An aircraft propulsion unit includes a turbojet engine, a lateral pylon connected to the fuselage of the aircraft, and a nacelle on the lateral pylon. The nacelle includes an upstream section having an air intake, a downstream section housing a reverse thrust device, and a middle section having two fan half-cowls surrounding a fan housing of the turbojet engine, and when said half-cowls are in a closed position defining an aerodynamic continuity between the upstream and downstream sections. The fan half-cowls include a maintenance half-cowl positioned under the horizontal median plane of the nacelle, able to move between the closed position and an open position allowing access to the turbojet engine for maintenance operations on the turbojet engine. The nacelle further includes at least one standby lock, designed to hold the maintenance half-cowl in a position intermediate to the closed and open positions.
ENSEMBLE PROPULSIF POUR AÉRONEF, RELIÉ AU FUSELAGE DUDIT AÉRONEF
AIRCRAFT PROPULSION UNIT, CONNECTED TO THE FUSELAGE OF SAID AIRCRAFT
AN DEN FLUGZEUGRUMPF ANGESCHLOSSENE ANTRIEBSEINHEIT FÜR DAS FLUGZEUG
2020-02-05
Patent
Electronic Resource
French
ENSEMBLE PROPULSIF POUR AERONEF, RELIE AU FUSELAGE DUDIT AERONEF
European Patent Office | 2018
|ENSEMBLE PROPULSIF POUR AÉRONEF, RELIÉ AU FUSELAGE DUDIT AÉRONEF
European Patent Office | 2018
|