The Experts below are selected from a list of 300 Experts worldwide ranked by ideXlab platform
Fengchun Jiang - One of the best experts on this subject based on the ideXlab platform.
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synthesis and mechanical properties of novel ti sicf al3ti ceramic Fiber Reinforced Metal interMetallic laminated cfr mil composites
Journal of Alloys and Compounds, 2017Co-Authors: Chunfa Lin, Chunhuan Guo, Xiaoxiao Han, Yuqiang Han, Yunpeng Chang, Lin Lan, Fengchun JiangAbstract:Abstract The innovative Ti-(SiC f /Al 3 Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites were successfully fabricated by vacuum hot pressing using titanium foils, aluminum foils and SiC ceramic Fibers. The synthesized Ti-(SiC f /Al 3 Ti) composite showed a unique multilayered microstructure consisting of alternating SiC f /Al 3 Ti composite layers (SiC Fiber as reinforcement) and Ti layers. In addition, reaction annealing technique was employed to improve the interfacial performance of SiC Fiber with Al 3 Ti matrix. The microstructure evolution of the laminated composite during hot-pressing and annealing was experimentally characterized using scanning electron microscopy and energy dispersive spectroscopy. The formation mechanism of micro-laminated structure was discussed. Furthermore, the mechanical properties of the Ti-(SiC f /Al 3 Ti) laminated composite and its components were investigated by tensile and nanoindentation tests. The results indicated that Ti-(SiC f /Al 3 Ti) laminated composite exhibited superior mechanical properties compared to Ti-Al 3 Ti, which was likely attributed to the introduction of SiC Fiber. The failure mechanism of CFR-MIL composite was the combined fracture behaviors of ductile fracture of Ti, brittle fracture of Al 3 Ti and Fiber debonding, pullout and breakage of SiC.
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Synthesis and mechanical properties of novel Ti-(SiCf/Al3Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites
Journal of Alloys and Compounds, 2017Co-Authors: Chunfa Lin, Chunhuan Guo, Xiaoxiao Han, Yuqiang Han, Yunpeng Chang, Lin Lan, Fengchun JiangAbstract:Abstract The innovative Ti-(SiC f /Al 3 Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites were successfully fabricated by vacuum hot pressing using titanium foils, aluminum foils and SiC ceramic Fibers. The synthesized Ti-(SiC f /Al 3 Ti) composite showed a unique multilayered microstructure consisting of alternating SiC f /Al 3 Ti composite layers (SiC Fiber as reinforcement) and Ti layers. In addition, reaction annealing technique was employed to improve the interfacial performance of SiC Fiber with Al 3 Ti matrix. The microstructure evolution of the laminated composite during hot-pressing and annealing was experimentally characterized using scanning electron microscopy and energy dispersive spectroscopy. The formation mechanism of micro-laminated structure was discussed. Furthermore, the mechanical properties of the Ti-(SiC f /Al 3 Ti) laminated composite and its components were investigated by tensile and nanoindentation tests. The results indicated that Ti-(SiC f /Al 3 Ti) laminated composite exhibited superior mechanical properties compared to Ti-Al 3 Ti, which was likely attributed to the introduction of SiC Fiber. The failure mechanism of CFR-MIL composite was the combined fracture behaviors of ductile fracture of Ti, brittle fracture of Al 3 Ti and Fiber debonding, pullout and breakage of SiC.
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fabrication mechanical properties and damping capacity of shape memory alloy niti Fiber Reinforced Metal interMetallic laminate smafr mil composite
Materials & Design, 2016Co-Authors: Enhao Wang, Chunhuan Guo, Peijun Zhou, Chunfa Lin, Xiaoxiao Han, Fengchun JiangAbstract:Abstract A novel Shape Memory Alloy NiTi Fiber-Reinforced Metal-interMetallic–laminate (SMAFR-MIL) composite with a volume fraction of ~ 3.5% NiTi was fabricated using vacuum hot pressing method in this paper. The microstructure characterization of this laminate composite was performed by scanning electron microscope (SEM), energy dispersive spectrometer (EDS) and X-ray diffractometer (XRD), and the mechanical property of SMAFR-MIL composite was determined by compression test. In addition, damping capacity was measured using Dynamic Mechanical Analyzer (DMA) in a temperature range from 30 °C to 50 °C. The experimental results indicated that the average compressive strength and the strain to failure are ~ 1208 MPa and ~ 4.4% for loading perpendicular to the layers, and ~ 962 MPa and ~ 4.8% for loading parallel to the layers, respectively. The loss modulus of SMAFR-MIL composite is ~ 3.7 GPa, which is five times greater than that of Ti/Al3Ti laminate composite without NiTi Fiber reinforcement, while the damping factor of SMAFR-MIL composite is ~ 4.5%. Both the mechanical and damping tests demonstrated that SMAFR-MIL composite is a new class of structural and functional composite with superior mechanical and damping properties.
