多向作用力状态下的前缘蒙皮零件成形方法的研究  

Research on Forming Method of Leading Edge Skin Parts under Multi-directional Force

作　　者：王建华 徐驰 赵柳 Wang Jianhua;Xu Chi;Zhao Liu(Workshop of China Aviation Industry Changhe Aircraft Industry(Group)Co.,Ltd.,Jingdezhen Jiangxi 333000)

机构地区：[1]中国航空工业昌河飞机工业(集团)有限责任公司二十三车间

出　　处：《机械管理开发》2019年第11期47-48,84,共3页Mechanical Management and Development

摘　　要：蒙皮成形技术是航空航天制造领域的一项重要的加工技术,其先进程度是衡量一个国家飞机制造能力和水平的重要标识之一,因此研究蒙皮成形技术对于我国航空制造具有十分重要的意义。通过改变零件成形作用力,改善成形应力状态,充分发挥零件材料塑性;利用拉形成形和压形成形相结合的成形方法,对前缘蒙皮生产过程中存在的回弹问题进行生产性试验和测量分析,实现前缘蒙皮零件精准成形。The skin forming technology is an important processing technology in the field of aerospace manufacturing,and its advanced degree is one of the important marks to measure the manufacturing ability and level of a country’s aircraft, so it is of great significance to study skin forming technology for aviation manufacturing in China. By changing the forming force of the part, improving the forming stress state and giving full play to the plasticity of the part material,the springback problem existing in the production process of the leading edge skin is tested and measured and analyzed by using the forming method of the combination of drawing forming and compression forming, so as to realize the accurate forming of the leading edge skin part.

关 键 词：飞机蒙皮 应力状态 拉形成形 压形成形 

分 类 号：V26[航空宇航科学与技术—航空宇航制造工程]