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Journal articles on the topic 'Riveted joints'

Author: Grafiati

Published: 4 June 2021

Last updated: 25 July 2025

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1

Witek, Lucjan, and Monika Lubas. "Experimental Strength Analysis of Riveted Joints Using Blind Rivets." Journal of KONES 26, no. 1 (2019): 199–206. http://dx.doi.org/10.2478/kones-2019-0024.

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Abstract This article presents results of experimental investigations of the lap blind riveted joint. The main goal of the work is determination of destructive load of the blind riveted joints. The blind rivets were originally used in the aircraft structures where access to both sides of the riveted structure is impossible. Blind rivets are now commonly used in many branches of industry because of their low cost. Moreover, the riveting process is uncomplicated. There are many publications about analysis of strength of solid rivets in the research literature. However, the strength analysis of t

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2

Dourado, Marco Daniel Malheiro, and José Filipe Bizarro de Meireles. "A Simplified Finite Element Riveted Lap Joint Model in Structural Dynamic Analysis." Advanced Materials Research 1016 (August 2014): 185–91. http://dx.doi.org/10.4028/www.scientific.net/amr.1016.185.

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This paper proposes a simplified finite element model to represent a riveted lap joint in structural dynamic analysis field. The rivet is modeled byspring-damperelements. Several numerical models are studied with different quantities of rivets (1, 3 and 5) andspring-damperelements (4, 6, 8, 12, 16 and 20) per rivet. In parallel, samples of two aluminum material plates connected by different quantities of rivets (1, 3 and 5) are built and tested in order to be known its modal characteristics – natural frequencies and mode shapes. The purpose of the different settings is to get the best numerica

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3

Rudawska, Anna, Izabela Miturska, Dana Stančeková, and Jacek Mucha. "The strength of traditional and self-pierced riveted joints." MATEC Web of Conferences 244 (2018): 01007. http://dx.doi.org/10.1051/matecconf/201824401007.

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The objective of this study is to compare the strength of riveted joints fabricated by traditional riveting (with pre-drilled holes) and self-piercing riveting (SPR) for different types of joints. Riveted joints were produced using steel and aluminum alloy rivets and two types of sheet material: 235JR steel sheet and EN AW 6060 aluminum alloy sheet with the following dimensions: length l = 100 ± 1 mm, width b = 50 ± 1 mm and thickness g = 2 mm. For all tested types of riveted joints (pre-drilled and SPR), 5 sets of joints were fabricated, each set containing 6 samples. The sets of joints diffe

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4

Fortier, Vincent, Jean-E. Brunel, and Louis L Lebel. "Fastening composite structures using braided thermoplastic composite rivets." Journal of Composite Materials 54, no. 6 (2019): 801–12. http://dx.doi.org/10.1177/0021998319867375.

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Aerospace composite material components are currently joined using heavy titanium bolts. This joining method is not ideal when considering its weight, thermal expansion, electrical conductivity, and risk of unbalanced load distribution. We propose here an innovative fastening technology using thermoplastic composite rivets. A rivet blank is heated above its melting temperature using Joule heating and is formed directly in the composite laminates by an automated process. Carbon fiber and polyamide blanks were used with two fiber architecture: 2D braid and unidirectional. The braided architectur

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5

Roszak, Robert, Karol Bula, Ilia Sagradov, Tomasz Sterzyński, Daniela Schob, and Matthias Ziegenhorn. "Experimental and numerical investigation of metal-polymer riveted joints." Materials Research Express 9, no. 1 (2022): 015303. http://dx.doi.org/10.1088/2053-1591/ac49bb.

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Abstract This paper presents the modeling and analysis of the joints of metal inserts with polyamide 6 using the injection technique. Based on the experiments carried out, modeling and numerical calculations of the joints were performed for various joint configurations. The metal parts made of DS04 steel have holes. The holes are filled with polyamide 6 (PA6) by injection molding and both components are joined, resulting in a riveted joint. As part of the work, the steel / PA6 riveted joints were tested in a uniaxial tensile test. The main objective was to investigate the strength of the rivet

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6

Liu, Jintong, Anan Zhao, Zhenzheng Ke, Zhendong Zhu, and Yunbo Bi. "Influence of Rivet Diameter and Pitch on the Fatigue Performance of Riveted Lap Joints Based on Stress Distribution Analysis." Materials 13, no. 16 (2020): 3625. http://dx.doi.org/10.3390/ma13163625.

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Interference-fit riveting is one of the most widely used mechanical joining ways in aircraft assembly. The fatigue performance of riveted joints has a significant impact on the service life and reliability of aircraft. In this paper, the fatigue performance of the riveted lap joints with various rivet diameters and pitches are studied based on stress distribution analysis under tensile load. First, a theoretical model of the riveted lap joint under tensile load is developed by using the spring-mass model. The rivet-load stress, bypass stress, and interference stress around the riveted hole are

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7

Rośkowicz, Marek, Jan Godzimirski, Michał Jasztal, and Jarosław Gąsior. "Improvement of fatigue life of riveted joints in helicopter airframes." Eksploatacja i Niezawodnosc - Maintenance and Reliability 23, no. 1 (2021): 167–75. http://dx.doi.org/10.17531/ein.2021.1.17.

