东北大学学报（自然科学版）

东北大学学报:自然科学版 ›› 2015, Vol. 36 ›› Issue (5): 704-708.DOI: 10.12068/j.issn.1005-3026.2015.05.021

• 机械工程 • 上一篇    下一篇

基于多域集成映射的飞机部件及其夹具模型

徐开元1,2， 曲蓉霞1， 王健熙3   

  1. (1. 东北大学 流程工业综合自动化国家重点实验室， 辽宁 沈阳110819;2. 东北大学 机械工程与自动化学院， 辽宁 沈阳110819;3. 中国人民解放军驻沈阳黎明航空发动机公司军事代表室， 辽宁 沈阳110043)
  • 收稿日期:2014-04-10 修回日期:2014-04-10 出版日期:2015-05-15 发布日期:2014-11-07
  • 通讯作者: 徐开元
  • 作者简介:徐开元(1985-)，男，河北唐山人，东北大学博士研究生.
  • 基金资助:
    总装备部预研基金重大资助项目(5131XXXXX)； 国家自然科学基金资助项目(51305074).

Aircraft Part and Its Assembly Fixture Model Based on Multi-domain Integrated Mapping

XU Kai-yuan1, 2， QU Rong-xia1， WANG Jian-xi3   

  1. 1. State Key Lab of Integrated Automation for Process Industry， Northeastern University， Shenyang 110819， China; 2. School of Mechanical Engineering & Automation， Northeastern University， Shenyang 110819， China; 3. Military Representative Office of PLA， Shenyang Liming Aero-Engine Co.， Shenyang 110043， China.
  • Received:2014-04-10 Revised:2014-04-10 Online:2015-05-15 Published:2014-11-07
  • Contact: XU Kai-yuan
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摘要： 面向装配信息数据表达与飞机零部件装配夹具协同设计问题，阐述了飞机装配对象及其夹具多域集成建模过程，该建模过程给出了多域集成模型的知识框架.其次，定义各领域信息构成，全面系统地描述了装配工艺规划的所有数据.提出了装配对象与装配夹具之间互映射机理，详细阐述了互映射过程中所需的4个关键知识点.最后以翼尖小翼为实例，证明建模方法的可行性与有效性，使夹具设计更加系统化，提高了飞机结构、装配工艺规划和工装设计的协同设计效率和响应速度.

关键词: 飞机装配夹具设计, 特征建模, 翼尖小翼, 多域集成映射

Abstract: Considering the problem of aircraft part assembly fixture collaborative design and assembly data expression， the modeling process of aircraft assembly object and its fixture multi-domain integration was discussed. The modeling process provides the knowledge framework of multi-domain integration model. The information composition of all domain， and describe all the data in the assembly process field were defined. At the same time， the mapping mechanism between assembly object and assembly fixture， and elaborate four key knowledge points included in mapping process was proposed. Finally， the effectiveness and feasibility of the method are demonstrated by winglet example， making it more systematic and improving the response speed & the collaborative design efficiency of aircraft structure， assembly process planning， and tooling design.

Key words: aircraft assembly fixture design, feature modeling, winglet, multi-domain integrated mapping

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