Patent ID: 8752842
Filing Date: 2014-06-17
Classification: B64D,F16J

Abstract:
1. A sealing member to be interposed between a nacelle element and an element of a turbojet of a propulsion unit of an aircraft, the sealing member comprising: at least two parallel independent tubular elements each having a quadrangular cross section including a planar bearing face at one end, a convex contact face for contact with an element to be sealed at another end, and two concave side faces connecting the convex contact face to the planar bearing face, the two tubular elements being connected by a common sole and formed by a knitted fabric coated with a synthetic matrix, wherein the planar bearing face merges in part with the sole, wherein the sealing member is configured to be compressed to a constant width by the concave side faces of the at least two parallel tubular portions, the concave side faces bending toward an inside of the tubular portion when the convex contact face contacts and is compressed by the element to be sealed.