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Fabrication, mechanical properties and damping capacity of shape memory alloy NiTi Fiber-Reinforced Metal–interMetallic–laminate (SMAFR-MIL) composite
Materials & Design, 2016Co-Authors: Enhao Wang, Chunhuan Guo, Peijun Zhou, Chunfa Lin, Xiaoxiao Han, Fengchun JiangAbstract:Abstract A novel Shape Memory Alloy NiTi Fiber-Reinforced Metal-interMetallic–laminate (SMAFR-MIL) composite with a volume fraction of ~ 3.5% NiTi was fabricated using vacuum hot pressing method in this paper. The microstructure characterization of this laminate composite was performed by scanning electron microscope (SEM), energy dispersive spectrometer (EDS) and X-ray diffractometer (XRD), and the mechanical property of SMAFR-MIL composite was determined by compression test. In addition, damping capacity was measured using Dynamic Mechanical Analyzer (DMA) in a temperature range from 30 °C to 50 °C. The experimental results indicated that the average compressive strength and the strain to failure are ~ 1208 MPa and ~ 4.4% for loading perpendicular to the layers, and ~ 962 MPa and ~ 4.8% for loading parallel to the layers, respectively. The loss modulus of SMAFR-MIL composite is ~ 3.7 GPa, which is five times greater than that of Ti/Al3Ti laminate composite without NiTi Fiber reinforcement, while the damping factor of SMAFR-MIL composite is ~ 4.5%. Both the mechanical and damping tests demonstrated that SMAFR-MIL composite is a new class of structural and functional composite with superior mechanical and damping properties.
Chunfa Lin - One of the best experts on this subject based on the ideXlab platform.
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synthesis and mechanical properties of novel ti sicf al3ti ceramic Fiber Reinforced Metal interMetallic laminated cfr mil composites
Journal of Alloys and Compounds, 2017Co-Authors: Chunfa Lin, Chunhuan Guo, Xiaoxiao Han, Yuqiang Han, Yunpeng Chang, Lin Lan, Fengchun JiangAbstract:Abstract The innovative Ti-(SiC f /Al 3 Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites were successfully fabricated by vacuum hot pressing using titanium foils, aluminum foils and SiC ceramic Fibers. The synthesized Ti-(SiC f /Al 3 Ti) composite showed a unique multilayered microstructure consisting of alternating SiC f /Al 3 Ti composite layers (SiC Fiber as reinforcement) and Ti layers. In addition, reaction annealing technique was employed to improve the interfacial performance of SiC Fiber with Al 3 Ti matrix. The microstructure evolution of the laminated composite during hot-pressing and annealing was experimentally characterized using scanning electron microscopy and energy dispersive spectroscopy. The formation mechanism of micro-laminated structure was discussed. Furthermore, the mechanical properties of the Ti-(SiC f /Al 3 Ti) laminated composite and its components were investigated by tensile and nanoindentation tests. The results indicated that Ti-(SiC f /Al 3 Ti) laminated composite exhibited superior mechanical properties compared to Ti-Al 3 Ti, which was likely attributed to the introduction of SiC Fiber. The failure mechanism of CFR-MIL composite was the combined fracture behaviors of ductile fracture of Ti, brittle fracture of Al 3 Ti and Fiber debonding, pullout and breakage of SiC.
