Content area

Abstract

Purpose

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Aerospace assembly demands high drilling position accuracy for fastener holes. Hole position error correction is a key issue to meet the required hole position accuracy. This paper aims to propose a combined hole position error correction method to achieve high positioning accuracy.

Design/methodology/approach

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The bilinear interpolation surface function based on the shape of the aerospace structure is capable of dealing with position error of non-gravity deformation. A gravity deformation model is developed based on mechanics theory to efficiently correct deformation error caused by gravity. Moreover, three solution strategies of the average, least-squares and genetic optimization algorithms are used to solve the coefficients in the gravity deformation model to further improve position accuracy and efficiency.

Findings

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Experimental validation shows that the combined position error correction method proposed in this paper significantly reduces the position errors of fastener holes from 1.106 to 0.123 mm. The total position error is reduced by 43.49% compared with the traditional mechanics theory method.

Research limitations/implications

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The position error correlation method could reach an accuracy of millimeter or submillimeter scale, which may not satisfy higher precision.

Practical implications

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The proposed position error correction method has been integrated into the automatic drilling machine to ensure the drilling position accuracy.

Social implications

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The proposed position error method could promote the wide application of automatic drilling and riveting machining system in aerospace industry.

Originality/value

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A combined position error correction method and the complete roadmap for error compensation are proposed. The position accuracy of fastener holes is reduced stably below 0.2 mm, which can fulfill the requirements of aero-structural assembly.

Details

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Title
A combined hole position error correction method for automated drilling of large-span aerospace assembly structures
Author
Hu, Junshan 1 ; Sun, Xinyue 2 ; Tian, Wei 2 ; Shanyong Xuan 3 ; Yang, Yan 2 ; Wang, Changrui 2 ; Liao, Wenhe 4 

 College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China and Wuhu Machinery Factory, Wuhu, China 
 College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China 
 Wuhu Machinery Factory, Wuhu, China 
 School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing, China 
Publication title
Volume
42
Issue
3
Pages
293-305
Number of pages
13
Publication year
2022
Publication date
2022
Publisher
Emerald Group Publishing Limited
Place of publication
Bingley
Country of publication
United Kingdom
ISSN
01445154
e-ISSN
17584078
Source type
Scholarly Journal
Language of publication
English
Document type
Journal Article
Publication history
 
 
Online publication date
2022-04-11
Milestone dates
2021-01-14 (Received); 2021-08-15 (Revised); 2021-11-06 (Revised); 2021-12-08 (Revised); 2021-12-27 (Accepted)
Publication history
 
 
   First posting date
11 Apr 2022
ProQuest document ID
2667679661
Document URL
https://www.proquest.com/scholarly-journals/combined-hole-position-error-correction-method/docview/2667679661/se-2?accountid=208611
Copyright
© Emerald Publishing Limited.
Last updated
2024-11-12
Database
ProQuest One Academic