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Using original cold-formed rivets in repairs of airframes of helicopters is difficult due to no access to inside parts of the airframe. Thus, the main aim of the study was to investigate the possibility to use the blind rivets or hybrid joints by verification the fatigue performance of such joints that must be better than with original rivets. Riveted and hybrid joints have been experimentally tested under static and fatigue loads. Furthermore, numerical calculations of stress distribution for strapped joint have been conducted. The test results covered fatigue life of lap joints and models of

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8

Livieri, Paolo. "Numerical Analysis of Double Riveted Lap Joints." Lubricants 11, no. 9 (2023): 396. http://dx.doi.org/10.3390/lubricants11090396.

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In a previous work, the fatigue behaviour of different hot riveted joints under fatigue loadings were experimentally calculated. In particular, the experimental data showed a Wöhler curve slope close to five against the slope of three proposed by Eurocode 3. However, two series of shear splice riveted joints showed, at two million cycles, a stress range very close to the value suggested by Eurocode for shear splices that use non-preloaded high-strength bolts. In order to clarify the fatigue behaviour of riveted joints at high- and medium-fatigue regimes, this paper presents a preliminary three

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9

A., Gujar. "Mechanical Behavior and Performance Analysis of Riveted Joints in Structural Assemblies." Advancement in Mechanical Engineering and Technology 7, no. 3 (2024): 49–54. https://doi.org/10.5281/zenodo.14168424.

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<em>Riveted joints are a fundamental component in mechanical structures and assemblies due to their ability to provide reliable and durable connections. This study investigates the mechanical behavior and performance characteristics of riveted joints under varying load conditions and material properties. Using experimental data and simulation techniques, such as Finite Element Analysis (FEA), we explore the failure modes, stress distribution, and fatigue life of riveted joints in various configurations. A detailed comparison is made between different rivet materials, joint geometries, and load

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10

Yu, Haidong, Bin Zheng, Xun Xu, and Xinmin Lai. "Residual stress and fatigue behavior of riveted lap joints with various riveting sequences, rivet patterns, and pitches." Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture 233, no. 12 (2019): 2306–19. http://dx.doi.org/10.1177/0954405419834481.

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The residual stress of multi-rivet structures is related with the riveting sequence, the rivet pattern, and the pitch due to the deformation interaction of different rivets. The stress amplitude of riveted structures subjected to the cyclic loads is affected by the residual stress, which increases the difficulty in the prediction of fatigue life. In this article, the riveting processes for single-row and triple-row riveted lap joints with various riveting sequences, rivet patterns, and pitches are studied numerically and experimentally. The residual stresses for both types of riveted structure

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11

Kondo, Atsushi, Toshiyuki Kasahara, and Atsushi Kanda. "A Simplified Finite Element Model of Riveted Joints for Structural Analyses with Consideration of Nonlinear Load-Transfer Characteristics." Aerospace 8, no. 7 (2021): 196. http://dx.doi.org/10.3390/aerospace8070196.

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A simplified finite element model of riveted joints for structural analyses which effectively incorporates nonlinear response of riveted joints is proposed. Load-transfer characteristics of riveted joints were experimentally and numerically studied. First, a detailed finite element analysis for the process of a tensile test of a single-row joint which consists of squeezing of the rivet and tensile loading to the joint was conducted to confirm the validity of a conventional method of analysis. The load–relative displacement behaviors of single-row joints observed in the detailed finite element

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12

Sadowski, T., and E. Zarzeka-Raczkowska. "Hybrid Adhesive Bonded and Riveted Joints – Influence of Rivet Geometrical Layout on Strength of Joints / Połączenia Hybrydowe Klejowo-Nitowe - Wpływ Geometrii Rozmieszczenia Nitów Na Wytrzymałość Połączeń." Archives of Metallurgy and Materials 57, no. 4 (2012): 1127–35. http://dx.doi.org/10.2478/v10172-012-0126-0.

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The hybrid adhesive bonded and riveted joints have wider and wider application in different branches of engineering: aerospace, mechanical, civil etc. The hybrid joints’ strength is 1.5 to 3 times higher than only adhesive bonded joints’ strength. The hybrid joints characterize higher reliability during long-term working. In this article we present the influence of rivets’ lay-out geometry on the hybrid adhesive bonded/riveted joints response to mechanical loading. Experimental research was carried using 3-D digital image correlation system ARAMIS. This system enables monitoring of the deforma

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13

Ren, Kerong, Haobing Han, Wentao Xu, and Hua Qing. "The Effect of Rivet Arrangement on the Strengths of Lap Joints and Lap Joint Design Methods." Applied Sciences 13, no. 9 (2023): 5629. http://dx.doi.org/10.3390/app13095629.