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Synthesis and mechanical properties of novel Ti-(SiCf/Al3Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites
Journal of Alloys and Compounds, 2017Co-Authors: Chunfa Lin, Chunhuan Guo, Xiaoxiao Han, Yuqiang Han, Yunpeng Chang, Lin Lan, Fengchun JiangAbstract:Abstract The innovative Ti-(SiC f /Al 3 Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites were successfully fabricated by vacuum hot pressing using titanium foils, aluminum foils and SiC ceramic Fibers. The synthesized Ti-(SiC f /Al 3 Ti) composite showed a unique multilayered microstructure consisting of alternating SiC f /Al 3 Ti composite layers (SiC Fiber as reinforcement) and Ti layers. In addition, reaction annealing technique was employed to improve the interfacial performance of SiC Fiber with Al 3 Ti matrix. The microstructure evolution of the laminated composite during hot-pressing and annealing was experimentally characterized using scanning electron microscopy and energy dispersive spectroscopy. The formation mechanism of micro-laminated structure was discussed. Furthermore, the mechanical properties of the Ti-(SiC f /Al 3 Ti) laminated composite and its components were investigated by tensile and nanoindentation tests. The results indicated that Ti-(SiC f /Al 3 Ti) laminated composite exhibited superior mechanical properties compared to Ti-Al 3 Ti, which was likely attributed to the introduction of SiC Fiber. The failure mechanism of CFR-MIL composite was the combined fracture behaviors of ductile fracture of Ti, brittle fracture of Al 3 Ti and Fiber debonding, pullout and breakage of SiC.
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fabrication mechanical properties and damping capacity of shape memory alloy niti Fiber Reinforced Metal interMetallic laminate smafr mil composite
Materials & Design, 2016Co-Authors: Enhao Wang, Chunhuan Guo, Peijun Zhou, Chunfa Lin, Xiaoxiao Han, Fengchun JiangAbstract:Abstract A novel Shape Memory Alloy NiTi Fiber-Reinforced Metal-interMetallic–laminate (SMAFR-MIL) composite with a volume fraction of ~ 3.5% NiTi was fabricated using vacuum hot pressing method in this paper. The microstructure characterization of this laminate composite was performed by scanning electron microscope (SEM), energy dispersive spectrometer (EDS) and X-ray diffractometer (XRD), and the mechanical property of SMAFR-MIL composite was determined by compression test. In addition, damping capacity was measured using Dynamic Mechanical Analyzer (DMA) in a temperature range from 30 °C to 50 °C. The experimental results indicated that the average compressive strength and the strain to failure are ~ 1208 MPa and ~ 4.4% for loading perpendicular to the layers, and ~ 962 MPa and ~ 4.8% for loading parallel to the layers, respectively. The loss modulus of SMAFR-MIL composite is ~ 3.7 GPa, which is five times greater than that of Ti/Al3Ti laminate composite without NiTi Fiber reinforcement, while the damping factor of SMAFR-MIL composite is ~ 4.5%. Both the mechanical and damping tests demonstrated that SMAFR-MIL composite is a new class of structural and functional composite with superior mechanical and damping properties.
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Fabrication, mechanical properties and damping capacity of shape memory alloy NiTi Fiber-Reinforced Metal–interMetallic–laminate (SMAFR-MIL) composite
Materials & Design, 2016Co-Authors: Enhao Wang, Chunhuan Guo, Peijun Zhou, Chunfa Lin, Xiaoxiao Han, Fengchun JiangAbstract:Abstract A novel Shape Memory Alloy NiTi Fiber-Reinforced Metal-interMetallic–laminate (SMAFR-MIL) composite with a volume fraction of ~ 3.5% NiTi was fabricated using vacuum hot pressing method in this paper. The microstructure characterization of this laminate composite was performed by scanning electron microscope (SEM), energy dispersive spectrometer (EDS) and X-ray diffractometer (XRD), and the mechanical property of SMAFR-MIL composite was determined by compression test. In addition, damping capacity was measured using Dynamic Mechanical Analyzer (DMA) in a temperature range from 30 °C to 50 °C. The experimental results indicated that the average compressive strength and the strain to failure are ~ 1208 MPa and ~ 4.4% for loading perpendicular to the layers, and ~ 962 MPa and ~ 4.8% for loading parallel to the layers, respectively. The loss modulus of SMAFR-MIL composite is ~ 3.7 GPa, which is five times greater than that of Ti/Al3Ti laminate composite without NiTi Fiber reinforcement, while the damping factor of SMAFR-MIL composite is ~ 4.5%. Both the mechanical and damping tests demonstrated that SMAFR-MIL composite is a new class of structural and functional composite with superior mechanical and damping properties.
