Research Progress on Milling Deformation and Control of Aviation Structural Parts

doi:10.16080/j.issn1671-833x.2022.03.108Aviation

您当前的位置：

首页 >

文章列表页 >

Research Progress on Milling Deformation and Control of Aviation Structural Parts

更新时间：2025-07-30

- Research Progress on Milling Deformation and Control of Aviation Structural Parts
- Aeronautical Manufacturing Technology Vol. 65, Issue 3, (2022)
- 作者机构：
  
  1. 哈尔滨理工大学,哈尔滨,150080
  2. 先进制造智能化技术教育部重点实验室,哈尔滨,150080
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2022.03.108Aviation
  CLC：
- Published：2022
- 稿件说明：
移动端阅览
赵明伟，岳彩旭，陈志涛，张俊涛，刘献礼. 航空结构件铣削变形及其控制研究进展[J]. 航空制造技术, 2022, 65(3): 108-117.

ZHAO Mingwei，YUE Caixu，CHEN Zhitao，ZHANG Juntao，LIU Xianli . Research Progress on Milling Deformation and Control of Aviation Structural Parts[J]. Aeronautical Manufacturing Technology, 2022, 65(3): 108-117.
赵明伟，岳彩旭，陈志涛，张俊涛，刘献礼. 航空结构件铣削变形及其控制研究进展[J]. 航空制造技术, 2022, 65(3): 108-117. DOI： 10.16080/j.issn1671-833x.2022.03.108Aviation.

ZHAO Mingwei，YUE Caixu，CHEN Zhitao，ZHANG Juntao，LIU Xianli . Research Progress on Milling Deformation and Control of Aviation Structural Parts[J]. Aeronautical Manufacturing Technology, 2022, 65(3): 108-117. DOI： 10.16080/j.issn1671-833x.2022.03.108Aviation.

摘要

随着机床加工性能和刀具切削性能的提升，航空结构件的高效高精加工成为可能。航空结构件薄壁加工特征多，在铣削过程中易发生变形，因此预测与控制航空结构件的加工变形是切削加工领域内亟待解决的难题。通过总结了航空结构件的特点及加工难点，对加工变形形成机理进行深入分析；对加工变形影响最为关键的铣削力模型进行归纳；阐述了航空结构件残余应力变形预测的研究进展，以及利用加工工艺优化、数控补偿技术和高速切削加工技术等实现航空结构件加工变形控制的主要策略，最后对其未来研究方向进行了展望。

Abstract

With the improvement of machine tool processing performance and tool cutting performance

high efficiency and high precision machining of aviation structural parts becomes possible. There are many thin-wall features of aviation structural parts

which are prone to deformation during the milling process. Therefore

the prediction and control of aviation structural parts deformation is an urgent problem to be solved in the field of machining. Through summarizing the characteristics and processing difficulties of aviation structural parts

the forming mechanism of machining deformation is deeply analyzed. This paper summarizes the milling force model that is most critical to processing deformation

and explains the research progress of residual stress and deformation prediction of aviation structural parts. Machining process optimization

numerical control compensation technology and high-speed cutting technology are the main strategies to realize the deformation control of aviation structural parts. Finally

the future development is forecasted.

关键词

Keywords

references

Views

948

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Research on Ultrasonic Vibration Stress Control Technology of 5B70 Aluminum Alloy Welds

Influences of Tool Path on Machining Deformation of Trapezoidal Frame Thin-Walled Parts

Design of Adaptive Machining Fixture for Large Aircraft Structural Part Based on TRIZ

A Review of Plastic Forming Technologies and Applications for Large and Complex-Shaped Panels

Study on Ultra-Thin Part Deformation in Turning

Related Author

YANG Yinfei

LAI Xiaoming

GAO Liguo

ZHANG Hengyi

ZHANG Bin

YANG Kai

LIU Quanshuang

LI Fagui

Related Institution

Nanjing University of Aeronautics and Astronautics

Beijing Spacecrafts Manufacturing Co., Ltd.

Anhui University

Anhui Tianhang Mechanical & Electrical Co., Ltd.

AVIC Chengdu Aircraft Industrial (Group) Co., Ltd.

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：34496 Visits Today：443

⁰