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To address the impact of rivet arrangement on the strengths of riveted lap joints, the failure modes and failure mechanisms of riveted lap joints were first studied using finite element analysis software. Next, the effects of the number of rivets, rivet rows, rivet arrangement, and row spacing on the lap joint strength were studied using the peak load as the evaluation index. Then, we proposed the concept of line load density to solve the problem that a varying rivet spacing and rivet edge distance will change the width of the sheet and thus the maximum load capacity, which is used as an index

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14

Lundkvist, Axel, Imad Barsoum, Zuheir Barsoum, and Mansoor Khurshid. "Geometric and Material Modelling Aspects for Strength Prediction of Riveted Joints." Metals 13, no. 3 (2023): 500. http://dx.doi.org/10.3390/met13030500.

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The aim of this study is to develop a methodology for static strength and failure mode simulation of hot-driven riveted joints. The purpose is to be able to accurately estimate a rivet joint’s static strength behaviour and its failure mode without relying on experiments, to save both time and resources during the design of joints. The non-linear finite element analysis modelling framework considered the rivet joint configurations and geometry, the material properties of the plate and rivet as well as the clamping force of the hot-driven rivet. A ductile damage model was also implemented to cap

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15

Mucha, Jacek, and Waldemar Witkowski. "The Structure of the Strength of Riveted Joints Determined in the Lap Joint Tensile Shear Test." Acta Mechanica et Automatica 9, no. 1 (2015): 44–49. http://dx.doi.org/10.1515/ama-2015-0009.

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Abstract The article presents the analysis of the structure of the load capacity of riveted joints. For the four joining systems the lap joint specimens were made and tested in the shearing test. The joints were prepared for the three combinations of the DC01 steel and EN AW- 5754 aluminium alloy sheets with the thickness of 2mm. On the basis of the obtained load-elongation diagram tensile shear test curves, the basic parameters defined in the ISO/DIS 12996 standard were determined. In the case of the conventional riveted joints the maximum load capacity of the joint is determined by the stren

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16

LEONTYEV, V. V. "ANALYSIS OF THE STRESS-STRAIN STATE OF A RIVET JOINT USING THE ABAQUS CAE SYSTEM." Fundamental and Applied Problems of Engineering and Technology 6 (2020): 51–57. http://dx.doi.org/10.33979/2073-7408-2020-344-6-51-57.

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The method for analyzing of stress-strain state characteristics of unloaded riveted joints performed with OST 1 11781-74 rivets has been developed using Coupled Euler-Lagrange finite element approach implemented in the CAD / CAE system Abaqus. A comparative analysis of the stress-strain state characteristics of the examined riveted joint’s finite element models using the Lagrangian and the Coupled Lagrangian-Eulerian finite element approaches has been conducted. A three- dimensional finite element model based on the CLE method has been proposed for further study of fatigue strength and durabil

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17

Sadowski, Tomasz, and Przemysław Golewski. "Effect of Tolerance in the Fitting of Rivets in the Holes of Double Lap Joints Subjected to Uniaxial Tension." Key Engineering Materials 607 (April 2014): 49–54. http://dx.doi.org/10.4028/www.scientific.net/kem.607.49.

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The study focused mainly on one of the parameters of mount technology - tolerance for fitting the rivet in the hole in riveted and hybrid (riveted adhesive) joints. The research included numerical simulations of double lap joints with four rivets arranged in two rows and subjected to uniaxial tension. Simulations were carried out in Abaqus both for the purely mechanical and the hybrid joints. The connections without clearance (neat-fit) and with clearance of 0.2 mm, as well as with interference of-0.2 mm. The presence of clearance in one of the holes in the hybrid joint causes a decrease in th

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18

Machniewicz, Tomasz, Małgorzata Skorupa, Andrzej Skorupa, and Adam Korbel. "Applicability of Empirical Formulae for the Fatigue Notch Factor to Estimate Riveted Lap Joint Fatigue Strength." Solid State Phenomena 224 (November 2014): 81–86. http://dx.doi.org/10.4028/www.scientific.net/ssp.224.81.

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A semi-empirical fatigue life prediction model under development by the present authors for riveted lap joints used in aircraft structures is outlined. In contrast to existing models, it will account for the influence of the rivet squeeze force on the fatigue life of riveted joints. To determine the effect of rivet-hole interference on the fatigue behaviour of a riveted joint, a series of fatigue tests on filled hole coupons with different amounts of interference will be carried out under loading conditions representing the bypass load, transfer load and secondary bending. These experiments wi

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19

ZHAO, Letian, Tianzhi YANG, Qi HUANG, and Yangjie ZUO. "Damage behavior and mechanical property investigation of CFRP/CFRP washer-bushing riveted joints." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 41, no. 6 (2023): 1089–96. http://dx.doi.org/10.1051/jnwpu/20234161089.

