Gap volume prediction for aircraft wing assembly

被引：2

作者：

Yang, Ye ^{[1
]}

Jin, Yan ^{[1
]}

Price, Mark ^{[1
]}

Abdelal, Gasser ^{[1
]}

Maropoulos, Paul ^{[1
]}

Higgins, Colm ^{[2
]}

机构：

[1] Queens Univ Belfast, Sch Mech & Aerosp Engn, Belfast, Antrim, North Ireland

[2] Queens Univ Belfast, Northern Ireland Technol Ctr, Belfast, Antrim, North Ireland

来源：

10TH CIRP SPONSORED CONFERENCE ON DIGITAL ENTERPRISE TECHNOLOGIES (DET 2020) - DIGITAL TECHNOLOGIES AS ENABLERS OF INDUSTRIAL COMPETITIVENESS AND SUSTAINABILITY | 2021年 / 54卷

基金：

英国工程与自然科学研究理事会;

关键词：

Predictive shimming; Laser scan; Point cloud data; Gap volume prediction; Aircraft assembly;

D O I：

10.1016/j.promfg.2021.07.035

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

In this work, two methods for predictive shimming based on laser scan technology and point cloud processing software have been presented. The first one is direct measurement method in PolyWorks, and the second one is feature-based modelling method in SolidWorks. Firstly, both component-level and assembly-level scans are collected by a laser scanner. Then, the point clouds are post-processed and registered in PolyWorks. Thirdly, gap information (shape and thickness) is obtained either in PolyWorks or in SolidWorks. Results show that the proposed methods can obtain gap information successfully based on current hardware and software. (c) 2020 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/)

引用

页码：227 / 232

页数：6

共 50 条

[11] Prognostic Algorithms for Flaw Growth Prediction in an Aircraft Wing
Bin Yousuf, Waleed
Khan, Tariq
Ali, Taha
IEEE TRANSACTIONS ON RELIABILITY, 2017, 66 (02) : 478 - 486
[12] Cycle time study of wing spar assembly on aircraft factory
Carbia Diaz, I.
Jin, Y.
Ares, E.
MANUFACTURING ENGINEERING SOCIETY INTERNATIONAL CONFERENCE 2017 (MESIC 2017), 2017, 13 : 1019 - 1025
[13] Implementing Determinate Assembly for the Leading Edge Sub-Assembly of Aircraft Wing Manufacture
Irving, Lucas
Ratchev, Svetan
Popov, Atanas
Rafla, Marcus
SAE INTERNATIONAL JOURNAL OF AEROSPACE, 2014, 7 (02): : 246 - 254
[14] Kinematic Design of a New Parallel Kinematic Machine for Aircraft Wing Assembly
Jin, Yan
Kong, Xianwen
Higgins, Colm
Price, Mark
2012 10TH IEEE INTERNATIONAL CONFERENCE ON INDUSTRIAL INFORMATICS (INDIN), 2012, : 669 - 674
[15] Joint measuring and evaluating technology for final assembly of aircraft wing and fuselage
Liu C.-H.
Ke Y.-L.
Zhejiang Daxue Xuebao (Gongxue Ban)/Journal of Zhejiang University (Engineering Science), 2011, 45 (02): : 201 - 208
[16] A Multi-aspect Simulation System for Flexible Aircraft Wing Assembly
Liu, Jihong
Zou, Cheng
INTELLIGENT ROBOTICS AND APPLICATIONS, PT II, PROCEEDINGS, 2008, 5315 : 679 - 687
[17] Manufacturing and assembly automation by integrated metrology systems for aircraft wing fabrication
Jamshidi, J.
Kayani, A.
Iravani, P.
Maropoulos, P. G.
Summers, M. D.
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART B-JOURNAL OF ENGINEERING MANUFACTURE, 2010, 224 (B1) : 25 - 36
[18] Numerical Study of a Transonic Aircraft Wing for the Prediction of Flutter Failure
Singh I.
Mishra R.K.
Aswatha Narayana P.S.
Journal of Failure Analysis and Prevention, 2017, 17 (1) : 107 - 119
[19] Numeric lightning protection prediction for wires in an aircraft wing raceway
Kebel R.
Stadtler T.
Rouquette J.-A.
Flourens F.
Avenet A.
Rouvrais N.
1600, Institute of Electrical and Electronics Engineers Inc., United States (05): : 71 - 79
[20] Aerodynamic Noise Prediction of Strut-Braced Wing Aircraft
Sticchi, E.
Ragni, D.
Casalino, D.
Avallone, F.
30TH AIAA/CEAS AEROACOUSTICS CONFERENCE 2024, 2024,

← 1 2 3 4 5 →