Xiaoxiao Han - One of the best experts on this subject based on the ideXlab platform.
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synthesis and mechanical properties of novel ti sicf al3ti ceramic Fiber Reinforced Metal interMetallic laminated cfr mil composites
Journal of Alloys and Compounds, 2017Co-Authors: Chunfa Lin, Chunhuan Guo, Xiaoxiao Han, Yuqiang Han, Yunpeng Chang, Lin Lan, Fengchun JiangAbstract:Abstract The innovative Ti-(SiC f /Al 3 Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites were successfully fabricated by vacuum hot pressing using titanium foils, aluminum foils and SiC ceramic Fibers. The synthesized Ti-(SiC f /Al 3 Ti) composite showed a unique multilayered microstructure consisting of alternating SiC f /Al 3 Ti composite layers (SiC Fiber as reinforcement) and Ti layers. In addition, reaction annealing technique was employed to improve the interfacial performance of SiC Fiber with Al 3 Ti matrix. The microstructure evolution of the laminated composite during hot-pressing and annealing was experimentally characterized using scanning electron microscopy and energy dispersive spectroscopy. The formation mechanism of micro-laminated structure was discussed. Furthermore, the mechanical properties of the Ti-(SiC f /Al 3 Ti) laminated composite and its components were investigated by tensile and nanoindentation tests. The results indicated that Ti-(SiC f /Al 3 Ti) laminated composite exhibited superior mechanical properties compared to Ti-Al 3 Ti, which was likely attributed to the introduction of SiC Fiber. The failure mechanism of CFR-MIL composite was the combined fracture behaviors of ductile fracture of Ti, brittle fracture of Al 3 Ti and Fiber debonding, pullout and breakage of SiC.
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Synthesis and mechanical properties of novel Ti-(SiCf/Al3Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites
Journal of Alloys and Compounds, 2017Co-Authors: Chunfa Lin, Chunhuan Guo, Xiaoxiao Han, Yuqiang Han, Yunpeng Chang, Lin Lan, Fengchun JiangAbstract:Abstract The innovative Ti-(SiC f /Al 3 Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites were successfully fabricated by vacuum hot pressing using titanium foils, aluminum foils and SiC ceramic Fibers. The synthesized Ti-(SiC f /Al 3 Ti) composite showed a unique multilayered microstructure consisting of alternating SiC f /Al 3 Ti composite layers (SiC Fiber as reinforcement) and Ti layers. In addition, reaction annealing technique was employed to improve the interfacial performance of SiC Fiber with Al 3 Ti matrix. The microstructure evolution of the laminated composite during hot-pressing and annealing was experimentally characterized using scanning electron microscopy and energy dispersive spectroscopy. The formation mechanism of micro-laminated structure was discussed. Furthermore, the mechanical properties of the Ti-(SiC f /Al 3 Ti) laminated composite and its components were investigated by tensile and nanoindentation tests. The results indicated that Ti-(SiC f /Al 3 Ti) laminated composite exhibited superior mechanical properties compared to Ti-Al 3 Ti, which was likely attributed to the introduction of SiC Fiber. The failure mechanism of CFR-MIL composite was the combined fracture behaviors of ductile fracture of Ti, brittle fracture of Al 3 Ti and Fiber debonding, pullout and breakage of SiC.
