The invention relates to a seal (1) designed to be placed between a turbojet engine and a movable part of a nacelle, said seal comprising a tubular body (28) delimiting an inner cavity (30) placed between at least one fixed part (32) and a platform (34), the platform (34) includes a first side edge (342) and a second side edge (344) and a planar surface (340) extending from the first side edge (342) to the second side edge (344).
本发明涉及一种密封件(1),其设计成置于涡轮喷气发动机和机舱的可动部件之间,所述密封件包括管状主体(28),所述管状主体界定置于至少一个固定部件(32)和平台(34)之间的内腔(30),所述平台(34)包括第一侧边缘(342)和第二侧边缘(344)以及从所述第一侧边缘(342)延伸至所述第二侧边缘(344)的平坦表面(340)。
Aircraft seal
飞行器密封件
2022-03-11
Patent
Electronic Resource
Chinese