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Carbon fiber reinforced composites (CFRP) are prone to occur riveting damage. Therefore, the damage behaviors and mechanical properties of CFRP/CFRP washer-bushing riveted joints were investigated experimentally in this paper. Results showed that due to the uneven expansion of rivet shank and local pressure caused by upsetting head, CFRP/CFRP riveted joints occurred multiple damage modes by using net riveting method and bushing method. The damage was mainly located in the layer around the CFRP hole near the upsetting head. However, washer-bushing riveting method effectively limited the uneven

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20

Liu, Jintong, Anan Zhao, Zhenzheng Ke, Zhiqiang Li, and Yunbo Bi. "Investigation on the Residual Stresses and Fatigue Performance of Riveted Single Strap Butt Joints." Materials 13, no. 15 (2020): 3436. http://dx.doi.org/10.3390/ma13153436.

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In aircraft manufacturing, riveting is one of the most important connection ways to fasten the sheet metal parts. The riveted single strap butt joints are mainly used in the load-bearing components of the aircraft such as the fuselage and wing panels. The connection quality and fatigue performance of the riveted joints directly affect the reliability and safety of the aircraft. In this paper, under the assumption of constant temperature, the fatigue strengthening mechanism of interference-fit riveting is introduced based on elastic-plastic mechanics and fracture mechanics. On this basis, the f

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21

Rohan, Bhalekar, and Gujar A. "Study on Rivets and Joints in Mechanical Applications." Research and Reviews on Experimental and Applied Mechanics 8, no. 1 (2025): 16–19. https://doi.org/10.5281/zenodo.15245032.

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<em>Riveted joints have been a foundational element in mechanical engineering and structural applications for centuries. Despite modern advancements in welding and adhesive bonding, rivets continue to hold significance due to their reliability, simplicity, and effectiveness in specific environments and load conditions. This research paper explores the types, design, materials, and mechanical behavior of rivets and joints, including their advantages, limitations, and application areas. Comparative analysis with other joining methods is provided to emphasize where riveted joints stand in current

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22

Černý, Michal, and Josef Filípek. "Corrosion damage of rivet joints." Acta Universitatis Agriculturae et Silviculturae Mendelianae Brunensis 56, no. 4 (2008): 37–46. http://dx.doi.org/10.11118/actaun200856040037.

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The work describes the effect of the atmospheric corrosion upon the mechanical properties of blind rivets. The subject of given research is: corrosion of metal materials, system resistance, design modification and others means of prevention against the corrosion attack. The problem of blind rivets, blind rivet setting, setting equipment, terminology and definitions, characteristic, and special blind rivet setting is also analysed. The experiment itself, the experimental method and the evaluation of the test are described. Mechanism of riveted joint damage produced by galvanic corrosion is prop

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23

Lei, Changyi, Qinggai Huang, and Yunbo Bi. "Tensile Load Distribution Improvement of Three-Row Riveted Lap Joint Based on Different Squeezing Displacement Combinations." Coatings 11, no. 7 (2021): 856. http://dx.doi.org/10.3390/coatings11070856.

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Many previous studies have mainly focused on the effects of riveting parameters on single-row riveted lap joints. Little attention has been paid to multi-row riveted lap joints. The outer rows of a normal multi-row riveted lap joint usually bear a larger part of the tensile load. However, none of the studies relate the phenomenon to the squeezing displacement combination of a multi-row riveted lap joint. To improve the performance of a three-row riveted lap joint, this paper aims to reveal the internal relation between tensile load distribution, structural deformation and squeezing displacemen

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Lipski, Adam, and Zbigniew Lis. "Improving Fatigue Life of Riveted Joints by Rivet Hole Sizing." Key Engineering Materials 598 (January 2014): 141–46. http://dx.doi.org/10.4028/www.scientific.net/kem.598.141.

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The aim of this paper is to assess the impact of the rivet hole sizing process on the fatigue life based on the example of the structural connections characteristic for riveted joints used in aviation industry. Test specimens reflected the structural connection consisting in a riveted lap joint of an airplane plating stiffened with a T-bar. Connected plates and the T-bar are made of D16CzATW aluminum alloy. 3 mm diameter oval head solid rivets for aviation-related purposes were made of PA24 aluminum. During fatigue tests, individual specimens with non-sized holes and with sized holes were subj

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Fung, C.-P., and J. Smart. "Riveted single lap joints. Part 1: A numerical parametric study." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 211, no. 1 (1997): 13–27. http://dx.doi.org/10.1243/0954410971532460.

