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I. The reinforcement of epoxy composites with carbon fibers, are reinforced with the traditional glass fibers or with carbon fibers with or without the distribution of the carbon fibers via fibers. All of these solutions show the higher costs or the lack of recyclability of traditional epoxy/glass composites. The companies that promote this kind of solutions, e.g., Boeing, Mitsubishi, between others, often promote the use of matrix composites, which can be recycled after the end of production of the wind turbine blades. The biggest disadvantage of matrix composites are the higher costs; especially the fibers are expensive and, in most cases, they are not recyclable or not easily recyclable after their use. The matrix of such composites is weaker, plastic and, thus, has lower wear resistance than the epoxy resin. However, in comparison to typical epoxy resin, a matrix composite has a higher thermal stability and higher dimensional stability, which is even more important in the process of finishing and tempering, in which the changes in the dimensions of the parts are determined by the melt viscosity changes. Furthermore, the carbon filler in carbon fiber composite is more suited to make the composite resistant to a high temperature and longer time examination than the epoxy resin, which leads to the increased applicability of carbon fiber composites in the area of application in the wind turbine blades. Besides the consideration of the costs, the ability to be recycled after the end of the production has to be taken into account for the materials that often are custom produced together with the entire wind turbine systems. The recyclable recycling of the composites should lead to the lessened environmental, and probably also to the lower costs of energy for the energy industry.

II. The wedgewise loading (pressure flapping, gravity forces, etc.) are associated with the laminate at the leading and trailing edge of the blade. The composite plates/fabrics and the spar are designed against brittle failure, which means that the laminates, the straps, the webs and the spar should have a very low weakness. Good mechanical properties of these structures have to be combined with a good toughness (resistance against progressive damage) and better fatigue properties. The most important failure criterion is the ability to survive the damage on the blade without causing any further damage, i.e., the ability to survive without progressive damage. d2c66b5586

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