A propulsion unit for an aircraft including a nacelle with a D-shaped structure housing a thrust-reversing device with movable vanes, the nacelle containing two D-shaped half-structures each including an external reverser half-cowl. The propulsion unit contains an assembly box-type structure, attached in downstream cantilevered fashion to the turbojet engine fan casing, the box-type structure including two guide rails guiding the deflection vanes, a locking device between the assembly box-type structure and the half-beams in the six o'clock position of the D-shaped half-structures, the assembly box-type structure being arranged in the propulsion unit such that the guide rails guiding the vanes of the assembly box-type structure are situated in the continuation of the guide rails in the six o'clock position guiding the vanes attached to the fan casing, to provide continuity between the rails.
ENSEMBLE PROPULSIF POUR AÉRONEF COMPORTANT UN CAISSON D'ASSEMBLAGE SIX HEURES
PROPULSION UNIT FOR AIRCRAFT COMPRISING AN ASSEMBLY BOX-TYPE STRUCTURE IN THE SIX O'CLOCK POSITION
ANTRIEBSEINHEIT FÜR EIN FLUGZEUG MIT EINEM MONTAGEBOXARTIGEM AUFBAU IN DER SECHS-UHR-STELLUNG
01.12.2021
Patent
Elektronische Ressource
Französisch
ENSEMBLE PROPULSIF POUR AÉRONEF COMPORTANT UN CAISSON D'ASSEMBLAGE SIX HEURES
Europäisches Patentamt | 2019
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Europäisches Patentamt | 2019
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