Autor: Derewońko, A. - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Failure Simulation of Metal-Composite Joints
Symulacje zniszczenia połączenia metalowo-kompozytowego
Autorzy:: Derewońko, A.
Powiązania:: https://bibliotekanauki.pl/articles/232218.pdf
Data publikacji:: 2013
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Biopolimerów i Włókien Chemicznych
Tematy:: failure
metal-composite bonded joint
finite element method (FEM)
awaria
metalowo-kompozytowe połączenia
metoda elementów skończonych (MES)
Opis:: The paper presents a numerical analysis method allowing the determination of the degree of failure of an adhesive joint with the use of CAE software. The results of an experimental test are used to describe properties of the joint parts. Described herein is the behaviour of a multi-stepping lap joint of metal with a multilayered fibre composite that is often used in the aircraft industry. Modelling of the contact problem between the metal surface and layer of the composite enables determination of the value of the external tensile load at which the process of failure of the joint begins. The author also proposes a simple method to shape solid finite elements which allows the elimination of the singularity around finite element vertices. The method has been applied to numerical analysis of the joint, in which the layers were stacked at various angle orientations. The influence of the step length of the metal part on the joint strength was also considered. The results of numerical analysis were compared with those of experimental investigations of the joint strength, giving satisfactory agreement.
W pracy przedstawiono metodę analizy numerycznej umożliwiającej określenie stopnia zniszczenia połączenia przy użyciu oprogramowania CAE, z wykorzystaniem wyników testów eksperymentalnych. Opisano zachowanie trójstopniowego połączenia zakładkowego metalu z wielowarstwowym kompozytem włóknistym, które jest często wykorzystywane w przemyśle lotniczym. Odwzorowanie zagadnienia kontaktu między powierzchnią metalu i warstwą kompozytu pozwala określić wartość obciążenia zewnętrznego, przy którym rozpoczyna się proces niszczenia połączenia, który jest wywołany rozciąganiem. Zaproponowano sposób ukształtowania bryłowych elementów skończonych, który pozwala wyeliminować nieciągłości występujące w obszarach naroży. Metoda została zastosowana do analizy numerycznej połączenia, w którym wielowarstwowy laminat utworzono z prepregu ułożonego pod różnymi kątami. Przeanalizowano wpływ wymiarów stopnia części metalowej na wytrzymałość połączenia. Wyniki analiz numerycznych porównano z rezultatami badań eksperymentalnych uzyskując zadowalającą zgodność.
Źródło:: Fibres & Textiles in Eastern Europe; 2013, 5 (101); 131-134
1230-3666
2300-7354
Pojawia się w:: Fibres & Textiles in Eastern Europe
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 2.

Tytuł:: Carbon - epoxy composite fatigue strength - experiment and fem numerical estimation
Autorzy:: Derewońko, A.
Gieleta, R.
Powiązania:: https://bibliotekanauki.pl/articles/246504.pdf
Data publikacji:: 2012
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: fatigue strength
carbon-epoxy composite
FEM
Opis:: The development of composite materials characterized by the constant amelioration of their mechanical properties (stiffness and strength) has widened their application for structural elements, mainly in aeronautical, naval and automobile industries. The possibility of tailoring the composite’s properties appropriately to the applied load (by changing the direction of the fibre alignment and applying a corresponding matrix) results in the growing importance of the design process. The paper presents a numerical technique of determining the fatigue strength of the laminated carbon–epoxy composite. The experimental investigations were carried out to determine the complete set of the stiffness characteristics Eij, Gij, ..ij, the strength characteristics ..i,n, ..i,n. and the S-N fatigue curves. The static and fatigue numerical calculations were carried out for the material anisotropic model of the particular composite layers. Eight-node 3D finite elements with the composite’s properties were used to develop the specimen’s numerical model. The contact problem between the composite layers enabling the reflection of a mutual interaction was taken into account. The numerical investigation also included the state of effort analysis and the fatigue life assessment of the composite. The assessment of the composite’s fatigue life was performed using the MSC.Fatigue code. The verification of models and numerical analysis was carried out for composite specimens made of the CE 8201-245- 45/120 prepreg. The experimental verification confirmed that the places of the lowest fatigue life, found out in numerical analysis, are located in the area of the gauge part.
Źródło:: Journal of KONES; 2012, 19, 3; 103-110
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 3.