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Snap and countersunk riveted single lap joints with either one or two-rows of rivets have been analysed using finite elements and fatigue tests have been performed. In this first paper, a numerical parametric study, the joints are subjected to an alternating cyclic load and plasticity and non-linear geometry are considered. The stresses around the rivet hole and the deformed shapes of the joints are presented together with the effects of varying the clamping force, the interference fit of the rivet, the coefficient of friction and the geometry of the joints when the joints are subjected to var

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Lubas, Monika. "The visual research of changes in the geometry of a rivet joint for material model effect for simulation riveted joints made of EN AW 5251." Technologia i Automatyzacja Montażu, no. 4 (2022): 54–64. http://dx.doi.org/10.7862/tiam.2022.4.6.

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The paper presents the results of a numerical analysis of a single-lap joint with a blind rivet and its geometrical verification by inside views from the experiment. The research aimed to determine how the results of numerical analyses (FEM) were influenced by the method of modeling the material model and how it relates to the experimental results. As part of the analyses, a discrete riveted model and material model: linear and nonlinear were constructed. The analyses took into account various load cases (500, 800, and 900 N) to better illustrate the relationship between the numerical and expe

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27

Lai, Jiamei, Zhichao Huang, Nanlin Tang, Zhaoxiao Hu, and Yuqiang Jiang. "Insight of Salt Spray Corrosion on Mechanical Properties of TA1-Al5052 Self-Piercing Riveted Joint." Materials 15, no. 23 (2022): 8643. http://dx.doi.org/10.3390/ma15238643.

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Self-piercing riveted (SPR) joints in automobiles inevitably suffer from corrosion damage and performance reduction. In this work, the influence of salt spray corrosion on the mechanical properties of TA1-Al5052 alloy SPR joints was studied. The TA1-5052 SPR joints were prepared and salt spray tests were carried out for different durations. The static and fatigue strengths of the joints after salt spray corrosion were tested to analyze the effect of salt spray duration on the performance of the joints. The results show that the joints’ static strength and fatigue strength decrease with prolong

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28

Fongsamootr, Thongchai, Charoenyut Dechwayukul, Notsanop Kamnerdtong, Carol A. Rubin, and George T. Hahn. "Parametric Study of Combined Adhesive-Riveted Lap Joints." Key Engineering Materials 261-263 (April 2004): 399–404. http://dx.doi.org/10.4028/www.scientific.net/kem.261-263.399.

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Riveted lap joints are widely used to assemble complex structures, e.g. aircraft fuselages. A thin layer of adhesive (sealant), is normally applied to lap joints in order to restrict the entry of moisture and retard corrosion. In this work, combined adhesive-riveted lap joints were studied to understand the effect of three parameters: panel thickness, adhesive stiffness and adhesive layer thickness, on single row non-countersunk riveted lap joints. Finite element analysis (FEA), along with Thin Adhesive Layer Analysis (TALA-developed for simulating the adhesive layer in lap joint models), were

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Skorupa, Andrzej, Małgorzata Skorupa, Tomasz Machniewicz, and Adam Korbel. "An Experimental Investigation on Crack Initiation and Growth in Aircraft Fuselage Riveted Lap Joints." Materials Science Forum 726 (August 2012): 211–17. http://dx.doi.org/10.4028/www.scientific.net/msf.726.211.

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Effects of variables related to design and production of riveted lap joints representative of longitudinal sheet connections for a pressurized transport aircraft fuselage were experimentally investigated. The specimens from an aircraft Al alloy D16 Alclad sheets of three different thicknesses (1.9, 1.2 and 0.8 mm) were assembled under load control using round head rivets and rivets with the compensator from a P24 Al alloy. For the joints from 1.9 mm thick sheets fatigue tests indicated a dependency of the crack initiation site and crack path on the squeeze force level and on the rivet type. At

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Nedelcu, Roxana, Daniela Bartiș, Anca Lupaș, Constantin Ilie, and Daniela Voicu. "Studies on Establishing a Methodology for Predicting the Riveted Joints Fatigue Durability in Aircraft Structures." Advanced Materials Research 1036 (October 2014): 668–73. http://dx.doi.org/10.4028/www.scientific.net/amr.1036.668.

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In this paper are described fatigue physical tests that were performed on a great number of riveted specimens with different constructive and technological parameters. Some of the purposes of the experimental tests, they were: determining the number of load cycles at which cracks by fatigue occurred, determining the moment of initiation, the location and propagation speed of the fatigue crack. For fatigue crack evolution study numerical models were designed. A simplified model for FEM analysis was proposed that reduced considerable the calculus effort and allows models for complex riveted join

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Otroshi, Mortaza, Gerson Meschut, Christian Bielak, Lukas Masendorf, and Alfons Esderts. "Modeling of Stiffness Anisotropy in Simulation of Self-Piercing Riveted Components." Key Engineering Materials 883 (April 2021): 35–40. http://dx.doi.org/10.4028/www.scientific.net/kem.883.35.