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fabrication mechanical properties and damping capacity of shape memory alloy niti Fiber Reinforced Metal interMetallic laminate smafr mil composite
Materials & Design, 2016Co-Authors: Enhao Wang, Chunhuan Guo, Peijun Zhou, Chunfa Lin, Xiaoxiao Han, Fengchun JiangAbstract:Abstract A novel Shape Memory Alloy NiTi Fiber-Reinforced Metal-interMetallic–laminate (SMAFR-MIL) composite with a volume fraction of ~ 3.5% NiTi was fabricated using vacuum hot pressing method in this paper. The microstructure characterization of this laminate composite was performed by scanning electron microscope (SEM), energy dispersive spectrometer (EDS) and X-ray diffractometer (XRD), and the mechanical property of SMAFR-MIL composite was determined by compression test. In addition, damping capacity was measured using Dynamic Mechanical Analyzer (DMA) in a temperature range from 30 °C to 50 °C. The experimental results indicated that the average compressive strength and the strain to failure are ~ 1208 MPa and ~ 4.4% for loading perpendicular to the layers, and ~ 962 MPa and ~ 4.8% for loading parallel to the layers, respectively. The loss modulus of SMAFR-MIL composite is ~ 3.7 GPa, which is five times greater than that of Ti/Al3Ti laminate composite without NiTi Fiber reinforcement, while the damping factor of SMAFR-MIL composite is ~ 4.5%. Both the mechanical and damping tests demonstrated that SMAFR-MIL composite is a new class of structural and functional composite with superior mechanical and damping properties.
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Fabrication, mechanical properties and damping capacity of shape memory alloy NiTi Fiber-Reinforced Metal–interMetallic–laminate (SMAFR-MIL) composite
Materials & Design, 2016Co-Authors: Enhao Wang, Chunhuan Guo, Peijun Zhou, Chunfa Lin, Xiaoxiao Han, Fengchun JiangAbstract:Abstract A novel Shape Memory Alloy NiTi Fiber-Reinforced Metal-interMetallic–laminate (SMAFR-MIL) composite with a volume fraction of ~ 3.5% NiTi was fabricated using vacuum hot pressing method in this paper. The microstructure characterization of this laminate composite was performed by scanning electron microscope (SEM), energy dispersive spectrometer (EDS) and X-ray diffractometer (XRD), and the mechanical property of SMAFR-MIL composite was determined by compression test. In addition, damping capacity was measured using Dynamic Mechanical Analyzer (DMA) in a temperature range from 30 °C to 50 °C. The experimental results indicated that the average compressive strength and the strain to failure are ~ 1208 MPa and ~ 4.4% for loading perpendicular to the layers, and ~ 962 MPa and ~ 4.8% for loading parallel to the layers, respectively. The loss modulus of SMAFR-MIL composite is ~ 3.7 GPa, which is five times greater than that of Ti/Al3Ti laminate composite without NiTi Fiber reinforcement, while the damping factor of SMAFR-MIL composite is ~ 4.5%. Both the mechanical and damping tests demonstrated that SMAFR-MIL composite is a new class of structural and functional composite with superior mechanical and damping properties.
Chunhuan Guo - One of the best experts on this subject based on the ideXlab platform.
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synthesis and mechanical properties of novel ti sicf al3ti ceramic Fiber Reinforced Metal interMetallic laminated cfr mil composites
Journal of Alloys and Compounds, 2017Co-Authors: Chunfa Lin, Chunhuan Guo, Xiaoxiao Han, Yuqiang Han, Yunpeng Chang, Lin Lan, Fengchun JiangAbstract:Abstract The innovative Ti-(SiC f /Al 3 Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites were successfully fabricated by vacuum hot pressing using titanium foils, aluminum foils and SiC ceramic Fibers. The synthesized Ti-(SiC f /Al 3 Ti) composite showed a unique multilayered microstructure consisting of alternating SiC f /Al 3 Ti composite layers (SiC Fiber as reinforcement) and Ti layers. In addition, reaction annealing technique was employed to improve the interfacial performance of SiC Fiber with Al 3 Ti matrix. The microstructure evolution of the laminated composite during hot-pressing and annealing was experimentally characterized using scanning electron microscopy and energy dispersive spectroscopy. The formation mechanism of micro-laminated structure was discussed. Furthermore, the mechanical properties of the Ti-(SiC f /Al 3 Ti) laminated composite and its components were investigated by tensile and nanoindentation tests. The results indicated that Ti-(SiC f /Al 3 Ti) laminated composite exhibited superior mechanical properties compared to Ti-Al 3 Ti, which was likely attributed to the introduction of SiC Fiber. The failure mechanism of CFR-MIL composite was the combined fracture behaviors of ductile fracture of Ti, brittle fracture of Al 3 Ti and Fiber debonding, pullout and breakage of SiC.