Tytuł:: Numerical analysis of the metal-composite joints
Autorzy:: Derewońko, A.
Cielęta, R.
Powiązania:: https://bibliotekanauki.pl/articles/243344.pdf
Data publikacji:: 2008
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: metal-composite joint
FEM
contact problem
nonlinearity
aircraft structure
Opis:: The development and implementation of the new technologies and materials are one of the conditions allowing improving the aircraft structures. The composite materials enable to reduce the aircraft weight and keep appropriate strength and fatigue properties. Application of the composite materials in the wing elements, and metal alloys in assemblies of the aircraft fuselage requires elaboration of the appropriate method for technology joining metal and composite. Bonding eliminates breakages in the composite plies which are initiated during assembly process of the structure with mechanically fastened joints e.g. bolts [1]. The strength and stiffness of the composite depend on shape and direction of the fibre which carry the tensile and compression stresses. Shear stress and strength of the composite depend on the resin system. Therefore, the use of composites brings more complicated design approach compare to metal. The aim of the study is tofind appropriate method to determine the failure loading of the metal-composite aircraft wing pivot fitting. Numerical and laboratory investigations for metal-composite joints are presented. Interaction between the composite plies is modelled as the contact problem. It allows determining the strain and stress at the contact surfaces and stress concentration fields. Contact modelling technique is also applied to model interface between metal and composite. Engineering approach to the model full-scale co-curing triple stepped lap joint is presented. The professional engineering software tools are used to create accurate models. Tensile tests of the metal-composite joint were carried out to verify the numerical analysis methods.
Źródło:: Journal of KONES; 2008, 15, 1; 39-50
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 4.

Tytuł:: Fatigue strength investigation of bonded joints
Autorzy:: Gieleta, R.
Derewońko, A.
Powiązania:: https://bibliotekanauki.pl/articles/243427.pdf
Data publikacji:: 2007
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: adhesive bonded joint
fatigue strength
non-linear analysis
Opis:: Numerous advantages of the bonded joints result in wide application in the aircraft, motor industry or powertrain components. These types of joints enable joining materials with different mechanical properties (e.g. Stiffness) and dimensions without structure change. Proper joint design limits the field of local stress concentrations or even eliminates them. The structural integrity of complete structure depends on the fatigue estimation of the bonded joint. Application of the finite element method to life prediction of the double lap bonded joint metal-composite-metal is presented. Three dimensional numerical models are generated by professional engineering software tools. The contact problem is modelled between the epoxy resin and metal and composite surfaces. A laminated composite consists of the epoxy woven carbon prepreg. Elasto-plastic materials models of the adhesion and metal and orthotropy composite model allowed determining the contact normal stress in the interfaces in each deformation increment which is induced by an external load. MSC.Marc was used to determine the strain and stress distribution in the double lap bonded joint including contact normal stress in the steel/adhesive and laminated composite/adhesive interfaces. Two numerical models of the double lap bonded joint were compared. The use of the presented method is more suitable for structure optimisation than numerical analysis.
Źródło:: Journal of KONES; 2007, 14, 3; 177-186
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 5.

Tytuł:: Analysis of residual stress fields in the riveted joint
Autorzy:: Szymczyk, E.
Jachimowicz, J.
Derewońko, A.
Powiązania:: https://bibliotekanauki.pl/articles/243089.pdf
Data publikacji:: 2007
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: riveted joint
FEM local model
non-destructive testing methods
Opis:: The riveted joints are critical areas of the aircraft structure. The residual stress and strain state appears at the rivet hole after the riveting process and improves fatigue behaviour of the joint. Numerical FE simulations of the upsetting process are carried out using the MARC code. Three-dimensional numerical models are used to determine the resulting stress and strain fields at the countersunk rivet and around the hole. The contact with friction is defined between the mating parts of the joint. Calculations are carried out in an elastic-plastic range. The influence of the rivet geometry, rivet stiffness and the sheet material model on strain and stress states is studied. Non-destructive testing methods like X-ray diffraction, liquid penetrant inspection and visual detection analysis with a UV lamp are used for validation of numerical results. Comparison between numerical and experimental results gives a satisfactory agreement. Numerical simulations allow investigating the influence of imperfections on the strength of the joint.
Źródło:: Journal of KONES; 2007, 14, 2; 465-473
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 6.

