The invention relates to an aircraft pylon comprising an aircraft pylon fairing (4) extending along a longitudinal axis (40a), a primary structure (3) having pins (32) inserted into through-openings (43) of inner ribs (42) of the fairing (4), four yokes (42l, 42r, 44l, 44r) and four detachable fixing elements (46) which can be inserted from outside the fairing (4), the fixing element is inserted in a direction perpendicular to the longitudinal axis (40a) of the fairing (4) to hold a fitting (33) of the primary structure (3) in position, the fitting having an oblong through opening (33 ', 33' ') and being inserted into one of the yokes in the fairing (4). Advantageously, the operation of assembling the cowl can thus be considerably simplified, and a better protected fixed interface can be obtained, while allowing the cowl to be mounted on the primary structure in a statically determinate manner, with optimal load transfer between the cowl and the primary structure.
本发明涉及一种飞行器挂架,其包括沿纵向轴线(40a)延伸的飞行器挂架整流罩(4)、具有插入到所述整流罩(4)的内肋(42)的贯通开口(43)中的销钉(32)的初级结构(3)、四个轭(42l、42r、44l、44r)以及四个可拆卸的固定元件(46),固定元件可以从整流罩(4)外部插入,所述固定元件沿垂直于所述整流罩(4)的所述纵向轴线(40a)的方向插入以将初级结构(3)的配件(33)保持就位,配件具有长圆形贯通开口(33’、33”)并且插入到整流罩(4)中的所述轭之一中。有利地,因此可以相当地简化组装整流罩的操作、并获得被更佳保护的固定接口,同时允许整流罩以静定方式安装在初级结构上,切在整流罩与初级结构之间具有最佳的载荷传递。
Improved aircraft pylon fairing, fairing assembly, aircraft pylon and aircraft
改进的飞行器挂架整流罩、整流罩组件、飞行器挂架和飞行器
2024-03-05
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |