Title :
Notice of Retraction
An effective method of studying interference-fit riveting for 2117-T4 aluminum slug rivet
Author :
Weiqiang Mu ; Yuan Li ; Kaifu Zhang ; Hui Cheng
Author_Institution :
Minist. of Educ. Key Lab. of Contemporary Design & Integrated Manuf. Technol., Northwestern Polytech. Univ., Xi´an, China
Abstract :
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
Interference-fit riveting of slug rivet is a well-known enhanced joining technique for improving the fatigue life of aircraft structures significantly, and is widely used in aircraft thin-walled structures, where riveting interference which is controlled by process parameters is very important to the joining strength. This paper firstly analyzes the upsetting process of 2117-T4 aluminum slug rivet and divides it into two stages due to the deformation characteristics of rivet, the true strain of rivet header is composed by the strain in the shank upsetting stage and the strain in the header forming stage. Secondly, based on the above analysis, the power hardening rule is employed to establish the physics formula of pressing force, thereby derive the theoretical mathematic relationship between relative interference and riveting process parameters. Thirdly, a two-dimension axisymmetric model is used to simulate the upsetting process of slug rivet by Finite Element Method according to the rivet´s features. Finally, compare the results calculated by the two mentioned methods above and analyze the effects of riveting process parameters on the riveting interference. It is shown that the theoretical method can be used for future analysis.
Keywords :
aircraft; aluminium; deformation; fatigue; finite element analysis; interference; riveting; thin wall structures; 2117-T4 aluminum slug rivet; aircraft thin-walled structures; deformation characteristics; fatigue life; finite element method; header forming stage; interference-fit riveting; joining strength; joining technique; power hardening rule; shank upsetting stage; two-dimension axisymmetric model; upsetting process; Analytical models; Atmospheric modeling; Deformable models; Interference; Mathematical model; Medical services; Finite element simulation; Interference-fit riveting; Pressing Force; Relative interference;
Conference_Titel :
Computer and Communication Technologies in Agriculture Engineering (CCTAE), 2010 International Conference On
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-6944-4
DOI :
10.1109/CCTAE.2010.5544166