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Relevant bibliographies by topics / Riveted joints / Dissertations / Theses

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Dissertations / Theses on the topic 'Riveted joints'

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Published: 4 June 2021

Last updated: 25 July 2025

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1

Kecelioglu, Galip. "Stress And Fracture Analysis Of Riveted Joints." Master's thesis, METU, 2008. http://etd.lib.metu.edu.tr/upload/12610132/index.pdf.

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The objective of this study is to model and analyze a three dimensional single riveted lap joint (with and without a crack). By using finite element method, stress and fracture analyses are carried out under both the residual stress field and external tensile loading. Using a two step simulation, riveting process and subsequent tensile loading of the lap joint are simulated to determine the residual and overall stress state. Residual stress state due to riveting is obtained by interference and clamping misfit method. By employing different interference and clamping misfit values, the effects o

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2

Garcia, Abilio Neves. "Multiple site damage of aeronautical riveted joints." Thesis, Cranfield University, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.427165.

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3

Han, Li. "Mechanical behaviour of self-piercing riveted aluminium joints." Thesis, University of Hertfordshire, 2003. http://hdl.handle.net/2299/14159.

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The introduction of alternative materials and in particular aluminium alloys, for vehicle body applications has impelled the development of new joining techniques. Traditional joining methods such as spot-welding and arc-welding are being challenged. Self-piercing riveting has attracted considerable interest by the automotive industry and has been used as an alternative to spot-welding in vehicle body assembly. However, self-piercing riveting is a relatively new joining method and as such it is not well understood. The aim of this project was therefore to develop an understanding of the mechan

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4

Abdulla, Warda Ibrahim. "FATIGUE BEHAVIOR AND SCALE EFFECTS IN RIVETED JOINTS." University of Akron / OhioLINK, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=akron161651595564376.

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5

Scott, Jason P. "Corrosion and multiple site damage in riveted fuselage lap joints." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp04/mq22127.pdf.

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6

Scott, Jason P. (Jason Philip) Carleton University Dissertation Engineering Mechanical and Aerospace. "Corrosion and multiple site damage in riveted fuselage lap joints." Ottawa, 1997.

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7

Ioannou, John. "Mechanical behaviour and corrosion of interstitial-free steel-aluminium alloy self-piercing riveted joints." Thesis, University of Hertfordshire, 2010. http://hdl.handle.net/2299/4611.

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The overall aim of the project is to examine the rivetability of new steels and to investigate the mechanical behaviour of self-piercing riveted (SPR) aluminium-steel hybrid structures for automotive applications. Interstitial Free Steel (I.F.) of 1.2 mm thickness was joined to Aluminium 5754 of 2 mm thickness and Aluminium 5182 (coated and uncoated) of 1.5 mm thickness. The work began by initially conducting a quality assessment of the various joints that were produced in order to establish the optimum conditions for joining the various sample combinations to be investigated. A relationship w

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8

Bajracharya, Bijay Cheraghi Hossein Krishnan Krishna. "Effect of variations of riveting process on the quality of riveted joints." Diss., Click here for available full-text of this thesis, 2006. http://library.wichita.edu/digitallibrary/etd/2006/t085.pdf.

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Thesis (M.S.)--Wichita State University, Dept. of Industrial and Manufacturing Engineering.<br>" December 2006." Title from PDF title page (viewed on January 29, 2007). Thesis advisers: Hossein Cheraghi, Krishna Krishnan. Includes bibliographic references (leaves 62-64).

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9

Atre, Amarendra. "A Finite Element and Experimental Investigation on the Fatigue of Riveted Lap Joints in Aircraft Applications." Diss., Georgia Institute of Technology, 2006. http://hdl.handle.net/1853/10494.

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Aircraft fuselage skin panels are joined together by rivets. The initiation and propagation of fatigue cracks in aircraft structures at and around the rivet/skin interface is directly related to residual stress field induced during the riveting process and subsequent service loads. Variations in the manufacturing process, such as applied loading and presence of sealant can influence the induced residual stress field. In previous research, the riveting process has been simulated by a 2D axisymmetric force-controlled analysis. The 2D analysis cannot capture the unsymmetrical residual stress stat

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10

Borba, Natascha Zocoller [Verfasser]. "Design and mechanical integrity of friction riveted joints of thermoplastic composite / Natascha Zocoller Borba." Hamburg : Universitätsbibliothek der Technischen Universität Hamburg-Harburg, 2020. http://d-nb.info/1219963526/34.

