Study on Optimization for Automatic Drilling and Riveting Off-line Programming Process of Aircraft Panel

LI Ming; QIU Nan; WANG Jing

doi:10.16080/j.issn1671–833x.2019.15.068

您当前的位置：

首页 >

文章列表页 >

Study on Optimization for Automatic Drilling and Riveting Off-line Programming Process of Aircraft Panel

更新时间：2025-10-30

- Study on Optimization for Automatic Drilling and Riveting Off-line Programming Process of Aircraft Panel
- Aeronautical Manufacturing Technology Vol. 62, Issue 15, Pages: 68-74(2019)
- 作者机构：
  
  航空工业江西洪都商用飞机股份有限公司,南昌,330096
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671–833x.2019.15.068
  CLC：
- Published：2019
- 稿件说明：
移动端阅览
黎明，邱楠，汪静. 飞机机身壁板自动钻铆离线编程过程优化研究[J]. 航空制造技术, 2019, 62(15): 68-74.

LI Ming, QIU Nan, WANG Jing. Study on Optimization for Automatic Drilling and Riveting Off-line Programming Process of Aircraft Panel. Aeronautical Manufacturing Technology, 2019, 62(15): 68-74.
黎明，邱楠，汪静. 飞机机身壁板自动钻铆离线编程过程优化研究[J]. 航空制造技术, 2019, 62(15): 68-74. DOI： 10.16080/j.issn1671–833x.2019.15.068.

LI Ming, QIU Nan, WANG Jing. Study on Optimization for Automatic Drilling and Riveting Off-line Programming Process of Aircraft Panel. Aeronautical Manufacturing Technology, 2019, 62(15): 68-74. DOI： 10.16080/j.issn1671–833x.2019.15.068.

摘要

自动钻铆离线编程是自动钻铆技术应用关键环节之一，离线编程质量与效率将直接影响飞机壁板的生产制造周期。研究分析了当前飞机机身壁板自动钻铆离线编程过程，针对目前飞机机身壁板自动钻铆离线编程过程效率低下、编程质量不高的现状，提出了一种飞机壁板自动钻铆快速离线编程方法，该方法优化了自动钻铆离线编程流程，同时针对自动钻铆离线编程过程数据处理繁琐、工作量大的问题基于CAA二次开发技术实现了离线编程过程数据的批量化处理。基于该自动钻铆离线编程方法可大幅提升当前飞机机身壁板自动钻铆离线编程质量与效率。

Abstract

As one of the critical steps of application of Automatic drilling and riveting technology

automatic drilling and riveting off-line programming will directly impact the manufacturing period of aircraft panel. This paper analyzed the process of automatic drilling and riveting off-line programming for aircraft panel. Aiming at improving the current situation

a method of fast automatic drilling and riveting off-line programming for aircraft panel is proposed

which has optimized off-line programming process and realizes batch processing for data of off-line programming based on CAA program development technology. It improves the efficiency and quality of automatic drilling and riveting off-line programming of the aircraft panel greatly based on this method.

关键词

Keywords

references

Views

284

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Strength Design and Optimization of Aviation Filter Assembly Based on CF/PEEK Composite

Research Progress on Matrix Composition Regulation of SiC/SiC Composites

Research Progress on Ceramic Matrix Composites for Aviation Applications

Assessment of Technological Advancement Based on Fuzzy Comprehensive Evaluation

Dynamic Measurement Method for Shaft Deflection Angles in Helicopter Drive Systems

Related Author

No data

Related Institution

No data

The platform construction and operation are provided by Beijing Founder electronics co., LTD 京ICP备09064830号-19 京公网安备11010802024621
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.
Total Visits：34528 Visits Today：6

⁰