A seal interposed between a turbojet engine and a movable part of a nacelle includes a tubular body delimiting an inner cavity interposed between at least one fixing part and a platform. The platform includes a first lateral edge, a second lateral edge and a planar surface extending from the first lateral edge to the second lateral edge. The seal includes a protuberance arranged on the platform. The protuberance is centered on the platform or extends from the first lateral edge to the second lateral edge.
JOINT D'ÉTANCHÉITÉ POUR AÉRONEF
SEAL FOR AN AIRCRAFT
DICHTUNG FÜR EIN FLUGZEUG
2022-06-01
Patent
Electronic Resource
French
Joint d’étanchéité pour aéronef et aéronef incorporant au moins un tel joint.
European Patent Office | 2023
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