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Tytuł:
Experimental Determination of the Mode I Fracture Toughness in FRP Laminates with Hybrid Delamination Interfaces
Autorzy:
Rzeczkowski, Jakub
Samborski, Sylwester
Prokopek, Katarzyna
Powiązania:
https://bibliotekanauki.pl/articles/2204947.pdf
Data publikacji:
2022
Wydawca:
Stowarzyszenie Inżynierów i Techników Mechaników Polskich
Tematy:
DCB test
hybrid laminates
fracture toughness
composite laminates
Opis:
This paper aims at experimental research of the effect of hybrid interface (carbon/glass fibers) on delamination resistance in unidirectional fiber reinforced polymer (FRP) composite laminates under the mode I opening load conditions. Three group of laminates exhibiting different combinations of reinforcing materials at delamination plane were tested. Critical strain energy release rates were determined by using the double cantilever beam (DCB) tests in accordance with the ASTM D5528 Standard. Values of the GIC were calculated by using classical data reduction schemes and they were compared with values obtained by using an alternative compliance based beam method (CBBM). For precise detection of delamination onset all tests were additionally supported by registration of the acoustic emission (AE) signal. Contribution of mixed-modes were evaluated by using numerical finite element analysis. Obtained outcomes revealed, that differences in the mode I c-SERR values obtained by using four different methods were insignificant. Moreover, the greatest value of the GIC was determined for laminates with hybrid interface and it was equal 0.24 N/mm.
Źródło:
Advances in Science and Technology. Research Journal; 2022, 16, 5; 129--135
2299-8624
Pojawia się w:
Advances in Science and Technology. Research Journal
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Postbuckling behaviour of laminated plates with a cut-out
Autorzy:
Falkowicz, K.
Dębski, H.
Powiązania:
https://bibliotekanauki.pl/articles/102047.pdf
Data publikacji:
2017
Wydawca:
Stowarzyszenie Inżynierów i Techników Mechaników Polskich
Tematy:
laminates
buckling
postbuckling
Finite Element Method
Opis:
The subject of research is the numerical and experimental analysis of a thin-walled plate with the cut-out, made of the laminate and subjected to the axial compression. In order to ensure the stable plate work in the postcritical range, it need to force its work by higher flexural-torsional form of buckling. The scope of the research included nonlinear numerical analysis with Finite Element Method (FEM) and experimental verification of calculation results. For the composite material in numerical calculations, the model of orthotropic material in the flat state of tension was defined. For the mapping of the plate element coating finite elements of type SHELL was applied with a shape function of the second order to allow the mapping of the composite structure for the element thickness. The experimental research was carried out in a special grips providing the articulated support of the upper and lower edges of the plate. The deformation registration of compression structures were carried out with resistance extensometry. This allowed to define of postcritical equilibrium paths of real structure, showing the dependence of the force to displacement. The instrument used was a numerical program ABAQUS®.
Źródło:
Advances in Science and Technology. Research Journal; 2017, 11, 1; 186-193
2299-8624
Pojawia się w:
Advances in Science and Technology. Research Journal
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Development and Assessment of Polymeric Laminate blended composites Reinforced with Bi-Woven Aramidic Fiber
Autorzy:
Amarababu, B.
Rangadu, V. P.
Powiązania:
https://bibliotekanauki.pl/articles/411638.pdf
Data publikacji:
2014
Wydawca:
Przedsiębiorstwo Wydawnictw Naukowych Darwin / Scientific Publishing House DARWIN
Tematy:
laminates
polymer blends
thermomechanical
chemical resistance
Opis:
In the present paper evaluates laminated aramidic bi-woven fibers reinforced in polyester-vinylester blended composites. The Duo polymers, polyester-vinylester were blended using in situ polymerization technique. Four planar layers were made simultaneously and keeping one over another and each layer make sure to be weighed off 15% were maintained in all layers with different orientations. Pre-assumed Layer-1(50/50) 50 %, 0º; Layer-2(35/35/30) 35 % 0º, 35 % +45º, 30 %,0; Layer-3 (25/50/25) 25 % 0º, 50% +45º, 25-45º; Layer-4 (25/25/25/25) (2 5% 0º, 25 % +45º, 25 % -45º, 25 % 90º). Tthe composite was prepared with the help of hand layup technique. Test ready specimens were the help of shearing machine in accordance with ASTM. It was observed that, polyester and vinylester had good miscibility makes combined solid material. Flexural strength, tensile strength was improved up to 3ed layer, decreases after, whereas flexural modulus and tensile modulus were linearly increased up to 4th layer. Thermal stability and glass transition temperature were also found satisfactory for all the laminated layers. Chemical resistance was good for the entire chemical except toluene.
Źródło:
International Letters of Chemistry, Physics and Astronomy; 2014, 19, 1; 99-110
2299-3843
Pojawia się w:
International Letters of Chemistry, Physics and Astronomy
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Preliminary studies of riveted joints at feed force
Autorzy:
Bielawski, R.
Kowalik, M.
Rządkowski, W.
Pyrzanowski, P.
