飞机舱门工装柔性技术研究  

Flexible Tooling Assembly Design of Engine Cabin Door

作　　者：王巍[1] 乌琛 闫梦娜 于国栋 孔林 WANG Wei;WU Chen;YAN Mengna;YU Guodong;KONG Lin(College of Aerospace Engineering,Shenyang Aerospace University,Shenyang 110136,China)

机构地区：[1]沈阳航空航天大学航空宇航学院,沈阳110136

出　　处：《机械工程师》2022年第9期10-12,16,共4页Mechanical Engineer

摘　　要：为了提高飞机舱门的稳定性及精度,基于飞机舱门的装配需求,结合柔性装配技术,完成了舱门柔性装配工装设计,由蒙皮定位工装和骨架定位工装构成,并利用有限元仿真技术验证工装设计的合理性。通过飞机舱门的柔性工装设计及研究,对于提高舱门装配精度以及促进柔性装配技术的发展具有重要意义。To improve the stability and precision of aircraft door, based on the assembly requirements of aircraft cabin doors, the flexible assembly tooling design is completed, which is composed of skin positioning tooling and skeleton positioning tooling, and the rationality of tooling design is verified by finite element simulation technology. It is of great significance to improve the assembly precision of aircraft door and promote the development of flexible assembly technology through the design and research of flexible assembly of cabin door.

关 键 词：柔性工装 舱门装配 真空吸盘 静力分析 

分 类 号：V262.35[航空宇航科学与技术—航空宇航制造工程]