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11

Faishal, Kazi Aman Ullah M. Cheraghi S. Hossein. "Impact of riveting sequence, pitch and gap between sheets on quality of riveted lap joints." Diss., A link to full text of this thesis in SOAR, 2006. http://soar.wichita.edu/dspace/handle/10057/645.

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Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Industrial and Manufacturing Engineering.<br>"December 2006." Title from PDF title page (viewed on Oct 31, 2007). Thesis adviser: S. Hossein Cheraghi. Includes bibliographic references (leaves 63-64).

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12

Arbex, Alexandra Alvim. "Análise estrutural e de fadiga de juntas rebitadas de uso aeronaútico utilizando o método dos elementos finitos /." Guaratinguetá : [s.n.], 2011. http://hdl.handle.net/11449/97053.

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Orientador: Fernando de Azevedo Silva<br>Banca: José Elias Tomazini<br>Banca: Silvana Aparecida Barbosa<br>Resumo: Juntas rebitadas sobrepostas representam elementos críticos na construção de estruturas aeronáuticas quando projetadas à fadiga. Por serem elementos de fixação largamente utilizados na indústria aeronáutica, o estudo de suas propriedades e variáveis à fadiga tem sido cada vez mais amplo. A variável que tem mostrado possuir alta influência na resistência à fadiga de juntas rebitadas é a força de aperto aplicada no processo de rebitagem. A vida da peça tende a ser maior quando o val

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13

Arbex, Alexandra Alvim [UNESP]. "Análise estrutural e de fadiga de juntas rebitadas de uso aeronaútico utilizando o método dos elementos finitos." Universidade Estadual Paulista (UNESP), 2011. http://hdl.handle.net/11449/97053.

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Made available in DSpace on 2014-06-11T19:28:33Z (GMT). No. of bitstreams: 0 Previous issue date: 2011-12-15Bitstream added on 2014-06-13T18:57:54Z : No. of bitstreams: 1 arbex_aa_me_guara.pdf: 3130393 bytes, checksum: e1c62358ab112fd781ed4b9dfabf900d (MD5)<br>Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)<br>Juntas rebitadas sobrepostas representam elementos críticos na construção de estruturas aeronáuticas quando projetadas à fadiga. Por serem elementos de fixação largamente utilizados na indústria aeronáutica, o estudo de suas propriedades e variáveis à fadiga tem sid

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14

Langrand, Bertrand. "Contribution a la caractérisation numérique et expérimentale d'assemblages structuraux rivetés sous sollicitation dynamique." Valenciennes, 1998. https://ged.uphf.fr/nuxeo/site/esupversions/be7d3137-d768-41f5-89ac-e08bad40b081.

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Dans le cadre de la conception des structures aéronautiques et de la modélisation de leur tenue mécanique, la représentation des comportements non linéaires locaux conduisant à la rupture est nécessaire et notamment ceux des liaisons. Ainsi en situation de crash survivable, les liaisons sont soumises à des charges dynamiques qui peuvent conduire à la rupture et à la désarticulation. Pour caractériser la tenue au crash des assemblages rivetés, une méthodologie dite de plans d'expérience numériques est proposée ; son intérêt est de limiter le cout des procédures expérimentales. Fondée sur les te

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15

Ali, Mohamad. "Assemblages structuraux des convertisseurs de puissance." Thesis, Toulouse, INPT, 2009. http://www.theses.fr/2009INPT003H/document.

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L'accroissement des performances des équipements de Traction ferroviaire, reposait essentiellement jusqu'à maintenant, sur l'intégration des innovations dans le domaine des composants électriques et des matériaux diélectriques mais la standardisation de sous-ensembles réutilisables nous conduit à reconsidérer les assemblages structuraux des coffres de traction (convertisseurs de puissance). Ces coffres de traction sont assemblés actuellement avec des éléments de fixation mécanique (boulon, rivet), le but est donc d'améliorer la connaissance des comportements mécaniques de ces types d'assemblag

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16

Carunchio, André Ferrara. "Análise numérica e experimental de juntas aeronáuticas rebitadas sob solicitação estática." Universidade de São Paulo, 2015. http://www.teses.usp.br/teses/disponiveis/3/3151/tde-12052016-144600/.

