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This Paper complies the study of effects of various filler materials on Mechanical Properties of ... more This Paper complies the study of effects of various filler materials on Mechanical Properties of Carbon-Epoxy Composite. The paper gives the diversified description of the behavior of the Carbon-Epoxy Composite, under different loadings and conditions. The Carbon-Epoxy Composite was fabricated using various fillers such as, Coremat, Aerosil and Granite. The Composition of the Carbon-Epoxy Composite consists of 50% Carbon Fiber, 40% Resin and 10% fillers by weight. Three different types of Carbon-Epoxy Composite specimen were fabricated using three different Fillers, as mentioned above. The Method Adopted to fabricate the Carbon-Epoxy Composite is conventional Hand Lay-up technique. Furthermore, the Carbon-Epoxy Composite specimen was subjected to various Test Conditions, namely Tensile Test, Impact Test and Water Absorption Test and the behavior of the same is recorded and described in this paper.
ABSTRACT- Due to the problems of potential corrosion and thermal expansion differences between tr... more ABSTRACT- Due to the problems of potential corrosion and thermal expansion differences between traditional metal connecting pieces and carbon fiber poles, it is difficult for them to meet the operating requirements of truss structures in the environment of stratosphere. Based on the large scale composite space truss structure of stratosphere aerostats, the carbon fiber flange connection joints were studied in the present paper Adopting the three-dimensional full five-directional braiding technology, Toray T700 S–12K carbon fiber is used as the raw material to manufacture flange joint preform, and to manufacture flange forming by RTM (resin transfer molding) process. As demonstrated by tensile and bending tests, the composite flange joints have better mechanical properties than flanges manufactured by aviation aluminum alloy, and meet requirements of stratosphere truss structure connecting pieces. In conjunction with the results of finite element analysis, mechanical properties can b...
This Paper complies the study of effects of various filler materials on Mechanical Properties of ... more This Paper complies the study of effects of various filler materials on Mechanical Properties of Carbon-Epoxy Composite. The paper gives the diversified description of the behavior of the Carbon-Epoxy Composite, under different loadings and conditions. The Carbon-Epoxy Composite was fabricated using various fillers such as, Coremat, Aerosil and Granite. The Composition of the Carbon-Epoxy Composite consists of 50 % Carbon Fiber, 40 % Resin and 10 % fillers by weight. Three different types of Carbon-Epoxy Composite specimen were fabricated using three different Fillers, as mentioned above. The Method Adopted to fabricate the Carbon-Epoxy Composite is conventional Hand Lay-up technique. Furthermore, the Carbon-Epoxy Composite specimen was subjected to various Test Conditions, namely Tensile Test, Impact Test and Water Absorption Test and the behavior of the same is recorded and described in this paper.
This Paper complies the study of effects of various filler materials on Mechanical Properties of ... more This Paper complies the study of effects of various filler materials on Mechanical Properties of Carbon-Epoxy Composite. The paper gives the diversified description of the behavior of the Carbon-Epoxy Composite, under different loadings and conditions. The Carbon-Epoxy Composite was fabricated using various fillers such as, Coremat, Aerosil and Granite. The Composition of the Carbon-Epoxy Composite consists of 50% Carbon Fiber, 40% Resin and 10% fillers by weight. Three different types of Carbon-Epoxy Composite specimen were fabricated using three different Fillers, as mentioned above. The Method Adopted to fabricate the Carbon-Epoxy Composite is conventional Hand Lay-up technique. Furthermore, the Carbon-Epoxy Composite specimen was subjected to various Test Conditions, namely Tensile Test, Impact Test and Water Absorption Test and the behavior of the same is recorded and described in this paper.
ABSTRACT- Due to the problems of potential corrosion and thermal expansion differences between tr... more ABSTRACT- Due to the problems of potential corrosion and thermal expansion differences between traditional metal connecting pieces and carbon fiber poles, it is difficult for them to meet the operating requirements of truss structures in the environment of stratosphere. Based on the large scale composite space truss structure of stratosphere aerostats, the carbon fiber flange connection joints were studied in the present paper Adopting the three-dimensional full five-directional braiding technology, Toray T700 S–12K carbon fiber is used as the raw material to manufacture flange joint preform, and to manufacture flange forming by RTM (resin transfer molding) process. As demonstrated by tensile and bending tests, the composite flange joints have better mechanical properties than flanges manufactured by aviation aluminum alloy, and meet requirements of stratosphere truss structure connecting pieces. In conjunction with the results of finite element analysis, mechanical properties can b...
This Paper complies the study of effects of various filler materials on Mechanical Properties of ... more This Paper complies the study of effects of various filler materials on Mechanical Properties of Carbon-Epoxy Composite. The paper gives the diversified description of the behavior of the Carbon-Epoxy Composite, under different loadings and conditions. The Carbon-Epoxy Composite was fabricated using various fillers such as, Coremat, Aerosil and Granite. The Composition of the Carbon-Epoxy Composite consists of 50 % Carbon Fiber, 40 % Resin and 10 % fillers by weight. Three different types of Carbon-Epoxy Composite specimen were fabricated using three different Fillers, as mentioned above. The Method Adopted to fabricate the Carbon-Epoxy Composite is conventional Hand Lay-up technique. Furthermore, the Carbon-Epoxy Composite specimen was subjected to various Test Conditions, namely Tensile Test, Impact Test and Water Absorption Test and the behavior of the same is recorded and described in this paper.