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Synthesis and mechanical properties of novel Ti-(SiCf/Al3Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites
Journal of Alloys and Compounds, 2017Co-Authors: Chunfa Lin, Chunhuan Guo, Xiaoxiao Han, Yuqiang Han, Yunpeng Chang, Lin Lan, Fengchun JiangAbstract:Abstract The innovative Ti-(SiC f /Al 3 Ti) ceramic-Fiber-Reinforced Metal-interMetallic-laminated (CFR-MIL) composites were successfully fabricated by vacuum hot pressing using titanium foils, aluminum foils and SiC ceramic Fibers. The synthesized Ti-(SiC f /Al 3 Ti) composite showed a unique multilayered microstructure consisting of alternating SiC f /Al 3 Ti composite layers (SiC Fiber as reinforcement) and Ti layers. In addition, reaction annealing technique was employed to improve the interfacial performance of SiC Fiber with Al 3 Ti matrix. The microstructure evolution of the laminated composite during hot-pressing and annealing was experimentally characterized using scanning electron microscopy and energy dispersive spectroscopy. The formation mechanism of micro-laminated structure was discussed. Furthermore, the mechanical properties of the Ti-(SiC f /Al 3 Ti) laminated composite and its components were investigated by tensile and nanoindentation tests. The results indicated that Ti-(SiC f /Al 3 Ti) laminated composite exhibited superior mechanical properties compared to Ti-Al 3 Ti, which was likely attributed to the introduction of SiC Fiber. The failure mechanism of CFR-MIL composite was the combined fracture behaviors of ductile fracture of Ti, brittle fracture of Al 3 Ti and Fiber debonding, pullout and breakage of SiC.
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fabrication mechanical properties and damping capacity of shape memory alloy niti Fiber Reinforced Metal interMetallic laminate smafr mil composite
Materials & Design, 2016Co-Authors: Enhao Wang, Chunhuan Guo, Peijun Zhou, Chunfa Lin, Xiaoxiao Han, Fengchun JiangAbstract:Abstract A novel Shape Memory Alloy NiTi Fiber-Reinforced Metal-interMetallic–laminate (SMAFR-MIL) composite with a volume fraction of ~ 3.5% NiTi was fabricated using vacuum hot pressing method in this paper. The microstructure characterization of this laminate composite was performed by scanning electron microscope (SEM), energy dispersive spectrometer (EDS) and X-ray diffractometer (XRD), and the mechanical property of SMAFR-MIL composite was determined by compression test. In addition, damping capacity was measured using Dynamic Mechanical Analyzer (DMA) in a temperature range from 30 °C to 50 °C. The experimental results indicated that the average compressive strength and the strain to failure are ~ 1208 MPa and ~ 4.4% for loading perpendicular to the layers, and ~ 962 MPa and ~ 4.8% for loading parallel to the layers, respectively. The loss modulus of SMAFR-MIL composite is ~ 3.7 GPa, which is five times greater than that of Ti/Al3Ti laminate composite without NiTi Fiber reinforcement, while the damping factor of SMAFR-MIL composite is ~ 4.5%. Both the mechanical and damping tests demonstrated that SMAFR-MIL composite is a new class of structural and functional composite with superior mechanical and damping properties.
