29 research outputs found

    Reversible Rail Shear Apparatus Applied to the Study of Woven Laminate Shear Behavior

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    The multitude of in-plane shear tests existing in the literature seems to demonstrate the complexity of developing a test adapted to all experimental works. In a general framework of investigation of translaminar cracks in thin laminates, a test able to reproduce a pure in-plane shear loading was required. The laminate studied is notably employed as helicopter blade skin, and cyclic torsion induced by aerodynamic load involves cyclic in-plane shear. This particular application established some specifications for the test needed to carry out this study. To comply with them, an original technological solution has been developed from a three-rail shear test apparatus. This paper describes the resulting “reversible rail shear test” solution and its application to the study of in-plane shear behavior of a thin glass-epoxy laminate. The results concern plain and notched coupons under quasi-static loading, and crack growth tests under cyclic loading

    Propagation de coupure dans des tissus de verre de pâles arrières d'hélicoptères

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    L'objet de ce travail est l'étude de la propagation de coupure en fatigue dans des tissus composites de verre/époxy utilisés pour la fabrication de pâles arrières d'hélicoptères par la société EUROCOPTER. Une étude des directions chaîne et trame du tissu a été menée et a montré une différence de comportement importante sur la vitesse de propagation d'une coupure; en particulier le temps d'initiation dans la direction trame s'est révélé près de 10 fois plus important que celui de la chaine

    Semi-continuous approach for the modeling of thin woven composite panels applied to oblique impacts on helicopter blades

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    International audienceIn aeronautics, passenger safety and reliability of structures are essential aspects. In the specific case of helicopters, blades are subjected to impact loadings. Modeling these phenomena continue to be difficult and experimental tests often replace the prediction. The following work will focus on the experimental and numerical study of an oblique impact on the skin of the blade. It is equivalent in a first approach to an impact on a sandwich panel made up of a foam core and a thin woven composite skin. The objectives are to identify the mechanisms of damage in the skin for this kind of loading and to develop a representative modeling of the chronology of damage adapted to the modeling of the complete structure. Thus, a semi-continuous F.E. explicit modeling has been developed. It relies on the development of a specific damageable element at the bundles scale. Satisfactory numerical results are obtained. They allow the identification of the damage mechanism of the woven skin

    Light coupling with a nonlinear prism

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    International audienceWe propose the use of a prism with nonlinear optical properties to improve the prism-coupling method. The principle is based on the inscription of an adapted waveguide inside this prism by beam self-trapping to enhance the coupling efficiency and stability. The experimental demonstration is realized with a prism diced from a LiNbO3 wafer to couple light into a resonator
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