Powiązania:
https://bibliotekanauki.pl/articles/102917.pdf
Data publikacji:
2015
Wydawca:
Stowarzyszenie Inżynierów i Techników Mechaników Polskich
Tematy:
laminates
damage mechanics
mechanical testing
joints
joining
Opis:
The aim of the study was to determine the feasibility of riveted joints in composites materials. Static tensile test method was used. In the test one type of glass fabric was used (Interglas 92140) from which two types of composite samples were prepared. In each sample the same type of fiber with the same fiber orientation – 3 layers - was used. The samples had dimensions of 100×100 mm and thickness of approximately 1 mm. The composite probes were located in a metal frame with a screw connection which was made of screws with nominal thread pitch M5. Screws were tightened with constant torque. It was to provide an axial force to the sample during the tensile test. The frame was placed between cross-bars of tensile machine INSTRON 8516. The samples were stretched at a speed of 0.05 mm/s at a distance up to 15 mm. During the tensile test displacement of the samples and pull force were registered. Depending on the fibre orientations and the value of feed force, damage models were described. On the basis of the results the possibility of usage of aluminium rivet nuts connections in composite materials was determined.
Źródło:
Advances in Science and Technology. Research Journal; 2015, 9, 27; 23-27
2299-8624
Pojawia się w:
Advances in Science and Technology. Research Journal
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Evaluation of Force-Time Changes During Impact of Hybrid Laminates Made of Titanium and Fibrous Composite
Autorzy:
Jakubczak, P.
Surowska, B.
Bieniaś, J.
Powiązania:
https://bibliotekanauki.pl/articles/352329.pdf
Data publikacji:
2016
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
hybrid composites
titanium-carbon laminates
impact
damage
Opis:
Fibre metal laminates (FML) are the modern hybrid materials with potential wide range of applications in aerospace technology due to their excellent mechanical properties (particularly fatigue strength, resistance to impacts) and also excellent corrosion resistance. The study describes the resistance to low velocity impacts in Ti/CFRP laminates. Tested laminates were produced in autoclave process. The laminates were characterized in terms of their response to impacts in specified energy range (5J, 10J, 20J). The tests were performed in accordance with ASTM D7137 standard. The laminates were subjected to impacts by means of hemispherical impactor with diameter of 12,7 mm. The following values have been determined: impact force vs. time, maximum force and the force at which the material destruction process commences (Pi). It has been found that fibre titanium laminates are characterized by high resistance to impacts. This feature is associated with elasto-plastic properties of metal and high rigidity of epoxy - fibre composite. It has been observed that Ti/CFRP laminates are characterized by more instable force during impact in stage of stabilization of impactor-laminate system and stage of force growth that glass fibre laminates. It has been observed more stable force decrease in stage of stress relaxation and withdrawal of the impactor. In energy range under test, the laminates based on titanium with glass and carbon fibres reinforcement demonstrate similar and high resistance to low-velocity impact, measured by means of failure initiation force and impact maximum force.
Źródło:
Archives of Metallurgy and Materials; 2016, 61, 2A; 689-694
1733-3490
Pojawia się w:
Archives of Metallurgy and Materials
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Damage Detection and Size Quantification of FML with the Use of NDE
Autorzy:
Dragan, K.
Kornas, Ł.
Kosmatka, M.
Leski, A.
Sałaciński, M.
Synaszko, P.
Bieniaś, J.
Powiązania:
https://bibliotekanauki.pl/articles/98012.pdf
Data publikacji:
2012
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:
fibre metal laminates
composites
non-destructive testing
Opis:
Composite materials have been developed in recent years. A new generation of structural composite materials for advanced aircraft is Fibre Metal Laminates (FML). They are hybrid composites consisting of alternating thin layers of metal sheets and fiber-reinforced composite material. FMLs have both low weight and good mechanical properties (high damage tolerance: fatigue and impact characteristics, corrosion and fire resistance). Quality control of materials and structures in aircraft is an important issue, also for Fibre Metal Laminates. For FML parts, a 100% non-destructive inspection for internal quality during the manufacturing process is required. In the case of FML composites, the most relevant defects that should be detected by non-destructive testing are porosity and delaminations. In this paper, a number of different non-destructive methods for the inspection of Fibre Metal Laminates were studied. The possibility of quality control of manufactured FML laminates - detection of defects as well as the procedures and processes are presented and discussed.
Źródło:
Fatigue of Aircraft Structures; 2012, 4; 5-9
2081-7738
2300-7591
Pojawia się w:
Fatigue of Aircraft Structures
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
The Influence of Material Configuration of Fibre-Metal Laminates with Alumina Core on Flexural Strength
Autorzy:
Frankiewicz, Mariusz
Karoluk, Michał
Dziedzic, Robert
Timmel, Tristan
Scholz, Peter
Powiązania:
https://bibliotekanauki.pl/articles/24201172.pdf
Data publikacji:
2022
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:
fibre-metal laminates
flexural strength
fatigue
composite materials
Opis:
Fibre metal laminates (FMLs) consisting of layers made of PA6 polyamide prepregs reinforced with glass and carbon fibres and an aluminium alloy core are the new variant of the other types used by aerospace FML materials such as GLARE or CARALL. By using a thermoplastic matrix, they can be shaped by stamping processes, which allows for a more efficient production process than classical laminating methods such as vacuum bagging. In addition to the improved impact energy absorption efficiency, the metallic core can be utilised to effectively bond the composite part to adjacent metallic structures. This article presents the influence of the material configuration of fibre-metal laminates consisting of continuous fibre-reinforced thermoplastic outer layers integrated with a layer of metallic aluminium alloy inserts - a number of layers, type and direction of reinforcing fibres - on the static and fatigue flexural properties. In this study, eight laminate configurations were prepared using a one-step variothermal consolidation process. The results showed that in the three-point flexural fatigue test, the samples exceeded 106 cycles at stresses <30% of the static bending strength. Laminates with predominantly longitudinally reinforced layers showed the highest fatigue strength among the FML samples analysed. The type of reinforcing fibres and the number of layers were less affected on the analysed mechanical properties.
