Sealing device for use between two structures e.g. honeycomb composite panels, of aircraft turbojet nacelle, has body comprising free end that is in contact with one structure, and made of rubber material allowing radial deformation of body

摘要

The device (105) has a rectangle or oval shaped body (107) comprising an end (109) that is fixed on a structure (103) of a sealing assembly (100) of a nacelle. The body comprises a free end (111) that is in contact with another structure (101) arranged near the former structure. The body is made of rubber material, which allows radial deformation of the body. The body comprises a core made of metal or glass and formed to maintain the body in position on the two structures. The fixed end of the body is provided with a seal.