Research and Application of Digital High Performance Assembly Coordination Technology for Aircraft Composite Main Bearing Structure

YANG Yapeng; ZHAO An’an; DU Kunpeng; PENG Yun; LI You; GUO Feiyan

doi:10.16080/j.issn1671-833x.2024.16.014

您当前的位置：

首页 >

文章列表页 >

Research and Application of Digital High Performance Assembly Coordination Technology for Aircraft Composite Main Bearing Structure

更新时间：2025-10-30

- Research and Application of Digital High Performance Assembly Coordination Technology for Aircraft Composite Main Bearing Structure
- Aeronautical Manufacturing Technology Vol. 67, Issue 16, Pages: 14-31(2024)
- 作者机构：
  
  1. 中航西安飞机工业集团股份有限公司,西安,710089
  2. 浙江大学,杭州,310058
  3. 北京科技大学,北京,100083
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2024.16.014
  CLC：
- Published：2024
- 稿件说明：
移动端阅览
杨亚鹏，赵安安，杜坤鹏，彭云，李游，郭飞燕. 飞机复材主承力结构数字化高性能装配协调技术研究与应用[J]. 航空制造技术, 2024, 67(16): 14-31.

YANG Yapeng, ZHAO An’an, DU Kunpeng, PENG Yun, LI You, GUO Feiyan. Research and Application of Digital High Performance Assembly Coordination Technology for Aircraft Composite Main Bearing Structure[J]. Aeronautical Manufacturing Technology, 2024, 67(16): 14-31.
杨亚鹏，赵安安，杜坤鹏，彭云，李游，郭飞燕. 飞机复材主承力结构数字化高性能装配协调技术研究与应用[J]. 航空制造技术, 2024, 67(16): 14-31. DOI： 10.16080/j.issn1671-833x.2024.16.014.

YANG Yapeng, ZHAO An’an, DU Kunpeng, PENG Yun, LI You, GUO Feiyan. Research and Application of Digital High Performance Assembly Coordination Technology for Aircraft Composite Main Bearing Structure[J]. Aeronautical Manufacturing Technology, 2024, 67(16): 14-31. DOI： 10.16080/j.issn1671-833x.2024.16.014.

摘要

为满足新一代大型飞机复合材料主承力结构高精度、低损伤、低应力的装配性能与技术指标保证需求，本文以产品多种类关键特征耦合分析与控制为装配协调设计线索，以工程化应用研究为主线，系统地阐述了以关键特征识别、三维工艺容差仿真分析、装配过程变形预测、实测数据预装分析、高精度装配补偿等方法为主要技术路径的飞机复材主承力结构数字化高性能装配协调技术体系，并以典型复材外翼盒段部件装配为对象，对上述体系方法进行了全流程工程应用研究与试验验证，解决了复材外翼盒段部件装配协调设计与产品补偿策略设计问题，产品装配质量满足设计要求。

Abstract

In order to meet the requirements of high-precision

low-damage

low-stress assembly performance and technical indicators of the composite main bearing structure of the new-generation large aircraft

this paper takes the coupling analysis and control of various key features of the product as the design clue

takes the engineering application research as the main line

and systematically expounds the digital high-performance assembly coordination technical system with key feature identification

tolerance simulation analysis

deformation prediction in assembly process

preassembly analysis of measured data and high-precision assembly compensation as the main technical paths. Taking the assembly of a typical composite outer wing box as the object

the above method is applied to a complete whole-process engineering application research and experimental verification

which solves the problems of assembly coordination and product compensation trategy design of the composite outer wing box components. The product assembly quality meets the design requirements.

关键词

Keywords

references

Views

189

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Dynamic Measurement Method for Shaft Deflection Angles in Helicopter Drive Systems

Design and Experimental Verification of Stitching Forming System for Rigid Sandwich Composite Preforms

Large-Distance Straight-Line Datum Construction Based on Laser Collimation

Electromechanical Behavior of Open-Hole Three-Dimensional Angle-Interlock Woven Carbon Fiber Reinforced Polymer Under Tensile Loading

Research on Ultrasonic Vibration-Assisted Milling and Grinding of Ceramic Matrix Composites

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：34360 Visits Today：307

⁰