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Fabrication, mechanical properties and damping capacity of shape memory alloy NiTi Fiber-Reinforced Metal–interMetallic–laminate (SMAFR-MIL) composite
Materials & Design, 2016Co-Authors: Enhao Wang, Chunhuan Guo, Peijun Zhou, Chunfa Lin, Xiaoxiao Han, Fengchun JiangAbstract:Abstract A novel Shape Memory Alloy NiTi Fiber-Reinforced Metal-interMetallic–laminate (SMAFR-MIL) composite with a volume fraction of ~ 3.5% NiTi was fabricated using vacuum hot pressing method in this paper. The microstructure characterization of this laminate composite was performed by scanning electron microscope (SEM), energy dispersive spectrometer (EDS) and X-ray diffractometer (XRD), and the mechanical property of SMAFR-MIL composite was determined by compression test. In addition, damping capacity was measured using Dynamic Mechanical Analyzer (DMA) in a temperature range from 30 °C to 50 °C. The experimental results indicated that the average compressive strength and the strain to failure are ~ 1208 MPa and ~ 4.4% for loading perpendicular to the layers, and ~ 962 MPa and ~ 4.8% for loading parallel to the layers, respectively. The loss modulus of SMAFR-MIL composite is ~ 3.7 GPa, which is five times greater than that of Ti/Al3Ti laminate composite without NiTi Fiber reinforcement, while the damping factor of SMAFR-MIL composite is ~ 4.5%. Both the mechanical and damping tests demonstrated that SMAFR-MIL composite is a new class of structural and functional composite with superior mechanical and damping properties.
Enhao Wang - One of the best experts on this subject based on the ideXlab platform.
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fabrication mechanical properties and damping capacity of shape memory alloy niti Fiber Reinforced Metal interMetallic laminate smafr mil composite
Materials & Design, 2016Co-Authors: Enhao Wang, Chunhuan Guo, Peijun Zhou, Chunfa Lin, Xiaoxiao Han, Fengchun JiangAbstract:Abstract A novel Shape Memory Alloy NiTi Fiber-Reinforced Metal-interMetallic–laminate (SMAFR-MIL) composite with a volume fraction of ~ 3.5% NiTi was fabricated using vacuum hot pressing method in this paper. The microstructure characterization of this laminate composite was performed by scanning electron microscope (SEM), energy dispersive spectrometer (EDS) and X-ray diffractometer (XRD), and the mechanical property of SMAFR-MIL composite was determined by compression test. In addition, damping capacity was measured using Dynamic Mechanical Analyzer (DMA) in a temperature range from 30 °C to 50 °C. The experimental results indicated that the average compressive strength and the strain to failure are ~ 1208 MPa and ~ 4.4% for loading perpendicular to the layers, and ~ 962 MPa and ~ 4.8% for loading parallel to the layers, respectively. The loss modulus of SMAFR-MIL composite is ~ 3.7 GPa, which is five times greater than that of Ti/Al3Ti laminate composite without NiTi Fiber reinforcement, while the damping factor of SMAFR-MIL composite is ~ 4.5%. Both the mechanical and damping tests demonstrated that SMAFR-MIL composite is a new class of structural and functional composite with superior mechanical and damping properties.
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Fabrication, mechanical properties and damping capacity of shape memory alloy NiTi Fiber-Reinforced Metal–interMetallic–laminate (SMAFR-MIL) composite
Materials & Design, 2016Co-Authors: Enhao Wang, Chunhuan Guo, Peijun Zhou, Chunfa Lin, Xiaoxiao Han, Fengchun JiangAbstract:Abstract A novel Shape Memory Alloy NiTi Fiber-Reinforced Metal-interMetallic–laminate (SMAFR-MIL) composite with a volume fraction of ~ 3.5% NiTi was fabricated using vacuum hot pressing method in this paper. The microstructure characterization of this laminate composite was performed by scanning electron microscope (SEM), energy dispersive spectrometer (EDS) and X-ray diffractometer (XRD), and the mechanical property of SMAFR-MIL composite was determined by compression test. In addition, damping capacity was measured using Dynamic Mechanical Analyzer (DMA) in a temperature range from 30 °C to 50 °C. The experimental results indicated that the average compressive strength and the strain to failure are ~ 1208 MPa and ~ 4.4% for loading perpendicular to the layers, and ~ 962 MPa and ~ 4.8% for loading parallel to the layers, respectively. The loss modulus of SMAFR-MIL composite is ~ 3.7 GPa, which is five times greater than that of Ti/Al3Ti laminate composite without NiTi Fiber reinforcement, while the damping factor of SMAFR-MIL composite is ~ 4.5%. Both the mechanical and damping tests demonstrated that SMAFR-MIL composite is a new class of structural and functional composite with superior mechanical and damping properties.