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Uniões por prendedores são elementos amplamente utilizados na indústria aeronáutica para a união de partes constituintes da aeronave. Contudo, devido à sua geometria e aos carregamentos sofridos, estes elementos estão frequentemente sujeitos a falhas por fadiga. Assim, para um projeto e dimensionamento bem executado dessas juntas, é necessário conhecer seu comportamento mecânico e o campo de tensões ao qual estão sujeitas. O método dos elementos finitos certamente atende a estas necessidades; porém, o uso de elementos sólidos tridimensionais para a representação destas uniões pode levar a anál

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17

Kim, Jueseok. "Linear Finite Element Modeling of Joined Structures with Riveted Connections." University of Cincinnati / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1563273473791073.

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18

Adámek, Petr. "Kritéria hodnocení únavové životnosti nýtových spojů." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2015. http://www.nusl.cz/ntk/nusl-232022.

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This thesis describes proposal of a methodology for evaluating fatigue life of riveted joints. The first section summarizes the theory used to evaluate fatigue life, description of the structure of operation load spectra and construction principles for the design joints for optimum durability. The second part of the thesis focuses on the proposal of a methodology enabling analytical solutions in closed form suitable for the initial structural design and also numerical solutions for use in detailed analyzes of the structure. The applicability of the methodology is demonstrated on an example of

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19

Krishnappa, Uma Shankar. "Numerical investigation of self-piercing riveted dual layer joint." Thesis, Wichita State University, 2008. http://hdl.handle.net/10057/2105.

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Self-piercing riveting (SPR) is a high-speed mechanical fastening technique for point joining of sheet-material components. SPR is becoming important in automotive applications for aluminium vehicle body assembly. However, compared with current sheet-metal joining processes in the automotive industry, the effects of various parameters such as mechanical properties, rivet setting methods and systems, methods of removing self-piercing rivets, etc. A study examining the effect of specimen configuration on the mechanical behavior of self-piercing riveted, dual-layer joints in aluminium alloys was

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20

Krishnappa, Uma Shankar Lankarani Hamid M. "Numerical investigation of self-piercing riveted dual layer joint." A link to full text of this thesis in SOAR, 2008. http://hdl.handle.net/10057/2105.

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Wichita State University, College of Engineering, Dept. of Mechanical Engineering.<br>Copyright 2008 by Uma Shankar Krishnappa. All Rights Reserved. Includes bibliographical references (leaves 51-53).

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21

Bijju, Manikanta. "Failure analysis of self-piercing riveted joint under different loading conditions using finite element method." Thesis, Wichita State University, 2010. http://hdl.handle.net/10057/3666.

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In a structure, a joint is considered as the weakest part, and it should not get separated when subjected to loading, so that an unstable collapse of structure can be avoided. It is important to investigate the failure in joint before it is used in a structure. Failure of a joint depends on various factors such as the geometry of joint configuration, sheet strength that are joined, rivet material used, cracks developed during joining, and many other. Self-Piercing riveting process is a new technology for joining sheet metals in automobile and aircraft industries. This process has many advantag

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22

Robidoux, Sébastien. "Influence des techniques d'assemblage sur la vie en fatigue des joints rivetés soumis à des charges variables." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1998. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp03/MQ38704.pdf.

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23

Жигилій, Дмитро Олексійович, Дмитрий Алексеевич Жигилий, Dmytro Oleksiiovych Zhyhylii, С. Н. Демченко та М. В. Акименко. "Розрахунок несучої здатності заклепкового з'єднання". Thesis, Сумський державний університет, 2014. http://essuir.sumdu.edu.ua/handle/123456789/40257.

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Заклепкові з‘єднання є нероз'ємними. Таке з‘єднання утворюють розклепуванням стержня заклепки, що вставлено в отвір деталі. При розклепуванні внаслідок пластичних деформацій утворюється замикальна головка, а стержень заклепки заповнює зазор в отворі.

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24

Ahmed, Abubaker Ali Tan Tein-Min. "Initiation and growth of multiple-site damage in the riveted lap joint of a curved stiffened fuselage panel : an experimental and analytical study /." Philadelphia, Pa. : Drexel University, 2007. http://hdl.handle.net/1860/1560.

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25

Weimer, William Eugene. "Corrosion of Magnesium, Aluminum, and Steel Automotive Sheet Metals Joined by Steel Self-Pierce Rivets." The Ohio State University, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=osu1420818436.