Tytuł:: Experimental and numerical verification of the pontoon bridge section
Autorzy:: Chłus, K.
Derewonko, A.
Krasoń, W.
Powiązania:: https://bibliotekanauki.pl/articles/244277.pdf
Data publikacji:: 2013
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: pontoon bridge section
demonstrator of construction
verification of numerical analysis
Opis:: The object of the paper is experimental and numerical verification of a pontoon bridge prototype section. The main part of a single segment is a waterproof cassette which contains a shell (pontoon). After filling with the air, the pontoon assures the required buoyancy. The cassette, in which the shell is located, has a movable bottom. Pontoon bridges are built of ready-to-use repeatable segments and they may be used as temporary crossings. Verification of the bridge modules was performed by launching a demonstrator compound of two modules of the pontoon bridge section, filling the pontoons with air and measuring their immersion. The test was performed in the pool, in the Military Engineering Works. S.A. (WZInż. S.A.) in Deblin. Recording and measurements were performed with two Phantom V12 cameras placed on static tripods. It allowed reading from each of the cameras the heights of the midpoints of the prow and the starboard above the water surface, and the inclination angle of the pontoon unit in transverse and longitudinal planes. The combination of these results allowed calculation of height of the roadway centre of pontoons set above the water surface. Displacement and stability of the structure was specified based on analytical calculations. This paper presents the results of numerical calculations of launching a pontoon bridge section demonstrator. Correctness of the numerical methods of calculation was examined based on a comparison of numerical and experimental results.
Źródło:: Journal of KONES; 2013, 20, 1; 35-40
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 7.

Tytuł:: TIG and laser beam welded joints – simplified numerical analyses
Autorzy:: Nasiłowska, B.
Derewońko, A.
Bogdanowicz, Z.
Powiązania:: https://bibliotekanauki.pl/articles/279511.pdf
Data publikacji:: 2018
Wydawca:: Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej
Tematy:: TIG
laser beam
welded joints
steel 904L
numerical analysis
residual stress
Opis:: Regardless of the welding method, a new joint and the surrounding area are inevitably subjected to thermo-physical perturbation. The paper presents analyses of many diﬀerent issues involved in welding and potential solutions including adoption of simplifying assumptions, application of numerical algorithms and development of reliable representative models. The Finite Element Method is used to determine residual stress distribution, using results from thermo-physical tests and widely known mechanical properties of metals subjected to welding processes. Experimental and numerical methods for determining residual stress are compared for welds generated using both TIG (Tungsten Inert Gas, Gas Tungsten Arc Welding) and a laser beam. This data reveals that it is necessary to precisely deﬁne location of the analyzed welded fragment to correctly determine thermal boundary conditions.
Źródło:: Journal of Theoretical and Applied Mechanics; 2018, 56, 3; 645-656
1429-2955
Pojawia się w:: Journal of Theoretical and Applied Mechanics
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 8.

Tytuł:: Modeling of the shock wave impact on the flexible shell
Autorzy:: Derewonko, A.
Szurgott, P.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/238097.pdf
Data publikacji:: 2009
Wydawca:: Instytut Technologii Bezpieczeństwa Moratex
Tematy:: elastyczne powłoki
modelowanie fali uderzeniowej
fala uderzeniowa
shock wave
flexible coating
modeling of shock wave
Opis:: An underwater explosion is one of the possible threat which can occure during military operations and/or civilian usage. The ballistic protection systems are the method to reduce the impact of the high explosive (HE) charge blast wave. The aim of this paper is to present the influence of the shock wave on the flexible shell. The simulation of the underwater detonation is provided with use of the Finite Element Method (FEM). The influence of the distance between the HE charge and the flexible shell on its deformation was estimated. The results of the conducted analysis including explosion were compared with those obtained for the basic model with no explosion.
Źródło:: Techniczne Wyroby Włókiennicze; 2009, R. 17, nr 2/3, 2/3; 107-111
1230-7491
Pojawia się w:: Techniczne Wyroby Włókiennicze
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 9.