Źródło:
Fatigue of Aircraft Structures; 2022, 14; 18--28
2081-7738
2300-7591
Pojawia się w:
Fatigue of Aircraft Structures
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Validation process for computational model of full-scale segment for design of composite footbridge
Autorzy:
Ferenc, Tomasz
Mikulski, Tomasz
Powiązania:
https://bibliotekanauki.pl/articles/259754.pdf
Data publikacji:
2020
Wydawca:
Politechnika Gdańska. Wydział Inżynierii Mechanicznej i Okrętownictwa
Tematy:
validation
numerical modelling
sandwich structure
polymer composites
GFRP laminates
Opis:
Experimental tests and numerical simulations of a full-scale segment of a foot and cycle bridge made of polimer composites are presented in the paper. The analysed structure is made of sandwich panels, which consist of glass fibre reinforced polymer (GFRP) multi-layered laminate faces and a PET foam (obtained from recycling) core. The dimensions of the segment cross-section are the same as for the target footbridge; however, span length was reduced to 3 m. The experimental tests were conducted in a laboratory of the Faculty of Ocean Engineering and Ship Technology at Gdansk University of Technology. A single vertical force was generated by a hydraulic cylinder and was applied to the platform of the structure. The experimental tests were supported by numerical analyses performed in Femap with NX Nastran software by means of the finite element method (FEM). Results obtained in the computational model were compared with results from experiments. Thus, the numerical model was validated and the obtained conclusions were used in the next step of the design process of a composite footbridge with a span length of 14.5 m.
Źródło:
Polish Maritime Research; 2020, 2; 158-167
1233-2585
Pojawia się w:
Polish Maritime Research
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Experimental Research in the Aspect of Determining the Mechanical and Strength Properties of the Composite Material Made of Carbon-Epoxy Composite
Autorzy:
Różyło, Patryk
Smagowski, Wojciech
Paśnik, Jakub
Powiązania:
https://bibliotekanauki.pl/articles/2201915.pdf
Data publikacji:
2023
Wydawca:
Stowarzyszenie Inżynierów i Techników Mechaników Polskich
Tematy:
material properties
laminates
strength testing
thin-walled composite structures
Opis:
The present paper, provides a study of conducting experimental investigations (based on the ISO standards), in the context of determining material properties (mechanical and strength parame-ters) in the case of thin-walled composite structures - made of carbon-epoxy composite. Tests were carried out on 5 different types of test specimens (in accordance with the standards), with a minimum of 9 specimens per each type of test. The tests provided high repeatability of results, and the large number of test specimens per each test made it possible to precisely average the test results in terms of determining the necessary material properties. The tests were carried out using a Zwick Z100 universal testing machine (UTM), under room temperature conditions, using two types of test heads that allow static experimental tests. The results presented in this paper con-stitute a prelude to research within the framework of the project from the National Science Centre (Poland) with the number 2021/41/B/ST8/00148. The paper presents the initial stage of the im-plementation of the aforementioned project - which was the determination of material parameters of the composite material from which the target thin-walled composite structures with closed sections were made.
Źródło:
Advances in Science and Technology. Research Journal; 2023, 17, 2; 232--246
2299-8624
Pojawia się w:
Advances in Science and Technology. Research Journal
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
The Effect of Fiber Arrangement in the Bio-Laminate and Geometric Parameters on the Stability of Thin-Walled Angle Column Under Axial Compression
Autorzy:
Gawryluk, Jarosław
Powiązania:
https://bibliotekanauki.pl/articles/2201861.pdf
Data publikacji:
2023
Wydawca:
Stowarzyszenie Inżynierów i Techników Mechaników Polskich
Tematy:
bio-laminates
flax
buckling analysis
L-profile
numerical case
Opis:
The aim of this study is to check how the change fiber configuration and geometric parameters affect the stability of a thin-walled angle column under compression. Buckling analysis of thin-walled structures made of bio-laminates was presented. Short angles with different configurations of reinforcing fibers and geometric parameters were studied. The laminate under analysis had a matrix made of epoxy resin reinforced with unidirectional flax fibers. The axially compressed structures were simply supported on both ends. Detailed numerical analyses were conducted by the finite element method using Abaqus software. The lowest two bifurcation loads and their corresponding eigenmodes were determined. Several configurations of unidirectional fiber arrangement with different width and length were tested. Results showed that the bio-laminate fiber configuration had a significant effect on the behavior of the compressed structure. Moreover, the change of geometrical parameters significantly influences the stability of the structure. In general, it was found that the bifurcation load decreased with the increase of the length of the L-profile column. However, increasing the flange width of the column resulted in a reduction of the bifurcation load (applies to a column with a length of 300 mm and longer). In paper the first stage of research is presented, which will be experimentally verified in subsequent studies.
