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
2023-11-29
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2019
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