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The so-called substitute models based on shell elements can be used to design the self-piercing riveted components economically and with sufficient accuracy. In this study, the SPR3 (Self-Piercing Rivet) model with anisotropic stiffness parameters implemented in commercial simulation software LS-DYNA is used to describe the stiffness of self-piercing riveted joints subjected to different loading conditions. The model provides the basis for the subsequent fatigue life estimation of self-piercing riveted joints under cyclic loading. By accurate prediction of the stiffness of self-piercing rivete

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32

Kulkarni, Santosh, Devendra Singh, Laeth Hussain, et al. "Finite element analysis of bonded, riveted and hybrid joints in glass fibre epoxy composite laminates for aircraft structure." E3S Web of Conferences 563 (2024): 02006. http://dx.doi.org/10.1051/e3sconf/202456302006.

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Because of their superior fatigue resistance and high strength-to-weight ratio, composite materials are essential to the construction of modern airplanes. The joints that interconnect the various parts of these structures play a critical role in their integrity and functionality. In aerospace applications, bonded, riveted, and hybrid joints are among the many types of joints that are frequently used. A thorough finite element analysis (FEA) of hybrid, bonded, and riveted joints in glass fiber epoxy composite laminates for airplane structures is presented in this work. The literature review add

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Wronicz, Wojciech, and Jerzy Kaniowski. "The Analysis of the Influence of Riveting Parameters Specified in Selected Riveting Instructions on Residual Stresses." Fatigue of Aircraft Structures 2014, no. 6 (2014): 63–71. http://dx.doi.org/10.1515/fas-2014-0005.

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Abstract The riveting parameters strongly affect residual stresses induced during riveting, which in turn have an impact on the fatigue life of riveted joints. Since rivets are established as critical from the fatigue point of view, the fatigue life of riveted joints often determines the life of the whole structure. The authors were able to become acquainted with three riveting instructions (process specifications) used by the aerospace companies from western Europe. This work presents the analysis of the riveting parameters' influence on residual stresses around the rivets. The impact of the

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Reddy, Ch Vinay kumar. "Efficiency of Riveted Joints: Lozenge Joint." International Journal for Research in Applied Science and Engineering Technology 6, no. 2 (2018): 542–44. http://dx.doi.org/10.22214/ijraset.2018.2105.

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Borba, Natascha Z., Jorge F. dos Santos, and Sergio T. Amancio-Filho. "The Influence of Clamping Pressure on Joint Formation and Mechanical Performance of Ti6Al4V/CF-PEEK Friction-Riveted Joints." Materials 12, no. 5 (2019): 745. http://dx.doi.org/10.3390/ma12050745.

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This work aims at investigating the influence of pre-set clamping pressure on the joint formation and mechanical strength of overlapping direct-friction-riveted joints. A pneumatic fixture device was developed for this work, with clamping pressure varying from 0.2 MPa to 0.6 MPa. A case study on overlapping joints using Ti6Al4V rivets and woven carbon fiber-reinforced polyether-ether-ketone (CF-PEEK) parts were produced. Digital image correlation and microscopy revealed the expected compressive behavior of the clamping system and the continuous pressure release upon the joining process owing t

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Ehmaida, Mutyaa, and Raghed Asaied Alsaeh. "Modeling and Simulation of Two Plates Connected Via a Single Riveted Lap-Joint." University of Zawia Journal of Engineering Sciences and Technology 1, no. 1 (2024): 30–45. http://dx.doi.org/10.26629/uzjest.2023.04.

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Rivets and riveted lap joints are important mechanical fasteners that are used in a large variety of applications, and their performance depends on many parameters. The goal of this study is to model and simulate two plates joined together by a riveted lap joint. Four configurations were used, which are 2-vertical, 2-horizontal, 4-inline and 4-staggered configurations, and diameters of 0.2 cm to 0.4 cm were also used. The plate was subjected to forces ranging between 2000 N to 8000 N. Results have shown that the 4-inline configuration was the best due to its lower stresses than the other confi

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Pitta, Roure, Crespo, and Rojas. "An Experimental and Numerical Study of Repairs on Composite Substrates with Composite and Aluminum Doublers Using Riveted, Bonded, and Hybrid Joints." Materials 12, no. 18 (2019): 2978. http://dx.doi.org/10.3390/ma12182978.

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In this work, experimental and numerical analyses of repairs on carbon fiber reinforced epoxy (CFRE) substrates, with CFRE and aluminum alloy doublers typical of aircraft structures, are presented. The substrates have a bridge gap of 12.7 mm (simulated crack), repaired with twin doublers joined with riveted, adhesive bonded, and hybrid joints. The performance of the repairs using different doubler materials and joining techniques are compared under static loading. The experimental results show that riveted joints have the lowest strength, while adhesive bonded joints have the highest strength,

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Běhal, Jiří, and Roman Růžek. "EFFECT OF THE RIVET-HOLE TOLERANCE ON THE STRESS-SEVERITY FACTOR." Materiali in tehnologije 55, no. 2 (2021): 237–42. http://dx.doi.org/10.17222/mit.2020.146.