Źródło:
Advances in Science and Technology. Research Journal; 2023, 17, 1; 150--159
2299-8624
Pojawia się w:
Advances in Science and Technology. Research Journal
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Analysis of cross-ply laminates with piezoelectric fiber-reinforced composite actuators using four-variable refined plate theory
Autorzy:
Rouzegar, J.
Abad, F.
Powiązania:
https://bibliotekanauki.pl/articles/949140.pdf
Data publikacji:
2015
Wydawca:
Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej
Tematy:
cross-ply laminates
electromechanical loading
four-variable theory
PFRC actuator
Opis:
This study presents an analytical solution for cross-ply composite laminates integrated with a piezoelectric fiber-reinforced composite (PFRC) actuator subjected to electromechanical loading using the four-variable refined plate theory. This theory predicts parabolic variation of transverse shear stresses and satisfies the zero traction on the plate surfaces without using the shear correction factor. Using the principle of minimum potential energy, the governing equations for simply supported rectangular plates are extracted and the Navier method is adopted for solution of the equations. The comparison of obtained results with other common plate theories and the exact solution indicates that besides the simplicity of the presented formulation, it is very accurate in analysis of laminated composite plates integrated with PFRC. Also the effects of the thickness ratio, aspect ratio, number of layers, staking sequence and amount of electrostatic loading on the displacements and stresses are investigated and the obtained findings are reported.
Źródło:
Journal of Theoretical and Applied Mechanics; 2015, 53, 2; 439-452
1429-2955
Pojawia się w:
Journal of Theoretical and Applied Mechanics
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
On the modelling and optimization of functionally graded laminates
Modelowanie i optymalizacja laminatów o strukturze gradientowej
Autorzy:
Rychlewska, J.
Powiązania:
https://bibliotekanauki.pl/articles/280698.pdf
Data publikacji:
2006
Wydawca:
Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej
Tematy:
laminaty
materiały gradientowe
modelowanie
optymalizacja
functionally graded laminates
dynamics
modelling
Opis:
The object of investigations are Functionally Graded Materials (FGM) which on the microstructural level are made of two kinds of very thin laminae. These FGM will be referred to as the Functionally Graded Laminates (FGL). The aim of this contribution is to formulate discrete-continuum and continuum 3D-models of elastodynamics of FGL. The proposed modelling procedure constitutes a certain generalization of the approach to the modelling of periodic structures leading to a system of finite difference equations and then to their continuum approximation, Rychlewska and Woźniak (2003). The obtained results are applied to the analysis of a certain layered structure with a FGL transition zone. The optimization problem related to the position of the transition zone is discussed.
Przedmiot rozważań stanowi szczególna klasa materiałów gradientowych, tzw. laminatów o strukturze gradientowej, które na poziomie mikrostrukturalnym złożone są z dużej liczby bardzo cienkich wartewek. celem pracy jest zaproponowanie modelu dyskretno-ciągłego i ciągłego zagadnień elastodynamiki takich laminatów. Sformułowany model ciągły został zastosowany do analizy drgań ośrodka obciążonego inercyjnie, złożonego z dwóch jednorodnych wartw, pomiędzy którymi znajduje się strefa przejściowa. Przedyskutowano zagadnienie optymalizacji położenia strefy przejściowej.
Źródło:
Journal of Theoretical and Applied Mechanics; 2006, 44, 4; 783-795
1429-2955
Pojawia się w:
Journal of Theoretical and Applied Mechanics
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Ultra-light vehicle for disable people
Autorzy:
Grzegożek, W.
Domagała, M.
Powiązania:
https://bibliotekanauki.pl/articles/246304.pdf
Data publikacji:
2015
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
ultralight vehicle
electric vehicle
laminates panels
vehicle for disable people
Opis:
The paper presents a study on concept of ultra-light vehicle created by innovatory technology with laminate panels what provided low weight of self-supporting body and in consequences low vehicle weight. The usage of panels with aluminum honeycomb core and glass fiber based skins allows creating large flat surfaces for interior and vehicle body without any additional treatment. Glued panels with aluminium core make closed, rigid structure of self-supporting body with relatively low weight. Independent suspension system which components are made of carbon fiber also guarantees low weight. Vehicle is powered by two electric motors BLDC type with power of 2 kW each, and they are placed in rear wheels. Low vehicle weight has important meaning, particularly for electric vehicles and its range. Presented vehicle belongs to L6-e category and does not require any licenses for driving. The vehicle is dedicated for disable people on wheel chairs. The fundamental problem for disable people on wheelchairs is getting inside a vehicle without any help. Proposed solution at the conceptual vehicle allows for getting the wheel chair inside the vehicle by the use of lower part of the rear door and the wheel chair play a role of the vehicle seat. Such solution also makes that the level of physical disability has no influence on auxiliary devices used for vehicle driving.
Źródło:
Journal of KONES; 2015, 22, 1; 115-126
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Overview of polymer laminates applicable to elements of light-weight ballistic shields of special purpose transport means
Autorzy:
Sliwinski, M.
Kucharczyk, W.
Guminski, R.
