The invention discloses a fairing lock seat assembly and an aircraft, and relates to the technical field of aviation. The fairing lock seat assembly comprises a fairing body, a support, a mounting part, a first connecting piece and a lock seat. The fairing body is fixedly connected with the support, the lock seat is connected with the mounting part, the support is provided with a first connectingstructure, the mounting part is provided with a second connecting structure, the first connecting structure is connected with the second connecting structure through the first connecting part, and thefirst connecting structure can move relative to the second connecting structure in the first direction. And the relative positions of the lock seat and the fairing body are adjusted in the first direction. Compared with the prior art, the fairing lock seat assembly provided by the invention adopts the first connecting structure arranged on the support and the second connecting structure arrangedon the mounting part, so that the position of the lock seat can be conveniently and quickly adjusted, later maintenance or part replacement is facilitated, and the fairing lock seat assembly is simplein structure and high in practicability.
本发明公开了一种整流罩锁座组件以及航空器,涉及航空技术领域。该整流罩锁座组件包括整流罩本体、支架、安装件、第一连接件和锁座。整流罩本体与支架固定连接,锁座与安装件连接,支架设置有第一连接结构,安装件设置有第二连接结构,第一连接结构通过第一连接件与第二连接结构连接,第一连接结构能够沿第一方向相对于第二连接结构运动,以在第一方向上调整锁座与整流罩本体的相对位置。与现有技术相比,本发明提供的整流罩锁座组件由于采用了设置于支架上的第一连接结构以及设置于安装件上的第二连接结构,所以能够方便快捷地对锁座的位置进行调整,便于后期维护或者零件更换,结构简单,实用性强。
Fairing lock seat assembly and aircraft
一种整流罩锁座组件以及航空器
2020-12-04
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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