Tytuł:: Pneumatic air object application in design of water crossing
Autorzy:: Derewońko, A.
Kołodziejczyk, D.
Golczak, K.
Powiązania:: https://bibliotekanauki.pl/articles/241775.pdf
Data publikacji:: 2012
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: cassette pontoon bridge
numerical analysis
transport infrastructure
air pollution
pneumatic airbag
Opis:: The results of numerical analysis of the decomposing process of a single pneumatic cassette pontoon bridge as a temporary roadway are presented in the paper. The cassette pontoon bridge is an innovative solution designed for quick assembly of the construction on water. The repeatability of a single module, facility of transportation and operation mean that it can be used in many applications: crossings for military vehicles (e.g. tanks or wheeled vehicles lightarmoured), replacement crossing for trucks (e.g. delivering materials for the construction of the permanent bridge), ribbons replacing flooded roads and footbridges on suddenly increased watercourses. The main problem in our consideration is single cassette pontoon stability at the moment of filling the pontoon. The numerical investigations presented in the present paper aimed at testing the influence of the load on the process of filling the single cassette pontoon. To perform the analyses, LS-DYNA software, in which the dynamic equations of motion are solved using an explicit time integration method, was used. The paper presents initial verification of the initial conditions influence on the process of filling the single cassette pontoon. An important factor considered in the work is a strong influence of an unbalanced load distribution on the surface of the cassette capacity on the process of filling the pontoon.
Źródło:: Journal of KONES; 2012, 19, 4; 155-161
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 10.

Tytuł:: Device supporting military vehicles buoyancy and ballistic resistance
Autorzy:: Derewońko, A.
Sławiński, G.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/244644.pdf
Data publikacji:: 2011
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: FEM
ballistic protection
buoyancy
military vehicles
panels
elasto-plastic
Opis:: A deep modernization of equipment due to its assembling to the modern requirements of a battlefield and getting full compatibility to NATO structures caused that some military vehicles equipment with additional staff lose their buoyancy or are at the edge of losing it. The solution to this problem can be setting an additional device which helps to increase mass that allows to keep buoyancy of a military vehicle. The panels are fixed as the outer elements of the container which is simultaneously used for storing the elastic air cushions. Before the water crossing, the air cushions are filled with gas and additional buoyancy force is generated. The paper presents a structure and usage of a multipurpose ballistic protection which, in the passive state, is an additional armour and in the unfolded state increases buoyancy lost in the case of setting additional devices or armament. In the paper, initial simulations developed with the use of Ls-Dyna software are described. The influence of modules number of the air cushion on the buoyancy of the multi-purpose ballistic protection is considered. The advantage of the solution is possibility of the chamber volume change which causes the increase of device volume of the whole module of the chambers is dependent on the vehicle buoyancy which results from its current weight.
Źródło:: Journal of KONES; 2011, 18, 1; 129-134
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 11.

