某型飞机起落架舱门与结构件的协调安装技术  

Coordinated Installation Technique of Landing Gear Hatch Door and Structure for a Certain Aircraft

作　　者：王艳丽 Wang Yanli(AVIC Xi'an Aircraft Industry (Group) Co.,Ltd.,Xi'an Shaanxi 710089)

机构地区：[1]航空工业西安飞机工业(集团)有限公司,陕西西安710089

出　　处：《现代工业经济和信息化》2019年第3期34-35,37,共3页Modern Industrial Economy and Informationization

摘　　要：就某型飞机起落架舱门的结构形式、装配过程中的关键工艺和外蒙皮定位问题等进行详细的分析研究。同时依据该机型特殊结构特点和相关经验,论证了舱门协调安装过程中的关键技术。In this paper,the structure form of landing gear hatch,the key technology during assembly and the location of outer skin are analyzed and studied in detail.At the same time,according to the special structural characteristics and relevant experience of the aircraft,the key technology of the coordinated installation of the hatch is demonstrated.

关 键 词：起落架舱门 间隙 阶差 同轴度 外蒙皮 

分 类 号：V262.41[航空宇航科学与技术—航空宇航制造工程]