Powiązania:
https://bibliotekanauki.pl/articles/30147051.pdf
Data publikacji:
2018
Wydawca:
Akademia Wojsk Lądowych imienia generała Tadeusza Kościuszki
Tematy:
aramid fibers
polyethylene fibers
polymeric laminates
bulletproof armor
ballistic plate
Opis:
The paper reviews and evaluates the possibility of using polymer fibrous composites for lightweight passive bulletproof armors for application in special-purpose means of transport. The shielding properties of the composite ballistic plates manufactured based on fibers commonly used for such applications: aramid (Kevlar, Twaron) and polyethylene ones (Spectra, Dyneema) as well as ceramic-laminate systems built based on the both above-mentioned ones have been characterized. Examples of application of lightweight, polymer ballistic laminates in armors and supplementary armors of special-purpose transport vehicles, illustrated by aircraft constructions, have been presented in accordance with literature sources and manufacturers' information.
Źródło:
Scientific Journal of the Military University of Land Forces; 2018, 50, 3(189); 228-243
2544-7122
2545-0719
Pojawia się w:
Scientific Journal of the Military University of Land Forces
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Topology optimization - broadening the areas of application
Autorzy:
Bendsoe, M. P.
Lund, E.
Olhoff, N.
Sigmund, O.
Powiązania:
https://bibliotekanauki.pl/articles/970157.pdf
Data publikacji:
2005
Wydawca:
Polska Akademia Nauk. Instytut Badań Systemowych PAN
Tematy:
optymalizacja topologiczna
laminat
płyn
topology optimization
laminates
pressure loads
multiphysics
fluids
Opis:
This paper deals with recent, developments of topology optimization techniques for application in some new types of design problems. The emphasis is on recent work of the Danish research groups at Aalborg University and at the Technical University of Denmark and focus is on the central role that the choice of objective functions and design parameterization plays for a successful extension of the material distribution approach to new design settings and to new types of physics models. The applications that will be outlined encompass design of laminated composite structures, design for pressure loads, design in fluids, design in acoustics, and design in photonics. A short outline of other design optimization activities is also given.
Źródło:
Control and Cybernetics; 2005, 34, 1; 7-35
0324-8569
Pojawia się w:
Control and Cybernetics
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Faults Detection In Layered Composite Structures Using Wavelet Transform
Detekcja uszkodzeń w warstwowych strukturach kompozytowych z zastosowaniem transformacji falkowej
Autorzy:
Katunin, A.
Moczulski, W.
Powiązania:
https://bibliotekanauki.pl/articles/328984.pdf
Data publikacji:
2010
Wydawca:
Polska Akademia Nauk. Polskie Towarzystwo Diagnostyki Technicznej PAN
Tematy:
laminaty polimerowe
detekcja uszkodzeń
transformacja falkowa
GFRP laminates
faults detection
wavelet transform
Opis:
In the paper the authors present their results concerning measurements of frequency responses of cantilever rectangular GFRP plates with intentionally inserted faults of three different types (fiber discontinuities, delaminations and notches for simulating cracks). The preliminary research shows that classical methods of signal conditioning (e.g. FFT or STFT) often do not project changes between damaged and undamaged structures, when faults are inconsiderable. In the experiment the frequency responses of the investigated samples with and without faults were obtained by means of the impact test carried out using LMS SCADAS and TestXPress software. For the approximation in wavelet transform (WT) Morlet and Db8 wavelet functions were applied. The shapes of these functions give the best imitation of the measured signal shape obtained from the impact test. The obtained results allow to assert that the proposed methodology of faults detection in layered structures based on WT can be useful for fault diagnosis even in early damage phase, when other methods are insensitive. In the further work the authors will develop the proposed method for faults identification and localization in layered structures and investigate laminate behavior with faults and self-heating in fatigue processes.
W pracy autorzy przedstawiają wyniki pomiarów odpowiedzi częstotliwościowych jednostronnie utwierdzonych prostokątnych płyt z kompozytu polimerowego zbrojonego włóknem szklanym z celowo wprowadzonymi uszkodzeniami trzech typów (nieciągłości włókien, delaminacje i karby symulujące pęknięcia). Badania wstępne pokazują, że klasyczne metody obróbki sygnałów (jak FFT czy STFT) często nie obrazują zmian pomiędzy strukturą uszkodzoną i nieuszkodzoną, gdy uszkodzenia są nieznaczne. W eksperymencie z zastosowaniem testu impulsowego były otrzymane odpowiedzi częstotliwościowe badanych próbek przy pomocy LMS SCADAS i oprogramowania TestXPress. Do aproksymacji w transformacji falkowej użyto funkcji bazowych Morleta i Db8. Kształt tych funkcji daje najlepsze przybliżenie przebiegu wartości chwilowych zmierzonego sygnału otrzymanego z testu impulsowego. Otrzymane wyniki pozwalają stwierdzić, że zaproponowana metodologia detekcji uszkodzeń w strukturach warstwowych oparta na transformacji falkowej może być użyteczne przy diagnostyce uszkodzeń nawet we wczesnych stadiach degradacji, gdy inne metody są nieczułe. W przyszłych pracach autorzy będą rozwijać zaproponowaną metodę pod kątem identyfikacji i lokalizacji uszkodzeń w strukturach warstwowych oraz badać zachowanie laminatów z uszkodzeniami i temperaturą samowzbudną w procesach zmęczeniowych.
