萨赫勒地区农村太阳能微型燃气轮机设计与CFD建模

Ababacar Thiam, E. Cissé, B. A. Ndiogou, Kory Faye, Mactar Faye
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摘要

本文提出了一种用于萨赫勒农村地区的微型太阳能燃气轮机的数值设计。采用热力学分析、Mean Line Method、Ansys Blade Gen、Ansys CFX Turbo Grid和Ansys CFX求解器进行了概念研究和数值分析。太阳能微型燃气轮机的平均线设计结果为:转速为11.5万rpm,压比为4,膨胀功率为40.28 kW,压缩功率为29.97 kW,风量为0.14 kg。s−1和涡轮入口温度等于850°C。汽轮机总效率为80%,压气机多向效率为79%。涡轮转子有13片叶片,压气机转子有18片主、副叶片。本文提出了一种用于萨赫勒农村地区的微型太阳能燃气轮机的数值设计。采用热力学分析、Mean Line Method、Ansys Blade Gen、Ansys CFX Turbo Grid和Ansys CFX求解器进行了概念研究和数值分析。太阳能微型燃气轮机的平均线设计结果为:转速为11.5万rpm,压比为4,膨胀功率为40.28 kW,压缩功率为29.97 kW,风量为0.14 kg。s−1和涡轮入口温度等于850°C。汽轮机总效率为80%,压气机多向效率为79%。涡轮转子有13片叶片,压气机转子有18片主、副叶片。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and CFD modeling of a solar micro gas turbine for rural zones in Sahel
This work presents a numerical design of a micro solar gas turbine for the rural areas of Sahel. Thermodynamic analysis, Mean Line Method, Ansys Blade Gen, Ansys CFX Turbo Grid and Ansys CFX solver were used to do the conceptual study and numerical analysis. The Mean line design results of solar micro gas turbine give a rotation speed of 115,000 rpm, a pressure ratio of 4, an expansion power equal to 40.28 kW and a compression power equal to 29.97 kW for an air flow of 0.14 kg.s−1 and a turbine inlet temperature equal to 850°C. Total to total turbine efficiency is 80% while compressor polytropic efficiency is 79%. The turbine rotor has 13 blades while that of the compressor consists of 18 main and secondary blades.This work presents a numerical design of a micro solar gas turbine for the rural areas of Sahel. Thermodynamic analysis, Mean Line Method, Ansys Blade Gen, Ansys CFX Turbo Grid and Ansys CFX solver were used to do the conceptual study and numerical analysis. The Mean line design results of solar micro gas turbine give a rotation speed of 115,000 rpm, a pressure ratio of 4, an expansion power equal to 40.28 kW and a compression power equal to 29.97 kW for an air flow of 0.14 kg.s−1 and a turbine inlet temperature equal to 850°C. Total to total turbine efficiency is 80% while compressor polytropic efficiency is 79%. The turbine rotor has 13 blades while that of the compressor consists of 18 main and secondary blades.
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