Flexible Assembly System of Aircraft Panel Based on Inner Surface of Skin Positioning

CHANG Songyang; WANG Hongsheng; SHANGGUAN Jingyi; ZHU Lei; FENG Jun; ZHENG Chenji; FANG Qiang

doi:10.16080/j.issn1671-833x.2021.04.050

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Flexible Assembly System of Aircraft Panel Based on Inner Surface of Skin Positioning

更新时间：2025-10-30

- Flexible Assembly System of Aircraft Panel Based on Inner Surface of Skin Positioning
- Aeronautical Manufacturing Technology Vol. 64, Issue 4, Pages: 50-58(2021)
- 作者机构：
  
  1. 浙江大学机械工程学院航空制造工程研究所,杭州,310027
  2. 中航西安飞机工业集团股份有限公司,西安,710089
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2021.04.050
  CLC：
- Published：2021
- 稿件说明：
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常颂扬，王鸿昇，上官敬益，朱雷，冯军，郑晨绩，方强. 基于蒙皮内形定位的飞机壁板柔性装配系统[J]. 航空制造技术, 2021, 64(4): 50-58.

CHANG Songyang,WANG Hongsheng,SHANGGUAN Jingyi,ZHU Lei,FENG Jun,ZHENG Chenji,FANG Qiang. Flexible Assembly System of Aircraft Panel Based on Inner Surface of Skin Positioning. 航空制造技术, 2021, 64(4): 50-58.
常颂扬，王鸿昇，上官敬益，朱雷，冯军，郑晨绩，方强. 基于蒙皮内形定位的飞机壁板柔性装配系统[J]. 航空制造技术, 2021, 64(4): 50-58. DOI： 10.16080/j.issn1671-833x.2021.04.050.

CHANG Songyang,WANG Hongsheng,SHANGGUAN Jingyi,ZHU Lei,FENG Jun,ZHENG Chenji,FANG Qiang. Flexible Assembly System of Aircraft Panel Based on Inner Surface of Skin Positioning. 航空制造技术, 2021, 64(4): 50-58. DOI： 10.16080/j.issn1671-833x.2021.04.050.

摘要

针对飞机壁板数字化、柔性化制造需求，提出一种基于蒙皮内形定位的飞机壁板柔性装配方法，通过有限元参数化建模，应用蒙皮支撑点寻优算法，实现卡板布局优化设计。根据壁板组件各零件的定位要求，详细设计了壁板柔性装配系统中长桁、蒙皮、角片的柔性定位方式，开发了基于 EtherCAT 总线的分布式网络控制系统用于完成整个壁板的装配。本系统实现了在一套柔性装配系统上完成 4 块壁板的装配，改变了传统固定式工装设计思维，对飞机壁板柔性装配技术的发展具有重要意义。

Abstract

In order to meet the requirements of digital and flexible manufacturing of aircraft panel

this paper proposes a flexible assembly method of aircraft panel based on inner surface of skin positioning. Through the application of finite element parametric modeling and the optimization algorithm of skin support points

the optimization design of fixture board layout is realized. According to the positioning requirements of each part of the panel component

the flexible positioning method of stringer

skin and shear clip in the flexible assembly system was designed in detail

and the distributed network control system based on EtherCAT fieldbus technology was developed to complete the panel assembly. Through the application of this system

the assembly of four panels can be completed on one flexible tooling

which changes the traditional design approach and is of great significance to the development of aircraft panel flexible assembly technology

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