Źródło:
Diagnostyka; 2010, 1(53); 27-32
1641-6414
2449-5220
Pojawia się w:
Diagnostyka
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Finite numerical analysis of composite structure under complex loading conditions - optimal ply design of laminate
Autorzy:
Dębski, H.
Powiązania:
https://bibliotekanauki.pl/articles/246147.pdf
Data publikacji:
2010
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
finite element method
laminates
strength of composite structures
composites damage
composites optimization
Opis:
The paper presents FEA numerical analysis of composite structure subjected to complex loading conditions (tension and shear). The layered structures were characterized from the standpoint of optimal selection and strength parameters. The subject of the examinations was a composite: glass fibres reinforcedpolymers-M12/26%/TVR380R-glass prepreg system (Hexcel, R-glass fibres-undirectional, M12 epoxy resin). The composite system is use in helicopter blades. It exhibits good fatigue life and hot/wet performances up to 100° C. The strength properties were investigated according to ISO and ASTM standards. The composites for the study were pro duce d by autoclave technique. The Layup-Ply method with ABAQUS/Standard program was applied as an analysis tool which was carried out the leading of calculation. It was used an incremental iterative Newton-Raphson's method in a range of nonlinear geometric. Numerical calculation was made as a part of introduction to failure analysis composite materials. The risk of laminate's damage could be estimated as a possible appearing in dangerous points of construction. There were taken four criteria: the Maximum Stress Criterion, Tsai-Hill's Criterion, tensor criterion of Tsai-Wu and Azzi-Tsai-HiU's criterion.
Źródło:
Journal of KONES; 2010, 17, 1; 111-115
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Determination of In-Plane Shear Properties of Laminate with V-Notch Rail Shear Test and Digital Image Correlation
Autorzy:
Karny, Maciej
Powiązania:
https://bibliotekanauki.pl/articles/36405939.pdf
Data publikacji:
2019
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:
digital image correlation
in-plane shear
thermoplastic laminates
v-notch rail shear
Opis:
This article presents the results of the application of Digital Image Correlation (DIC) to measurements of in-plane shear modulus and strength of three different carbon fiber reinforced laminates. Three different approaches to shear strain calculations via DIC are evaluated and compared with standard strain gage measurements. Calculation of shear strain based on averaging DIC strain values of strain gages area in most cases yielded results closest to strain gages, while measurements based on single point strain measuring differed the most from strain gages. These results are attributed to shear strain distribution in the center area of the specimen. Thermoplastic matrix fabric reinforced composite had the lowest shear strength at 5% of shear strain, but the highest ultimate shear strength and strain at failure. Of thermosetting materials, laminate reinforced with unidirectional carbon fiber had shear modulus about 10% lower, than fabric reinforced laminate, but higher ultimate strength and strain at failure. This behavior is attributed to the presence of weaves in fabric reinforcing the laminate, causing shear stiffening of the material, but lowering its ability to deform under shear loading.
Źródło:
Transactions on Aerospace Research; 2019, 3 (256); 57-65
0509-6669
2545-2835
Pojawia się w:
Transactions on Aerospace Research
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Modelling of the Temperature Field within Textile Inlayers of Clothing Laminates
Modelowanie pola temperatury we wkładach włókienniczych laminatów odzieżowych
Autorzy:
Korycki, R.
Szafrańska, H.
Powiązania:
https://bibliotekanauki.pl/articles/232203.pdf
Data publikacji:
2013
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Biopolimerów i Włókien Chemicznych
Tematy:
heat transfer
modelling
inlayer
clothing laminates
przenikanie ciepła
modelowanie
wkłady włókiennicze
laminaty odzieżowe
Opis:
Inlayers are introduced to improve the aesthetic qualities and stiffness against the creasing of clothing laminates. The laminate is created by the thermoplastic polymer glue between the inlayer and clothing material, softened by the heat. The connection is secured by the adhesive properties of the polymer and the pressure applied. The state variable is temperature. The heat transfer is described by the heat transport equation as well as by the set of boundary and intial conditions. The temperature distributions within the inlayers are determined by the numerical simulation for different temperatures of the heating plates. The temperature maps are shown by means of the graphical modulus of the program ADINA. The mean temperature of the polymer layer is next calculated.
Wkłady włókiennicze są stosowane w celu poprawy właściwości estetycznych i wzrostu sztywności zgniatania laminatów odzieżowych. Laminat odzieżowy jest tworzony z wykorzystaniem termoplastycznego kleju polimerowego, umieszczonego między wkładem i materiałem odzieżowym, rozrzedzonego za pomocą ciepła. Połączenie jest utrwalane dzięki właściwościom adhezyjnym polimeru oraz przyłożonemu naciskowi. Zmienna stanu to temperatura. Przepływ ciepła jest opisywany za pomocą równania transportu ciepła oraz układu warunków brzegowych i początkowych. Rozkład temperatury we wkładzie można określić za pomocą symulacji numerycznej dla różnych temperatur płyt grzejnych. Mapy temperatury można poddać wizualizacji za pomocą modułu graficznego programu ADINA. Następnie można określić temperaturę warstwy polimeru.
Źródło:
Fibres & Textiles in Eastern Europe; 2013, 4 (100); 118-122
1230-3666
2300-7354
Pojawia się w:
Fibres & Textiles in Eastern Europe
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Modern process of composite structures manufacturing based on cad definition of the composite
Nowoczesny proces produkcji struktur kompozytowych w oparciu o komputerową definicję kompozytu
Autorzy:
Krauze, W.