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This work is focused on a quantitative procedure for estimating the generally unfavourable effects that incorrectly drilled holes, characterized by the initial clearance between a rivet and a hole, have on the fatigue life of riveted joints. The solution is based on an analytical approach using the stress-severity-factor concept. An experimental programme with riveted-joint specimens characterized by low-load transfer factors was realized in the Czech Aerospace Research Centre (VZLU) test lab under constant amplitude loading. The holes for rivet joints with 4-mm diameters were prepared with th

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Mańkowski, Jarosław. "Numeric simulations of surface pressure and microslip phenomena occurring in riveted joints of semi-monococque structures in effect of the action of tension field." Advanced Technologies in Mechanics 3, no. 1(6) (2017): 7. http://dx.doi.org/10.17814/atim.2016.1(6).34.

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Tension fields are shown to have an influence on surface pressure and on material deformation in the riveted joints in thin walled structures and particularly in semistressed skin structures. Stresses and materials displacements were analyzed in the riveted joints performing under such conditions. Special attention has been attached to estimation of the microslips occurring between rivets and holes. A thin plate panel has been used for the test sample, which under effort condition revealed tension fields.

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Kamińska, Paulina, Piotr Synaszko, Patryk Ciężak, and Krzysztof Dragan. "Analysis of the Corrosion Resistance of Aircraft Structure Joints with Double-Sided Rivets and Single-Sided Rivets." Fatigue of Aircraft Structures 2020, no. 12 (2020): 57–68. http://dx.doi.org/10.2478/fas-2020-0006.

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Abstract An important factor having a negative impact on the technical condition of aircraft structure elements is the adverse effect of the atmosphere, which causes formation of corrosion in aircraft structures, especially in riveted lap joints. The electric potential difference between the sheet material and the rivet, in the presence of humid air, may cause electrochemical corrosion. The paper presents specimens that imitate the repair on the Mi-24 helicopter with the use of blind rivets in places where solid double-sided rivets could not be used. The aim of the research was to assess the c

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Wang, Di, Liyuan Qu, Tianyuanye Wang, et al. "Study on Effects of Geometric Parameters on Tensile Strength of Hybrid Bonded-Rived Joint of Fiber Reinforced Polymer Plates." Journal of Physics: Conference Series 2566, no. 1 (2023): 012039. http://dx.doi.org/10.1088/1742-6596/2566/1/012039.

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Abstract Hybrid bonded-rived joint combines bonding and riveting and has become one of the most important connection forms in composite materials. This paper investigates and analyzes the influence of geometric parameters of CFRP hybrid bonded-rived joints on load-bearing strength. The finite element method is used to analyze the strength of the hybrid bonded/riveted joint between carbon fiber composite and metal under tensile load. The different ratios of the hybrid joint’s e/D, w/D, and w/e are analyzed. It is shown that e/D and w/D significantly impact damage loads and failure mode of the h

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Woytowich, Richard. "Riveted Hull Joint Design in RMS Titanic and Other Pre—World War I Ships." Marine Technology and SNAME News 40, no. 02 (2003): 82–92. http://dx.doi.org/10.5957/mt1.2003.40.2.82.

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Beginning with an overview of riveted joint construction, this paper shows that the efficiency of riveted joints in pre-World War I ships decreased as plate thickness increased. In the case of the RMS Titanic, some of the joints involved in the iceberg impact were only about 27% as strong as the plates they connected. A finite element model is used to show how such a joint would respond to the sort of out-of-plane load that the iceberg would have applied. For one possible load configuration, the joint failure is recreated. Finally, although Titanic and her sisters were not built to class, the

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Fung, C.-P., and J. Smart. "An Experimental and Numerical Analysis of Riveted Single Lap Joints." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 208, no. 2 (1994): 79–90. http://dx.doi.org/10.1243/pime_proc_1994_208_257_02.

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Countersunk and snap riveted single lap joints have been examined both experimentally and numerically. A total of 11 specimens were fatigued to failure with failures occurring in either the plate or the rive***r. The failures have been metallurgically examined to determine the cause of failure. The joints have also been analysed using the finite element method. Initially a single lap joint has been modelled as a ‘stepped plate’ and the results for the stress concentration factor found to be in reasonable agreement with published data. However, the stress concentration for this joint occurred a

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Han, Li, Ken W. Young, R. Hewitt, A. Chrysanthou, and J. M. O'Sullivan. "The Effect of Pre-Straining on the Mechanical Behaviour of Self-Piercing Riveted Aluminium Alloy Sheets." Advanced Materials Research 6-8 (May 2005): 157–62. http://dx.doi.org/10.4028/www.scientific.net/amr.6-8.157.