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26

Soares, Henrique Nogueira. "Detecção por raios-x de trincas de fadiga em juntas rebitadas de Glare&reg." Universidade de São Paulo, 2007. http://www.teses.usp.br/teses/disponiveis/88/88131/tde-09042008-150513/.

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Foi realizado um estudo comparativo da capacidade de duas variantes do método de radiografia por raios- X em detectar trincas de fadiga em juntas sobrepostas rebitadas de laminado híbrido metal-fibra Glare® de uso aeronáutico. Durante os ensaios mecânicos de fadiga sob amplitude constante de tensão, diversos corpos de prova rebitados foram periodicamente inspecionados por raios-X, em ambas as modalidades convencional e digital. Raios-X em filmes convencionais digital. Raios-X em filmes convencionais proporcionaram ótimo detalhamento de trincas nas juntas mecânicas, enquanto que as imagens

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27

Giorgobiani, Ioseb. "Optimální modelování nýtového spoje pomocí metody konečných prvků." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2020. http://www.nusl.cz/ntk/nusl-417911.

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Diplomová práce je zaměřena na optimální modelování nýtového spoje pro tři různé konfigurace pomocí metody konečných prvků v programu MSC. Nastran/Patran. Na základě prezentovaných výsledků je možné virtuálně simulovat chování nýtových spojů při zatížení, za účelem správného návrhu před provedením statických pevnostních zkoušek. Použitím těchto MKP simulací v procesu certifikace výrobku lze významně redukovat časovou i finanční náročnost pevnostních zkoušek. Při lepším porozumění chování konstrukce lze také lépe predikovat reálnou únosnost nýtových spojů.

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28

Siemssen, Brandon Raymond. "Development and Characterization of Friction Bit Joining: A New Solid State Spot Joining Technology Applied to Dissimilar Al/Steel Joints." Diss., CLICK HERE for online access, 2008. http://contentdm.lib.byu.edu/ETD/image/etd2425.pdf.

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29

Краснопольський, Володимир Сергійович, та Volodymyr Serhiyovych Krasnopol'skii. "Прогнозування граничного стану заклепкових з'єднань авіаційних конструкцій при втомному багатоосередковому пошкодженні". Thesis, Національний авіаційний університет, 2020. https://er.nau.edu.ua/handle/NAU/44136.

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Дисертаційна робота присвячена вирішенню актуальної задачі – визначення надійності та ресурсу заклепкових з’єднань панельних авіаційних конструкцій при багатоосередковому пошкодженні. Дана задача вирішена шляхом наукового обґрунтування та розробки нового математичного забезпечення для моделювання процесів утворення та росту втомних тріщин в конструкціях з отворами із алюмінієвого сплаву Д16АТ з врахуванням експериментально встановлених закономірностей. При циклічному навантажуванні конструкцій літаків у заклепкових з'єднаннях утворюються та розповсюджуються тріщини втоми, що може привести до

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30

Mohanty, Ramesh Chandra. "Damping of Layered and Jointed Beams with Riveted Joints." Thesis, 2010. http://ethesis.nitrkl.ac.in/2799/1/PhD_thesis_50703001.pdf.

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The present investigation highlights the effect of interfacial slip on the damping of layered cantilever beams jointed with rivets undergoing free vibration. The inclusion of mechanical joints bears a strong influence in the overall system performance and behavior, particularly the damping level of the structures. In fact, the damping and its improvement in machines or structures are one of the biggest challenges to the practicing engineers. Usually, such structures inherently possess low structural damping necessitating the introduction of additional measures to improve their damping characte

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31

dasari, sahitya. "Damping of structures with riveted joints." Thesis, 2012. http://ethesis.nitrkl.ac.in/3942/1/SAHITYA_FINAL_THESIS.pdf.

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The main purpose of the structural design is to restrict the vibration of structures at a desirable level as per requirements.Usually, structures inherently possess low structural damping necessitating the introduction of additional measures to improve their damping characteristics in order to control the harmful effects of vibration in normal operating conditions. In fact, most monolithic structures possess low inherent damping thereby causing serious problems which will impair the function and life of structures leading to their ultimate failure. It is always desirable to keep the vibration

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32

Chinthapatla, Nikhil. "Damping of composite materials with riveted joints." Thesis, 2012. http://ethesis.nitrkl.ac.in/3775/1/Nikhil-108ME053.pdf.

