Seal having a large compression range

Details Seal having a large compression range Seal having a large compression range

F - Mech Eng,Light,Heat,Weapons

16

J

F16J 15/02 (2006.01) B64D 29/00 (2006.01) F02C 7/28 (2006.01) F16J 15/10 (2006.01)

Patent

CA 2696837

The invention relates to a seal (1) designed to be inserted between a cowl (51) of a rear section of a nacelle and a turbojet of an aircraft propulsion unit. Said seal (1) includes a cylindrical portion (2) and at least one lip (3) extending radially from a generatrix of the cylindrical part (2).

Ce joint d'étanchéité (1) est conçu pour être interposé entre un capot (51) d'une section arrière d'une nacelle et un turboréacteur d'un ensemble propulseur d'un aéronef. Ce joint d'étanchéité (1) présente une partie cylindrique (2) et au moins une lèvre (3) s'étendant radialement depuis une génératrice de la partie cylindrique (2).

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