Residual Stress Modeling and Simulating for the Panel with Interference-Fit Riveting

Dian Guo Yang; Kai Fu Zhang; Yuan Li; Hui Cheng; Bo Feng Liu

doi:10.4028/www.scientific.net/AMM.55-57.461

Paper Titles

Mechanical Properties of UP Resin from Soybean Oil
p.443

Preparing of SMC Artificial Marble and its Mechanical Properties
p.447

Quality Inspection and Analysis of Workpiece Surface in A3 Steel Machining
p.451

Preparation and Structure of Chitosan Swellable in Alkali Solution by Ultrasonic Treatment
p.456

Residual Stress Modeling and Simulating for the Panel with Interference-Fit Riveting
p.461

Edge Detection of Inner Crack Defects Based on Improved Sobel Operator and Clustering Algorithm
p.467

DFT-Based on Mahalanobis Distance Discriminant Analysis Method Channel Estimation Algorithm for OFDM Systems
p.472

Texture Baking Techniques on Construction of Virtual Reality Interactive Scenes
p.478

Explore on the Feasibility of RFID Technology in Library
p.484

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 55-57Residual Stress Modeling and Simulating for the...

Residual Stress Modeling and Simulating for the Panel with Interference-Fit Riveting

Abstract:

The interference-fit riveting technique is widely used in aircraft assembly, which can generate residual stress around the wall of hole and significantly improve the fatigue life of the structure. The residual stress is usually determined by experiment or numerical simulation, locking of theoretical support. So this paper researches the residual stress modeling of the panel in a riveting process. Firstly, based on the axisymmetric upsetting theory, dividing the riveting process into two stages, the formulas for calculating the contract pressure caused by the rivet around the hole of panel are built. Secondly, under the action of contact pressure, the residual stress distribution expressions are developed by elastic-plastic mechanics. Finally, in ABAQUS system, a three-dimensional instance made up of one flush rivet and two panels of aluminum alloy is used to verify the theoretical formulas. The feasibility of the theoretical formulas about the residual stress of the panel is validated by comparing the theoretical calculation and finite element simulation results.

You might also be interested in these eBooks

Recent Trends in Materials and Mechanical Engineering Materials, Mechatronics and Automation

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 55-57)

Pages:

461-466

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.55-57.461

Citation:

Cite this paper

Online since:

May 2011

Authors:

Dian Guo Yang, Kai Fu Zhang, Yuan Li, Hui Cheng, Bo Feng Liu

Keywords:

Finite Element (FE) Simulation, Interference-Fit Riveting, Panel, Residual Stress

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] S. Hossein: Adv. Manuf. Technol. Vol. 39 (2008), pp.1144-1145.

Google Scholar

[2] R.P.G. Muller: An Experimental and Analytical Investigation on the Fatigue Behavior of Fuselage Riveted Lap Joints (Ph.D., Delft University of Technology, Delft 1995).

Google Scholar

[3] M.P. Szolwinski and T.N. Farris: J. Aircr. Vol. 37 (2000), pp.130-137.

Google Scholar

[4] G. Li, G. Shi and N.C. Bellinger. AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (Austin, Texas, April 18-21, 2005). pp.18-21.

DOI: 10.2514/6.2005-2024

Google Scholar

[5] H.Q. Yu, J.D. Chen. Principles of Metal Plastic forming. (China Machine Press, China 1999).

Google Scholar

[6] J.H. Park, S.N. Atluri: Comput. Mech. Vol. 13 (1993), pp.189-203.

Google Scholar