Tytuł:: Numeryczne modelowanie zagadnienia kontaktu w procesie spęczania nitu
Numerical modelling of a contact problem in the rivet upsetting process
Autorzy:: Derewońko, A.
Szymczyk, E.
Jachimowicz, J.
Powiązania:: https://bibliotekanauki.pl/articles/208471.pdf
Data publikacji:: 2006
Wydawca:: Wojskowa Akademia Techniczna im. Jarosława Dąbrowskiego
Tematy:: MES (metoda elementów skończonych)
proces nitowania
zagadnienie kontaktu
połączenia nitowe
FEM
riveting process
contact problem
riveted joint
Opis:: Celem pracy jest dobór modelu numerycznego (właściwej siatki elementów skończonych) zapewniającego prawidłowe odwzorowanie współpracy kontaktujących się powierzchni nitu i blachy w procesie spęczania trzpienia nitu. Stanowi ona jeden z etapów badania lokalnych zjawisk fizycznych w połączeniach nitowych lotniczych konstrukcji cienkościennych [1-8]. Analizy z uwzględnieniem zagadnienia kontaktu i dużych odkształceń wykonano metodą elementów skończonych w programie MSC.Marc. Wyniki obliczeń numerycznych porównano z wartościami sił i naprężeń oszacowanymi analitycznie dla spęczanego swobodnego walca. Uzyskane numerycznie rozkłady naprężeń i odkształceń są zgodne z prezentowanymi w literaturze [13], co wskazuje, że proces zakuwania trzpienia nitu został odwzorowany poprawnie. Deformacje powierzchni kontaktu na granicy nitu i blachy wykazują dużą wrażliwość na parametry siatki elementów skończonych. Właściwy sposób podziału współpracujących brył na elementy skończone pozwala uniknąć wzajemnego przenikania węzłów, a tym samym niefizycznych koncentracji naprężeń w obszarze kontaktu.
The paper deals with numerical simulation of rivet upsetting in a hole. The work is aimed at a choice of numerical model (proper finite element mesh) that ensures suitable behaviour of the rivet and sheet hole surfaces during rivet's upsetting process. This is preliminary stage of an analysis of the local physical phenomena in the riveted joints of an aircraft structure. A contact problem and large strains are taken into consideration in FEM analysis performed with MARC code. Numerical results are compared with analytical estimations for upsetting a cylindrical specimen. Numerical stress and strain fields show that squeezing the rivet shank is correctly described. The deformations of contact surface between the rivet and the hole are sensitive on finite element mesh parameters. Due to appropriate meshing of the mating components, mutual node penetration and consequently, non-physical stress concentration on the contact surfaces can be avoided.
Źródło:: Biuletyn Wojskowej Akademii Technicznej; 2006, 55, 4; 89-100
1234-5865
Pojawia się w:: Biuletyn Wojskowej Akademii Technicznej
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 12.

Tytuł:: Szacowanie stabilności modułu pontonowego mostu kasetowego
Stabilility estimation of a single segment of a pontoon bridge
Autorzy:: Derewońko, A.
Niezgoda, T.
Sławiński, G.
Powiązania:: https://bibliotekanauki.pl/articles/209847.pdf
Data publikacji:: 2011
Wydawca:: Wojskowa Akademia Techniczna im. Jarosława Dąbrowskiego
Tematy:: mechanika
stabilność
fala uderzeniowa
most pontonowy
moduł kasetonowy
mechanics
stability
shock wave
pontoon bridge
single segment
Opis:: System pontonowego mostu kasetowego umożliwia zestawienie przeprawy przez przeszkodę wodną dla ludzi i sprzętu. Przeprawa powstaje jako dowolne złożenie powtarzalnych modułów pływających. Pojedynczy moduł mostu kasetowego stanowi szczelny prostopadłościan (kaseta) częściowo zanurzony w wodzie, którego siła wyporu jest zależna od ciężaru własnego. We wnętrzu kasety znajduje się powłoka, która może być pompowana gazem (powietrzem). W trakcie napełniania powłoki rosnące ciśnienie powoduje otwarcie dna kasety, a wzrastająca objętość powłoki skutkuje wzrostem siły wyporu. W pracy przedstawiono wstępne wyniki analiz, w których oceniono stabilność modułu kasetowego mostu pontonowego.
The cassette pontoon bridge enables river crossing for people and equipment. The cassette pontoon bridge is considered as an object assembled as any composition of the single buoyant segments. The single buoyant segment is a tight cuboid (cassette) which is partially immersed. The cassette buoyancy depends on weight of a cassette. The air cushion which can be filled with pressured air is stored inside the cassette. The buoyancy is caused by the air pressure increasing during filling the air cushion. The paper aims mainly at estimating the stability of a single segment of the pontoon bridge.
Źródło:: Biuletyn Wojskowej Akademii Technicznej; 2011, 60, 2; 243-251
1234-5865
Pojawia się w:: Biuletyn Wojskowej Akademii Technicznej
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 13.

