An aircraft propulsion system includes an engine assembly including a fan that moves air, and a cowl that surrounds at least a portion of the engine assembly when the cowl is in a closed position. The cowl includes an outer surface arranged away from the engine assembly that provides an aerodynamic surface. The aircraft propulsion system also includes a cowl mechanism connected to the cowl and configured to guide the cowl along a movement path from the closed position to an open position. In the open position, an entirety of the cowl is arranged farther away from a horizontal plane passing through a rotating axis of the fan than in the closed position.
AIRCRAFT ENGINE NACELLE COWLING MECHANISM
VERKLEIDUNGSMECHANISMUS FÜR TRIEBWERKSGONDEL EINES FLUGZEUGES
MÉCANISME DE CAPOTAGE DE NACELLE DE MOTEUR D'AÉRONEF
29.11.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Europäisches Patentamt | 2019
|Europäisches Patentamt | 2016
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