| 摘要 |
The present invention relates to a seal (105) for an aircraft turbojet engine nacelle thrust reverser, said seal comprising a body (113) of which the cross section with respect to a longitudinal axis (L) of the seal is, for example, substantially circular, and a base (115) which is intended to be mounted in a seal support. This seal is notable in that the base (115) of said seal has mutually-spaced openings (143). |
