Anti-fire seal assembly and nacelle comprising such a seal

摘要

A seal assembly for a turbojet nacelle includes a first end fastened to a first structure, and a second end contacting against a bearing zone of a second structure. The seal assembly further includes a plurality of adjacent blades arranged along the first end and extending longitudinally and perpendicularly thereto. In particular, a portion of the blades has an accordion-shaped structure.

主权项

1. A seal assembly for a turbojet nacelle, comprising:
a first end equipped with means for fastening to at least a first structure of the turbojet nacelle; a second end configured to come into contact against a bearing zone of a second structure of the turbojet nacelle; and at least two rows of blades each comprising a plurality of adjacent blades arranged along the first end and extending substantially longitudinally and substantially perpendicularly thereto, wherein at least one of the plurality of adjacent blades has an accordion-shaped structure, wherein said at least two rows of blades are radially spaced apart from each other with respect to a longitudinal axis of the adjacent blades, wherein said two rows of blades are circumferentially distributed around said longitudinal axis, and wherein said two rows of blades are configured to allow compression and release of the accordion-shaped structure without interfering with an adjacent row.