CAJ | 학술논문

针对翼身融合整体结构装配的需要，开展了翼身融合整体结构特点分析。根据不同装配阶段进行了骨架柔性定位技术规划、蒙皮与骨架自定位技术规划、自动制孔技术规划和数字化辅助测量定位及自动对接技术规划研究。通过本文的研究，可以为采用翼身融合结构的飞机开展柔性装配做出指导，同时也可为非翼身融合结构的飞机机翼或机身开展柔性装配提供帮助和技术支持。
침대익신융합정체결구장배적수요，개전료익신융합정체결구특점분석。근거불동장배계단진행료골가유성정위기술규화、몽피여골가자정위기술규화、자동제공기술규화화수자화보조측량정위급자동대접기술규화연구。통과본문적연구，가이위채용익신융합결구적비궤개전유성장배주출지도，동시야가위비익신융합결구적비궤궤익혹궤신개전유성장배제공방조화기술지지。
According to assembly BWB (blend-ed wing body) structure, the feature of BWB structure is analyzed. According to different assembly phase, schedul-ing of lfexible positioning technology of frame,skin self-positioning technology, automatic drilling technology, and digital measurement-assisted positioning and automatic junction technology is studied. Through the research, it is helpful for the BWB structure lfexible assembly, and other aircraft wing or fuselage lfexible assembly.