Adavances in composite wind turbine blades: A comparative study
(Sprache: Englisch)
In the wind industry, the current trend is towards building larger and larger turbines. This presents additional structural challenges and requires blade materials that are both lighter and stiffer than the ones presently used. This study is aimed to aid...
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In the wind industry, the current trend is towards building larger and larger turbines. This presents additional structural challenges and requires blade materials that are both lighter and stiffer than the ones presently used. This study is aimed to aid the work of designing new wind turbine blades by providing a comparative study of different composite materials. A coupled Finite-Element-Method (FEM) - Blade Element Momentum (BEM) code was used to simulate the aerodynamic forces subjected on the blade. For this study, the finite element study was conducted on the Static Structural Workbench of ANSYS, as for the geometry of the blade it was imported from a previous study prepared by Cornell University. Confirmation of the performance analysis of the chosen wind turbine blade is presented and discussed including the generated power, tip deflection, thrust and tangential force for a steady flow of 8m/s.A homogenization method was applied to derive the mechanical properties and ultimate strengths of the composites. The Tsai-Hill and Hoffman failure criterions were both conducted to the resulting stresses and shears for each blade composite material structure to determine the presence of static rupture. A progressive fatigue damage model was conducted to simulate the fatigue behavior of laminated composite materials, an algorithm developed by Shokrieh.
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Textprobe:CHAPTER V, Fatigue Model:
5.1, Overview:
Even though composite materials are designated as being fatigue-insensitive, especially when compared to metallic ones, they also suffer from fatigue loads. The use of composite materials in a wide range of applications obliged researchers to consider fatigue when investigating a composite material and engineers to realize that fatigue is an important parameter that must be considered in calculations during design processes, even for structures where fatigue was not traditionally considered an issue. Although composites were initially used as replacements for conventional materials such as steel, aluminum or wood, and later as advanced materials allowing engineers to adopt a different approach to design problems, the fatigue behavior of composite materials is different from that of metallic materials. Therefore, the already developed and validated methods for the fatigue life modeling and prediction of conventional materials cannot be directly applied to composite materials.
Mathematical models have been developed to describe fatigue damage analytically and eventually predict the fatigue lifetime of FRP composite materials. The ideal fatigue theory is described by Sendeckyj in 27 as one based on a damage metric hat accurately models the experimentally observed damage accumulation process, considers all pertinent material, test and environmental variables, correlates the data for a large class of materials, permits the accurate prediction of laminate fatigue behavior from lamina fatigue data, is readily extendable to two-stage and spectrum fatigue loading and takes data scatter into account. These requirements cannot be met simultaneously for many reasons and theoretical models that address only some of them have been introduced. For predicting the fatigue life of structural components made of composites, at least two alternative design concepts could be used: the damage-tolerant (or fail-safe) and the
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safe-life design concepts.
In the former it is assumed that a damage metric, such as crack length, delamination area, residual strength or stiffness, can be correlated to fatigue life via a valid criterion. The presence of damage is permitted as long as it is not critical i.e., it cannot lead to sudden failure. In the latter safe-life design situations cyclic stress or strain is directly associated to operational life via the S N or e-N curves. The structure is allowed to operate since no damage is observed, e.g., before the initiation of any measurable cracks. Although this design approach ensures the use of safe structures, it considerably increases their cost since it requires very low design values, below the estimated fatigue threshold observed in fracture mechanics experiments on FRP materials.
One of the broadest groups of theoretical models, representing damage-tolerant design concepts, comprises the phenomenological fatigue failure theories , also referred to as empirical fatigue theories . Models of this type are based on the definition of reliable S N curves and constant life diagram formulations that are used to estimate allowable numbers of cycles to failure under any given loading pattern from constant to variable amplitude. For most practical cases however, designers require models of behavior that can predict failure under realistic load combinations that yield realistic combinations of stresses, rather than under the uniaxial stress states that usually develop during laboratory experiments [26]. Multiaxial fatigue failure criteria have been developed to take multiaxial fatigue into account [28, 29]. Most of the aforementioned examples in the literature concentrate mainly on the introduction and validation of fatigue failure criteria suitable for constant amplitude multiaxial proportional stress fields without addressing the problem of life prediction under irregular load spectra.
The fatigue design of a structural application is generally base
In the former it is assumed that a damage metric, such as crack length, delamination area, residual strength or stiffness, can be correlated to fatigue life via a valid criterion. The presence of damage is permitted as long as it is not critical i.e., it cannot lead to sudden failure. In the latter safe-life design situations cyclic stress or strain is directly associated to operational life via the S N or e-N curves. The structure is allowed to operate since no damage is observed, e.g., before the initiation of any measurable cracks. Although this design approach ensures the use of safe structures, it considerably increases their cost since it requires very low design values, below the estimated fatigue threshold observed in fracture mechanics experiments on FRP materials.
One of the broadest groups of theoretical models, representing damage-tolerant design concepts, comprises the phenomenological fatigue failure theories , also referred to as empirical fatigue theories . Models of this type are based on the definition of reliable S N curves and constant life diagram formulations that are used to estimate allowable numbers of cycles to failure under any given loading pattern from constant to variable amplitude. For most practical cases however, designers require models of behavior that can predict failure under realistic load combinations that yield realistic combinations of stresses, rather than under the uniaxial stress states that usually develop during laboratory experiments [26]. Multiaxial fatigue failure criteria have been developed to take multiaxial fatigue into account [28, 29]. Most of the aforementioned examples in the literature concentrate mainly on the introduction and validation of fatigue failure criteria suitable for constant amplitude multiaxial proportional stress fields without addressing the problem of life prediction under irregular load spectra.
The fatigue design of a structural application is generally base
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Autoren-Porträt von Adam Chehouri
A PhD student in engineering at the University of Quebec at Chicoutimi (UQAC). I hold a BS and a MS in Mechanical Engineering from the Lebanese University, Beirut, Lebanon. Currently preparing my PhD thesis on Optimization of composite structures of wind turbine blades . Experience, skills and knowledge in the fields of aerodynamics, composites and optimization and its applications in Wind Energy. My master thesis was a comparative study of static and fatigue behaviours for various composite orthotropic properties for a wind turbine using a coupled FEM-BEM method under the supervision of Dean Dr Rafic Younes of the Faculty of Engineering at the Lebanese University. Some of my projects and work include preliminary study of the influence of air pollution on meteorology , Hybrid System Photovoltaic-Wind , yaw control for a wind turbine , design and prototype of a sensor for wind direction using thermocouples and preliminary site study for the installation of 100 and 150 KW wind turbines in the Bekaa region.
Bibliographische Angaben
- Autor: Adam Chehouri
- 2014, Erstauflage, 72 Seiten, 64 Abbildungen, Maße: 15,5 x 22 cm, Kartoniert (TB), Englisch
- Verlag: Anchor Academic Publishing
- ISBN-10: 3954892308
- ISBN-13: 9783954892303
Sprache:
Englisch
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