Powiązania:
https://bibliotekanauki.pl/articles/212886.pdf
Data publikacji:
2016
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:
producibility
flat pattern
layup
laminates
CATIA CPD
kompozyty
technologiczność kompozytów
rozkroje warstw
laminaty
Opis:
The article describes benefits for composite structures manufactured with the computer aid. The evolution of manufacturing process is presented, highlighting the specifics of anisotropic and laminar properties of composites. The paper shows steps of the process, including: design, preliminary computer analysis, virtual layup modelling, materials preparation. It comprehensively describes the state-of-the-art modern process featuring all technological equipment that facilitates the efficient and certifiable manufacturing. Important parameters of fabric for the producibility are presented. The article presents flat patterns creation, presumption of potential problems at work, as well as important parameters for the producibility check. Functions that make manufacturing department's (M&P) life easier are brought closer. Different software is named in the article, one is chosen as an example in the article and guided through.
Artykuł opisuje jak komputerowa definicja struktur kompozytowych w modelu CAD upraszcza proces wytwórczy oraz przyczynia się do uzyskania najwyżej jakości owych struktur. Zaprezentowana została ewolucja procesu wytwarzania struktur z uwzględnieniem anizotropowych i warstwowych właściwości kompozytu. Krok po kroku ukazany jest proces projektowania części kompozytowych włączając w to definiowanie kompozytu w modelu komputerowym, symulacje technologiczności, uzyskiwanie płaskich kształtów poszczególnych warstw i transfer wyników na produkcję. Kompleksowo opisany został stan techniki, oprogramowanie i przyrządy konieczne by w sposób nowoczesny produkować wysokiej jakości części. Odpowiednio przygotowany przez konstruktora proces jest wielkim ułatwieniem podczas wytwarzania co w jasny sposób zostało ukazane w niniejszym artykule.
Źródło:
Prace Instytutu Lotnictwa; 2016, 4 (245); 70-78
0509-6669
2300-5408
Pojawia się w:
Prace Instytutu Lotnictwa
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Stationary heat conduction in transversally graded laminates with uniform and non-uniform distribution of laminas
Autorzy:
Jędrysiak, J.
Powiązania:
https://bibliotekanauki.pl/articles/362609.pdf
Data publikacji:
2010
Wydawca:
Instytut Fizyki Budowli Katarzyna i Piotr Klemm
Tematy:
przewodzenie ciepła
poprzeczne stopniowanie laminatów
uśredniona tolerancja
heat conduction
transversally graded laminates
tolerance averaging
Opis:
A problem of stationary heat conduction in laminates with transversally graded structure is analysed. These composites consist of two components, non-periodically distributed as laminas. Averaged (macroscopic) properties of these laminates are slowly and continuously varied along the axis normal to laminas. In this contribution the stationary heat conduction problem is analysed in the framework of the tolerance model, proposed by Jędrysiak and Radzikowska [2,6,3].
Źródło:
Fizyka Budowli w Teorii i Praktyce; 2010, T. 5, nr 3, 3; 17-20
1734-4891
Pojawia się w:
Fizyka Budowli w Teorii i Praktyce
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Numerical study of the fatigue delamination growth considering thermal phenomena
Analiza numeryczna zmęczeniowego przyrostu delaminacji z uwzględnieniem zjawisk cieplnych
Autorzy:
Katunin, A.
Powiązania:
https://bibliotekanauki.pl/articles/327658.pdf
Data publikacji:
2010
Wydawca:
Polska Akademia Nauk. Polskie Towarzystwo Diagnostyki Technicznej PAN
Tematy:
laminaty polimerowe
samorozgrzanie
przyrost delaminacji
diagnostyka
polymer-based laminates
self-heating
delamination growth
diagnostics
Opis:
The wide applicability of polymer-based laminates in the engineering practice causes the development of methods of their diagnosing. One of the most crucial faults in polymer-based laminates is their delamination. The problem becomes more complicated while thermal effects (e.g. self-heating and frictional heating) are taken into consideration. In the present study the numerical model of fatigue growth of the delamination in linearly viscoelastic polymer-based laminate was developed. The obtained results show, that the neglecting of the thermal effects in delamination process with some loading parameters for such structures can cause large inaccuracies in delamination growth evaluation and prediction.
Szerokie zastosowanie laminatów polimerowych w praktyce inżynierskiej wywołuje potrzebę rozwoju metod ich diagnostyki. Jednym z najbardziej krytycznych uszkodzeń w laminatach polimerowych jest delaminacja. Problem staje się bardziej skomplikowany, gdy pod uwagę bierze się efekty cieplne (samorozgrzanie, rozgrzanie od tarcia). W niniejszej pracy zaproponowano model numeryczny zmęczeniowego przyrostu delaminacji w liniowo-lepkosprężystym laminacie polimerowym. Otrzymane wyniki wskazują, że pominięcie efektów cieplnych w procesie delaminacji z pewnymi parametrami obciążenia dla takich struktur może powodować duże niedokładności w oszacowaniu i predykcji przyrostu delaminacji.
