Research on Modular Assembly Technology of Aircraft Wing

WANG Shouchuan; HAO Ju; LI Xining; GUO Feng; WANG Yonghong; WANG Zhanfeng

doi:10.16080/j.issn1671-833x.2018.13.068

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Research on Modular Assembly Technology of Aircraft Wing

更新时间：2025-10-30

- Research on Modular Assembly Technology of Aircraft Wing
- Aeronautical Manufacturing Technology Vol. 61, Issue 13, Pages: 68-73(2018)
- 作者机构：
  
  1. 航空工业西飞技术装备设计所,西安,710089
  2. 西北工业大学机电学院，现代设计与集成制造技术教育部重点实验室,西安,710072
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2018.13.068
  CLC：
- Published：2018
- 稿件说明：
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王守川1，郝巨1，李西宁2，郭峰1，王永宏1，王战峰1. 飞机机翼模块化装配技术研究[J]. 航空制造技术, 2018, 61(13): 68-73.

WANG Shouchuan1, HAO Ju1, LI Xining2, GUO Feng1, WANG Yonghong1, WANG Zhanfeng1. Research on Modular Assembly Technology of Aircraft Wing. Aeronautical Manufacturing Technology, 2018, 61(13): 68-73.
王守川1，郝巨1，李西宁2，郭峰1，王永宏1，王战峰1. 飞机机翼模块化装配技术研究[J]. 航空制造技术, 2018, 61(13): 68-73. DOI： 10.16080/j.issn1671-833x.2018.13.068.

WANG Shouchuan1, HAO Ju1, LI Xining2, GUO Feng1, WANG Yonghong1, WANG Zhanfeng1. Research on Modular Assembly Technology of Aircraft Wing. Aeronautical Manufacturing Technology, 2018, 61(13): 68-73. DOI： 10.16080/j.issn1671-833x.2018.13.068.

摘要

针对某大飞机机翼模块化工程实现，对飞机部件模块化装配技术背景和机翼模块化特征进行了分析，梳理出了机翼模块化流程和影响因子，从机翼模块化装配流程、机翼模块化/ 集成化装配、活动翼面模块化调装与测试3方面进行了工程设计。对机翼集成化/ 柔性化装配的高集成工作平台、柔性化滑轨安装车和活动翼面单元化测试的控制逻辑结构、测试方法、测试设备规划进行了详细的设计分析。最后对机翼模块化装配实施与应用效果进行了介绍。

Abstract

In view of the engineering realization of the modular assembly of a large aircraft wing

the technical background and the modular features of the aircraft components module are analyzed

and the module assembly process and the influencing factors are combed. The engineering design of wing assembly process

wing integration / flexible assembly and active airfoil unit is carried out. The integrated flexible working platform and rail mounting vehicle are designed. The design and analysis of control logic structure

test method and test equipment planning for aircraft active airfoil are finished. Finally

the application of wing module assembly and its effect are introduced.

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