A Subassembly Simulation Method with Physical Deformation and Reconstruction of an Aircraft

Yong Gang Kang; Fei Yan Guo; Ting Xu; Jie Huang; Cong Ren

doi:10.4028/www.scientific.net/AMM.420.3

Paper Titles

Preface and Organizing Committee

A Subassembly Simulation Method with Physical Deformation and Reconstruction of an Aircraft
p.3

Study on Influences of Air Spring Failures on Ride Quality of High-Speed Railway Trains
p.9

Study on the Resonant Frequency Gliding in the Ultrasonic Systems Loaded with Variable Axial Compression Force
p.16

Application of Fuzzy Structural Analysis for Damage Prediction Considering Uncertain S/N Curve
p.21

Rough Air-Soft Elastohydrodynamic Lubrication
p.30

Theoretical Investigation of Transient Lubrication in Spur Gear
p.36

Variable Reynolds Number Experimental Study on Aerodynamic Characteristic of Supercritical Airfoil RAE2822
p.42

Experimental Investigation on Cavitation Characteristics of a Three-Groove Journal Bearing
p.47

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 420A Subassembly Simulation Method with Physical...

A Subassembly Simulation Method with Physical Deformation and Reconstruction of an Aircraft

Abstract:

In order to include the physical deformation of the large thin-walled structure in the subassembly simulation process in aerospace, a new method based on model reconstruction was proposed. Firstly, finite element method is applied for calculating the deformation of the structural parts according to different assembly status with certain temperature and stress field. Based on the actual deformation data of the surface, some reference point was selected and the method of bicubic B-spline surface interpolation is selected to reconstruct the above surface, and to express the deformed structural parts. Based on physical deformation, a compensating method is proposed to amend assembly path in corresponding assembly process with the constructed model. Under the DELMIA virtual environment with the real, the simulation method has been put in to use on aircraft sidewall panel assembly, and the validity of the method is verified experimentally.

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Periodical:

Applied Mechanics and Materials (Volume 420)

Pages:

3-8

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.420.3

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Online since:

September 2013

Authors:

Yong Gang Kang, Fei Yan Guo, Ting Xu, Jie Huang, Cong Ren

Keywords:

Aircraft Panel, Assembly Simulation, Model Reconstruction, Physical Deformation

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