Źródło:
Diagnostyka; 2010, 4(56); 23-26
1641-6414
2449-5220
Pojawia się w:
Diagnostyka
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Sensitivity of Temperature Field to Material Parameters within the Clothing Laminate Process
Wrażliwość pola temperatury na parametry materiałowe w procesie laminowania odzieży
Autorzy:
Korycki, R
Szafrańska, H
Powiązania:
https://bibliotekanauki.pl/articles/231943.pdf
Data publikacji:
2014
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Biopolimerów i Włókien Chemicznych
Tematy:
sensitivity
temperature field
clothing laminates
wrażliwość pola temperatury
laminowanie odzieży
laminat włókienniczy
parametry materiałowe
Opis:
Textile laminate is created by introducing a thermoplastic polymer between the inner layer and outer material, which is then softened by heat. The connection is secured by adhesive properties of the polymer and the pressure applied after the heating zone. The state variables are defined as thus: the temperature of the heating zone and the pressure of rollers for the pressure system. The heat problem is described by the heat transport equation as well as the boundary and initial conditions. The distributions of the mean temperature within the polymer layer can be determined by numerical simulation. The sensitivity of the temperature field to the selected material parameters within clothing laminates is determined.
Laminat włókienniczy jest tworzony przez termoplastyczny polimer zmiękczany cieplnie, wprowadzany między wkład odzieżowy i materiał zewnętrzny. Połączenie jest tworzone dzięki właściwościom adhezyjnym polimeru oraz naciskowi przykładanemu poza strefą nagrzewania. Zmienne stanu to temperatura dla strefy nagrzewania oraz nacisk wałków systemu dociskowego. Problem cieplny jest opisany przez równanie transportu ciepła oraz warunki brzegowe i początkowe. Rozkład średniej temperatury w warstwie polimeru może zostać określony poprzez symulacje numeryczne. Została wyznaczona wrażliwość pola temperatury w laminatach odzieżowych na wybrane parametry materiałowe.
Źródło:
Fibres & Textiles in Eastern Europe; 2014, 5 (107); 83-88
1230-3666
2300-7354
Pojawia się w:
Fibres & Textiles in Eastern Europe
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Stability of the thin-walled angle column made of bio-laminate versus glass-laminate under axial compression – numerical study
Autorzy:
Gawryluk, Jarosław
Powiązania:
https://bibliotekanauki.pl/articles/27309877.pdf
Data publikacji:
2023
Wydawca:
Polska Akademia Nauk. Czasopisma i Monografie PAN
Tematy:
bio-laminates
buckling
thin-walled structures
FEM
eigenproblem
biolaminat
wyboczenie
konstrukcje cienkościenne
MES
problem własny
Opis:
The aim of this study was to determine how the change of glass laminate fibres to flax fibres will affect the stability of thin-walled angle columns. Numerical analyses were conducted by the finite element method. Short L-shaped columns with different configurations of reinforcing fibres and geometric parameters were tested. The axially compressed structures were simply supported on both ends. The lowest two bifurcation loads and their corresponding eigenmodes were determined. Several configurations of unidirectional fibre arrangement were tested. Moreover, the influence of a flange width change by ±100% and a column length change by ±33% on the bifurcation load of the compressed structure was determined. It was found that glass laminate could be successfully replaced with a bio-laminate with flax fibres. Similar results were obtained for both materials. For the same configuration of fibre arrangement, the flax laminate showed a lower sensitivity to the change in flange width than the glass material. However, the flax laminate column showed a greater sensitivity to changes in length than the glass laminate one. In a follow-up study, selected configurations will be tested experimentally.
Źródło:
Archive of Mechanical Engineering; 2023, LXX, 1; 43--61
0004-0738
Pojawia się w:
Archive of Mechanical Engineering
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Stationary heat conduction in laminates with non-uniform distribution of laminas
Stacjonarne przewodnictwo ciepła w laminatach o nierównomiernym rozmieszczeniu warstw
Autorzy:
Jędrysiak, J.
Powiązania:
https://bibliotekanauki.pl/articles/395959.pdf
Data publikacji:
2010
Wydawca:
Uniwersytet Zielonogórski. Oficyna Wydawnicza
Tematy:
laminaty
poprzeczna gradacja struktury
przewodnictwo cieplne
laminates
transversally graded structure
nonhomogeneous distribution of laminas
heat conduction
Opis:
In this paper it is analysed a stationary heat conduction in laminates made of two materials non-periodically distributed as microlaminas along one direction. It is assumed that this laminate has a functionally (transversally) graded macrostructure along this direction. Some effects of the microstructure in a distribution of a temperature are investigated using the tolerance modelling, cf. the book edited by Cz. Woźniak et al. [6].
W pracy rozpatrywany jest stacjonarny problem przewodnictwa ciepła w laminatach charakteryzujących się "wolną" zmianą własności makroskopowych (uśrednionych) w kierunku prostopadłym do warstw. Przyjęto, że rozmieszczenie warstw jest nierównomierne. Wpływ mikrostruktury na rozkład temperatury całkowitej zbadano wykorzystując modelowanie tolerancyjne, por. Cz. Woźniak et al. [6].
Źródło:
Civil and Environmental Engineering Reports; 2010, 5; 101-111
2080-5187
2450-8594
Pojawia się w:
Civil and Environmental Engineering Reports
Dostawca treści:
Biblioteka Nauki
Artykuł
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