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Self-piercing riveting as an alternative joining method to spot-welding has attracted considerable interest from the automotive industry and has been widely used in aluminium intensive vehicles. Pressing and stamping are important processes in automotive production and result in additional straining on the vehicle body sheet material. It is therefore important to have knowledge of the effect of sheet pre-straining on the quality of the self-piercing riveted joints and on the mechanical behaviour of the riveted aluminium alloy sheets. This paper reports the influence of sheet pre-straining on t

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Фатюхин, Дмитрий, Dmitriy Fatyukhin, Равиль Нигметзянов, et al. "Engineering process of manufacturing riveted joint using ultrasonic percussive impact." Science intensive technologies in mechanical engineering 2019, no. 6 (2019): 17–21. http://dx.doi.org/10.30987/article_5ce675a19ef690.18259732.

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The matters of riveted joint production effectiveness increase are considered. A circuit of percussive ultrasonic riveting is presented. There is offered an engineering process for riveted joint production. The test results of joints manufactured by percussive ultrasonic riveting are shown.

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Torres-Arellano, Mauricio, Manuel de Jesus Bolom-Martínez, Edgar Adrian Franco-Urquiza, Ruben Pérez-Mora, Omar A. Jiménez-Arévalo, and Philippe Olivier. "Bearing Strength and Failure Mechanisms of Riveted Woven Carbon Composite Joints." Aerospace 8, no. 4 (2021): 105. http://dx.doi.org/10.3390/aerospace8040105.

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This research aimed to determine riveted carbon/epoxy composites’ mechanical performance when fabricated by resin transfer molding (RTM). As this manufacturing process is gaining importance in the aeronautics and automotive industries, assembly methods and their reliability must be studied in terms of their airworthiness and transportation implementation. The study case resumes the determination of the bearing strength of RTM-woven carbon composites for different rivet joint diameters (1/8, 5/32 and 3/16 in). The joint shear strength was obtained following the ASTM D5961 instructions, and post

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Beber, Martin, Martin Stejskal, and Frantisek Sedlacek. "Determination of Mechanical Properties of Blind Rivet Joints Using Numerical Simulations and Experimental Testing." Materials 18, no. 2 (2025): 229. https://doi.org/10.3390/ma18020229.

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This study explores the tensile performance of blind rivet joints in galvanized steel sheets, focusing on their behavior under shear and normal load conditions. Blind rivets are frequently used in structural applications due to their ease of installation and ability to be applied from one side, making them highly effective in industries like aerospace and automotive. Two types of DIN 7337—4.8 × 8 blind rivets—galvanized steel St/St and stainless steel A2/A2—paired with galvanized steel sheets DX51D + Z275, were experimentally tested to assess how their material properties affect their joint st

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Konoplin, A. Yu, and N. I. Baurova. "Complex evaluation of quality of glued-mechanical joints." Adhesives. Sealants. Technologias, no. 10 (October 2020): 32–37. http://dx.doi.org/10.31044/1813-7008-2020-0-10-32-37.

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The component tree of the complex index of the glued-mechanical joint quality is presented. Its main branches are purpose and processability indices, and economy indices. The change of quality indices when replacing the traditional mechanical joints (welded, riveted) by the glued-mechanical ones (glued-welded, glued-riveted) was examined. The classification of factors that have influence on fracture processes of glued-mechanical joints is given. Based on analysis of fracture characters of glued-mechanical joints, possible causes of fractures are demonstrated.

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Gavrylov, Eugene. "Експериментальне дослідження впливу плівкоутворюючих антикорозійних сполук на втому заклепкових з’єднань". Aerospace Technic and Technology, № 1 (27 лютого 2024): 56–63. http://dx.doi.org/10.32620/aktt.2024.1.05.

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The subject matter of this article is the influence of film-forming corrosion preventive compounds on aviation riveted joints fatigue life. The goal of this work is to develop a method for the assessment of negative side effects caused by the application of corrosion preventive compounds. Tasks of the work are as follows: analysis of the aircraft corrosion problem; critical review of existing publications concerning possible negative side effects caused by the application of corrosion preventive compounds for protection of aviation riveted joints against corrosion, where reduction of the fatig

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Wang, Bin, Chuanyong Hao, Jinsong Zhang, and Hongyan Zhang. "A New Self-Piercing Riveting Process and Strength Evaluation." Journal of Manufacturing Science and Engineering 128, no. 2 (2005): 580–87. http://dx.doi.org/10.1115/1.2137746.

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Self-piercing riveting (SPR) has become an important alternative joining technique for the automotive applications of aluminum sheets. Most existing SPR machines use electrical motors to drive a rivet into the sheets. A significant amount of research has been conducted to improve an SPR joint’s strength by increasing the mechanical interlock. In this paper, a new process is presented using gunpowder to drive the riveting process. A joint formed using the new process has different geometric characteristics from one created using a conventional system. The tensile-shear, cross-tension, fatigue,

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