REMOVABLE COVER AND AIRCRAFT PROVIDED WITH SAID PROPULSION ASSEMBLY
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
2021-03-24
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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