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US 11,885,283 B2Granted
Aircraft seal
AssigneeSafran Nacelles
InventorsCédric Renault, Arnaud Bonny
Life of this patent
Estimating the term…
Abstract
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.
Claims13
A seal interposed between a turbojet engine and a movable part of a nacelle, the seal comprising:
- a tubular body delimiting an inner cavity interposed between at least one fixing part and a platform, the platform comprising a first lateral edge, a second lateral edge and a planar surface extending from the first lateral edge to the second lateral edge at least when the seal is at rest, when no compression is applied to the seal,
- wherein the seal comprises a protuberance arranged on the platform.
Dependencies are inferred from the claim text.