Tytuł:: Thermal-mechanical coupled simulation
Autorzy:: Nguyen, H. P.
Derewońko, A.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/244229.pdf
Data publikacji:: 2015
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: thermo-mechanical coupled
simulation
plastic deformation
Opis:: Optimal design of engineering structures and technological processes requires taking into account various factors affecting the state of strain and stresses in the structure. Coupled thermo-mechanical analysis enables, among others, determination of undesirable changes in a body shape resulting from the implementation method of the initially-boundary conditions, for example, time-varying load and physical properties of the material depending on the temperature. They are also used to determine residual stresses remaining after manufacturing to prevent revalued stiffness and rigidity of the designed construction. In this study, coupled thermo-mechanical analysis illustrated by metal machining operation is presented. The commercial code MSC.Marc has been used to develop a coupled thermo-mechanical finite element model of plane-stress orthogonal metal cutting operations. Metal cutting is one of the most important and common manufacturing processes in the car industry. A thermal mechanical transient analysis is performed to convert mechanical work into heat by plastic deformation of the workpiece material and friction during metal machining operation. The finite element mesh distortion, due to large deformations, requires a remesh technique. The influence of parameters of the 2D and 3D finite element mesh adaptation on plastic deformation and temperature generated in the cutting processing is considered.
Źródło:: Journal of KONES; 2015, 22, 3; 161-168
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 14.

Tytuł:: Comparison of the dynamic riveting process of a rivet with and without a compensator
Autorzy:: Szymczyk, E.
Slawinski, G.
Jachimowicz, J.
Derewonko, A.
Powiązania:: https://bibliotekanauki.pl/articles/245374.pdf
Data publikacji:: 2009
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: riveted joint
mushroom rivet
FEM local model
deformation fields
Opis:: The paper deals with the analysis of deformation of a rivet hole in a riveted joint after the manual dynamic riveting process. For many years, riveting remains a traditional and the most popular method ofjoining in aircraft structures. The residual stress and strain state appear at the rivet hole after the riveting process, which improves the joint's fatigue behaviour. The local finite element models are made with Patran. The rivet and sheets are described using eight-noded, three-dimensional brick elements. The riveting tools consist of four-noded, two-dimensional shell elements. Numerical FE simulations of the upsetting process are carried out using the Ls-Dyna code. The contact with friction is defined between the collaborating parts of the specimen. The results of simulations of the dynamic riveting process of a mushroom rivet with and without a compensator are compared in this paper. Hole deformation of the upper and lower sheet, squeezing force, as well as deformations of the rivet head are analysed. The influence of the compensator on strain and displacement states is studied. Simulation shows that some technological factors may have positive influence on the residual stress fields. Using the rivet with a compensator results in a better rivet hole filling capability. The rivet hole displacement in upper and lower sheets are at the same level. Paper also present manual dynamic riveting process of reverse and standard riveting procedure and model of riveted specimen.
Źródło:: Journal of KONES; 2009, 16, 4; 455-462
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 15.

Tytuł:: Comparison of the dynamic riveting process of a rivet with and without a compensator
Autorzy:: Szymczyk, E.
Slawinski, G.
Jachimowicz, J.
Derewonko, A.
Powiązania:: https://bibliotekanauki.pl/articles/245575.pdf
Data publikacji:: 2009
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: riveted joint
mushroom rivet
FEM local model
deformation fields
Opis:: The paper deals with the analysis of deformation of a rivet hole in a riveted joint after the manual dynamic riveting process. For many years, riveting remains a traditional and the most popular method of joining in aircraft structures. The residual stress and strain state appear at the rivet hole after the riveting process, which improves the joint's fatigue behaviour. The local finite element models are made with Patron. The rivet and sheets are described using eight-noded, three-dimensional brick elements. The riveting tools consist of four-noded, two-dimensional shell elements. Numerical FE simulations of the upsetting process are carried out using the Ls-Dyna code. The contact with friction is defined between the collaborating parts of the specimen. The results of simulations of the dynamic riveting process of a mushroom rivet with and without a compensator are compared in this paper. Hole deformation of the upper and lower sheet, squeezing force, as well as deformations of the rivet head are analysed. The influence of the compensator on strain and displacement states is studied. Simulation shows that some technological factors may have positive influence on the residual stress fields. Using the rivet with a compensator results in a better rivet hole filling capability. The rivet hole displacement in upper and lower sheets are at the same level. Paper also present manual dynamic riveting process ofreverse and standard riveting procedure and model of riveted specimen.
Źródło:: Journal of KONES; 2009, 16, 3; 415-422
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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