机身骨架装配柔性工装设计

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英文篇名：Flexible Tooling for Fuselage Skeleton Assembly 作者：孙永杰 ; 田威 ; 廖文和 ; 刘明爽 英文作者：SUN Yongjie;TIAN Wei;LIAO Wenhe;LIU Mingshuang;College of Mechanical & Electrical Engineering,Nanjing University of Aeronautics and Astronautics; 关键词：柔性工装 ; 交点孔定位 ; 机身骨架 英文关键词：Flexible tooling;;Intersection hole orientation;;Fuselage frame 中文刊名：HKGJ 英文刊名：Aeronautical Manufacturing Technology 机构：南京航空航天大学机电学院; 出版日期：2017-04-01 出版单位：航空制造技术 年：2017 期：No.526 基金：国家科技重大事项资助项目(2014ZX04001071) 语种：中文; 页：HKGJ201707017 页数：7 CN：07 ISSN：11-4387/V 分类号：81-86+91

摘要

为解决当前飞机机身装配工装效率低、定位精度不高、通用性差等问题,根据飞机机身结构,分析其装配需求,采用模块化设计思想,研制了面向机身骨架的"龙门式"柔性装配工装。该套柔性工装能够适应截面直径尺寸小于3m、机身筒段长度3~5m的产品,通过伺服电机驱动、手工调整以及更换特殊定位器等来实现对新类型机身的定位。工装操作简单、适应性强,能够以较低的成本提供较大的柔性。
        In order to solve the current problem of low efficiency,low positioning and poor generality accuracy of aircraft fuselage assembly tooling,according to the aircraft fuselage structure,analyze the assembly requirements,and the idea of modular design is developed for the fuselage frame "gantry" flexible assembly tooling. The set of flexible fixture is suitable for products section diameter size being less than 3m,the fuselage tube length being 3-5m,and could implement new type body positioning,etc. by servo motor,manual adjustment and replacement of special locator. Equipment operation is simple,strong adaptability,and can provide greater flexibility at a lower cost.

引文

[1]郭洪杰,康晓峰,王亮,等,飞机部件装配数字化柔性工装技术研究[J].航空制造技术,2011(22):94-97.GUO Hongjie,KANG Xiaofeng,WANG Liang,et al.Research on flexible tooling technology for digital assembly of aircraft fuselage[J].Aeronautical Manufacturing Technology,2011(22):94-97.
    [2]王亮,李东升,刘凤贵.飞机壁板类组件数字化装配柔性工装技术及应用[J].航空制造技术,2010(10):58-61.WANG Liang,LI Dongsheng,LIU Fenggui.Flexible tooling technology and application for digital assembly of aircraft panel component[J].Aeronautical Manufacturing Technology,2010(10):58-61.
    [3]王亮,李东升.飞机数字化装配柔性工装技术体系研究[J].航空制造技术,2012(7):34-39.WANG Liang,LI Dongsheng.Flexible tooling technology system for aircraft digital assembly[J].Aeronautical Manufacturing Technology,2012(7):34-39.
    [4]田威,廖文和,唐金成.面向复杂产品装配的柔性工装共性技术研究[J].中国机械工程,2010(22):2699-2704.TIAN Wei,LIAO Wenhe,TANG Jincheng.Common technology on flexible tooling for complex product assembly[J].The Chinese Mechanical Engineering,2010,21(22):2699-2704.
    [5]王建华,欧阳佳,陈文亮.飞机柔性装配工装关键技术及发展趋势[J].航空制造技术,2013(17):49-52.WANG Jianhua,OUYANG Jia,CHEN Wenliang.Key technology and development of flexible assembly tool for aircraft[J].Aeronautical Manufacturing Technology,2013(17):49-52.
    [6]袁立,郭洪杰.一代飞机一代技术[J].航空制造技术,2012(23/24):38-41.YUAN Li,GUO Hongjie.New generation aircraft with new generation technology[J].Aeronautical Manufacturing Technology,2012(23/24):38-41.
    [7]王仲奇,康永刚,王辉坪,等,飞机部件级的数字化柔性工装设计[J].航空制造技术,2011(22):101-104.WANG Zhongqi,KANG Yonggang,WANG Huiping,et al.Design of digital flexible assembly tooling on aircraft component[J].Aeronautical Manufacturing Technology,2011(22):101-104.
    [8]王仲奇,王赢,郭飞燕,等,壁板组件柔性装配工装技术[J].航空制造技术,2013(12):44-47.WANG Zhongqi,WANG Ying,GUO Feiyan,et al.Tooling technology of flexible assembly for panel component[J].Aeronautical Manufacturing Technology,2013(12):44-47.
    [9]郭洪杰,黄宁,武锋锋,等.“桥架式”柔性工装直接位置闭环控制技术研究[J].制造业自动化,2014(16):68-70,85.GUO Hongjie,HUANG Ning,WU Fengfeng,et al.The investigation of direct position close-loop control system technique for bridge-frame flexible tooling[J].Manufacturing Automation,2014(16):68-70,85.
    [10]郭飞燕,王仲奇,康永刚,等,飞机柔性装配工装设计[J].航空制造技术,2014(16):12-16.GUO Feiyan,WANG Zhongqi,KANG Yonggang,et al.Design of the flexible assemby tooling for aircraft[J].Aeronautical Manufacturing Technology,2014(16):12-16.