Simulation of the Solid Rivet Installation Process

Baha, S.E.; Hesebeck, Olaf

doi:10.4271/2010-01-1843

Cited by 12 publications

(5 citation statements)

References 5 publications

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“…The friction coefficient experiments have been studied using MMW-2 microcomputer controlled high temperature friction and wear tester. The average friction coefficient is 0.19 between rivet and sheet metal and 0.17 between rivet and punch, which are close to 0.2 in literature (Baha et al, 2010).…”

Section: Friction Coefficient and Contact Conditionssupporting

confidence: 83%

“…Some experimental research gave information about the expansion and fatigue life of riveted joints (Huang, 2012). However, the riveting process is very complex due to following non-linearity (Baha II et al, 2010):…”

Section: Fe Model Developmentmentioning

confidence: 99%

“…Some experimental research gave information about the expansion and fatigue life of riveted joints (Huang et al, 2012). However, the riveting process is very complex because of the following non-linearity (Baha et al, 2010): 1 geometric non-linearity due to large displacement effect; 2 boundary non-linearity due to contact between die and rivet, rivet and sheet, sheet and sheet and also clamp and sheet; and 3 material non-linearity due to plastic deformation.…”

Section: Finite Element Model Developmentmentioning

confidence: 99%

“…The interaction between rivet and die has an important effect on the shape of the formed rivet head (Baha et al, 2010), which is considered as an indication of the fatigue performance of aircraft lap joints (De Rijck et al, 2007) (Table II). The precise friction coefficient is a critical parameter in the simulation of riveting process.…”

Section: Friction Coefficient and Contact Conditionsmentioning

confidence: 99%

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Modeling and predicting of aeronautical thin-walled sheet metal parts riveting deformation

Chang

Wang

Jiang

et al. 2016

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feiyan guo Yong-gang Kang , (2016),"Modeling and predicting of aeronautical thin-walled sheet metal parts riveting deformation", Assembly Automation, Vol. 36 Iss 3 pp. -Permanent link to this document: http://dx.If you would like to write for this, or any other Emerald publication, then please use our Emerald for Authors service information about how to choose which publication to write for and submission guidelines are available for all. Please visit www.emeraldinsight.com/authors for more information. About Emerald www.emeraldinsight.comEmerald is a global publisher linking research and practice to the benefit of society. The company manages a portfolio of more than 290 journals and over 2,350 books and book series volumes, as well as providing an extensive range of online products and additional customer resources and services.Emerald is both COUNTER 4 and TRANSFER compliant. The organization is a partner of the Committee on Publication Ethics (COPE) and also works with Portico and the LOCKSS initiative for digital archive preservation.Modeling and predicting of aeronautical thin-walled sheet metal parts riveting deformation Abstract Purpose -Riveting deformation is inevitable due to local relatively large material flows and typical compliant parts assembly, which affects the final product dimensional quality and fatigue durability. However, traditional approaches are concentrated on elastic assembly variation simulation and do not consider the impact of local plastic deformation. This paper presents a successive calculation model to study the riveting deformation where local deformation is taken into consideration. Design/methodology/approach -Based on the material constitutive model and friction coefficient obtained by experiments, an accurate three-dimension finite element (FE) model was built primarily using ABAQUS and verified by experiments. A successive calculation model of predicting riveting deformation was implemented by the Python and Matlab and solved by the ABAQUS. Finally, three configuration experiments were conducted to evaluate the effectiveness of the model. Findings -The model predicting results, obtained from both two simple coupons and a wing panel, showed that the model it was a good compliant with the experimental results and the riveting sequences had a significant effect on the distribution and magnitude of deformation. Practical implications -The proposed model to predict of predicting the deformation from riveting process was available in the early design stages and some efficient suggestions for controlling deformation could be obtained. Originality/value -A new predicting model of thin-walled sheet metal parts riveting deformation was presented to help the engineers to predict and control the assembly deformation more exactly.

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Section: Friction Coefficient and Contact Conditionssupporting

confidence: 83%

Section: Fe Model Developmentmentioning

confidence: 99%

Section: Finite Element Model Developmentmentioning

confidence: 99%

Section: Friction Coefficient and Contact Conditionsmentioning

confidence: 99%

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Modeling and predicting of aeronautical thin-walled sheet metal parts riveting deformation

Chang

Wang

Jiang

et al. 2016

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“…Spot welding [4][5][6] can not be used to heterogeneous sheets connection. Riveting joining [7,8] obviously increases the weight of the connections, although it can realize the connection between heterogeneous sheets. Sheet material, thickness and the number of layers have no influence on the threaded connections [9,10], but the *Corresponding author: e-mail address: fli@hrbust.edu.cn or hitlif@126.com connections are easy to loose during long time performance.…”

Section: Introductionmentioning

confidence: 99%

Mechanism and reliability of sheets embedded by cold press joining

LI¹,

YUAN²,

LIU³

et al. 2016

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Conventional mechanical joining methods, such as riveting, threaded connection and stamping connection, have obvious shortcomings in heterogeneous sheets joining. A new method of embedded cold joining was put forward, which can easily realize the connection between heterogeneous sheets. The method is suitable for connection of heterogeneous sheets with multi-layers and different thicknesses. This method can also decrease the cost greatly at the same time. Numerical simulation and experimental results indicate that a round hole sample has the maximum embedded depth and flash volume. Meanwhile, the elongation of aluminum sheet in hexagonal hole sample is the smallest. The joint strength of round hole sample increases with increment of the load pressure. Under the same load conditions, the joint strength of hexagonal hole sample is significantly higher than that of round hole and square hole sample. Additionally, the thickness decreased at different points on joint region because of the load pressure increasing. This paper shows an effective way how to realize the heterogeneous sheets connections.

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Analytical model for aircraft design based on Design for Excellence (DFX) concepts and use of composite material oriented to automated processes

Barbosa

Carvalho

2013

Int J Adv Manuf Technol

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Simulation of the Solid Rivet Installation Process

Cited by 12 publications

References 5 publications

Modeling and predicting of aeronautical thin-walled sheet metal parts riveting deformation

Modeling and predicting of aeronautical thin-walled sheet metal parts riveting deformation

Mechanism and reliability of sheets embedded by cold press joining

Analytical model for aircraft design based on Design for Excellence (DFX) concepts and use of composite material oriented to automated processes

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