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Vibration and noise reduction are crucial in maintaining high performance level and prolonging the useful life of machinery, automobiles, aerodynamic and spacecraft structures. It is observed that damping in materials occur due to energy release due to micro-slips along frictional interfaces and due to varying strain regions and interaction between the metals. But it was found that the damping effect in metals is quite small that it can be neglected. Damping in metals is due to the micro-slips along frictional interfaces. Composites, however, have better damping properties than structural meta

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33

Pavankumar, Vodnala. "Damping of machine tool structures with riveted joints." Thesis, 2011. http://ethesis.nitrkl.ac.in/2721/1/PAVAN-THESIS.pdf.

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Light weight structures typically have low inherent structural damping. The damping mechanism of jointed and riveted structures can be explained by considering the energy loss due to friction and the dynamic slip produced at the interfaces. The frictional damping is evaluated from the relative slip between the jointed interfaces and is considered to be the most useful method for investigating the structural damping. The damping characteristics in jointed structures are influenced by the intensity of pressure distribution, micro-slip and kinematic coefficient of friction at the interfaces and t

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34

Moreira, Pedro Miguel Guimarães Pires. "A contribution to the study of fatigue of riveted lap joints." Master's thesis, 2004. http://hdl.handle.net/10216/12365.

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Dissertação apresentada para obtenção do grau de Mestre em Engenharia Mecânica, na Faculdade de Engenharia da Universidade do Porto, sob a orientação dos Professores Paulo M.S.T. de Castro e Artur Portela

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Moreira, Pedro Miguel Guimarães Pires. "A contribution to the study of fatigue of riveted lap joints." Dissertação, 2004. http://hdl.handle.net/10216/12365.

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Dissertação apresentada para obtenção do grau de Mestre em Engenharia Mecânica, na Faculdade de Engenharia da Universidade do Porto, sob a orientação dos Professores Paulo M.S.T. de Castro e Artur Portela

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36

Bajracharya, Bijay. "Effect of variations of riveting process on the quality of riveted joints." Thesis, 2006. http://hdl.handle.net/10057/432.

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This thesis presents a study of the effect of controllable riveting parameters, mainly squeeze force, rivet length, rivet diameter tolerance, hole countersunk depth and hole diameter tolerance, on the quality of formed rivet. The quality of a formed rivet is determined by the geometry of its head formation and the extent to which the hole is filled. The study determines maximum allowable tolerance on drilled hole in a 0.064” thick aluminum sheet for a 1/8” rivet. The study is performed using finite element simulation of the riveting process. Theoretical relations between squeeze force and form

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37

Faishal, Kazi Aman Ullah Mohammad. "Impact of riveting sequence, pitch and gap between sheets on quality of riveted lap joints." Thesis, 2006. http://hdl.handle.net/10057/645.

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This thesis presents a study on the effect of controllable process parameters in riveting (i.e., such as the sequence of riveting, distance between rivets (pitch) and gap between sheets) on the quality of riveted lap joint and formed rivet. The quality of a riveted lap joint is characterized by sheet metal bulging, sheet material growth, residual stress level on sheets and rivets, and post riveting clearance in the joint. The quality of a formed rivet is often determined by the geometry of its head formation. This study is to determine the best riveting sequence for riveted lap joint in sheet

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38

Girard, Samuel. "Étude expérimentale et modélisation de joints composites collés, rivetés et hybrides." Thèse, 2016. http://depot-e.uqtr.ca/7842/1/031262083.pdf.

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39

Chen, Chun-Hung, and 陳俊宏. "Mechanical properties of new model riveted bolt applying in single-lapped joint of nanocomposite laminates." Thesis, 2008. http://ndltd.ncl.edu.tw/handle/51918446632969818771.

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碩士<br>中華技術學院<br>飛機系統工程研究所<br>96<br>The purpose of this proposal is first to develop the new model riveted bolt that includes two functions such as 1 the components are nailed by a riveted joint at one side working, 2 the parts are fastened by the thread of bolt and nut with twisting way. Combining the advantages of two functions effectively fabricates a rigid joint to fix the connection of the specimen-lapped. And, the design of new load cell was obtained the clamping force of the joint as applying the torque by using new model riveted bolt. Then, the carbon fiber/epoxy (TC35/Y15037P) prepregs

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