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145results about How to "High performance features" patented technology

Epitaxial structure for nitride high electron mobility transistors of composite buffer layers

ActiveCN102646700AEnhanced 2DEG localizationImprove frequency performance and power characteristicsSemiconductor devicesElectron mobilityGallium nitride
The invention relates to an epitaxial structure for nitride high electron mobility transistors of composite buffer layers, which includes that a growth nucleating layer is arranged on a substrate; a first buffer layer is arranged on the growth nucleating layer; a second buffer layer is arranged on the first buffer layer; a growth channel layer is arranged on the second buffer layer; and a growth barrier layer is arranged on the growth channel layer. The growth method includes baking the substrate at a high temperature in a reaction chamber after the substrate is washed and dried; growing the nucleating layer on the substrate, the first buffer layer on the nucleating layer, the second buffer layer on the first buffer layer, the growth channel layer on the second buffer layer, and the growth barrier layer on the channel layer; and reducing the temperature to the room temperature. The epitaxial structure for nitride high electron mobility transistors of composite buffer layers has the advantages of being still capable of forming conduction band discontinuity with a gallium nitride (GaN) channel layer, enhancing 2 dimensional electron gas (DEG) confinement, improving microwave performances and power characteristics of devices, being capable of improving the heat conductivity of the buffer layer, and effectively reducing self-heating effect of high electron mobility transistors (HEMT) of AlGaN buffer layer. Quality of crystals of AlyGal-yN buffer layer can be effectively improved, and the epitaxial structure is helpful for further improving the performance and reliability of devices.
Owner:NO 55 INST CHINA ELECTRONIC SCI & TECHNOLOGYGROUP CO LTD

Preparation method of high-power carbon-coated synthetic graphite negative electrode material

The invention relates to the technical field of carbon-coated synthetic graphite negative electrode materials, in particular to a preparation method of a high-power carbon-coated synthetic graphite negative electrode material. The preparation method is characterized by comprising the following steps: crushing coal-measure green coke serving as a raw material A, so as to form a micro powder; crushing and grading asphalt serving a raw material B, so as to form a micro powder; performing modified heat treatment on the micro powder of the raw material A, and then performing normal temperature graphitization in a resistance type graphitization furnace; mixing and sieving obtained materials subjected to graphitization, so as to obtain a single particle graphitization product; uniformly mixing the single particle graphitization product and the micro powder of the raw material B, so as to perform coated modification; performing carbonizing treatment on materials subjected to coated modification, so as to solidify a coated layer; cooling the material to a room temperature, and mixing and sieving, so as to obtain a product. Compared with the prior art, the preparation method has the advantages that the electrode material has smaller reaction impedance, and the low-temperature performance and power characteristic of the material are enhanced; the cycling performance of the material is improved, meanwhile the graphitization cost is reduced, and the purpose of energy conservation is achieved.
Owner:福建杉杉科技有限公司

Vertical axis wind turbine airfoil design method under condition of large attack angle range

The invention discloses a vertical axis wind turbine airfoil design method under the condition of a large attack angle range. The method comprises the following steps: representing an airfoil profileby adopting a method of combining a class function and a B spline, and selecting an NACA0015 symmetric airfoil as an original airfoil; considering three groups of attack angle ranges, respectively establishing a wind turbine airfoil optimization mathematical model taking the maximum sum of tangential moment coefficients as an objective function, compiling a particle swarm optimization program, andcoupling RFOIL software to perform optimization design on the vertical axis wind turbine airfoil. According to the invention, the improvement of the tangential force of the airfoil profile under a large attack angle range is pursued, so that the aerodynamic performance of the whole HVAWT is improved. The novel HVAWT and the initial HVAWT aerodynamic performance are compared and analyzed, the airfoil profile more suitable for the HVAWT is obtained through optimization by optimizing three sets of different attack angle parameter ranges, the blade torque coefficient is integrally improved, and therefore the wind energy utilization rate of the HVAWT can be effectively increased.
Owner:HUBEI UNIV OF TECH
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