마이크로 가스터빈 내의 열유동해석 Heat and Flow Analysis in the Micro Gas Turbine
한국기계기술학회지
(韓國機械技術學會誌)
제17권 제3호
(2015.06)
pp.539-544
pp.539-544
한국기계기술학회
(Korean Society of Mechanical Technology)
초록
This research is to investigate the performance analysis of micro gas turbine for power generation with three different numbers of the nozzle vane in the micro gas turbine. Velocity, pressure. and temperature distributions of fluid over the flow domain of the turbine and turbulent kinetic energy of three different turbine blades are numerically calculated for the optimum design of turbine blade with two different rotational speeds of the turbine blade (10000 and 20000 RPM). Ultimately, the energy-efficient and maximum power-generated shape of the nozzle vane are determined through two different rotational speeds of the turbine with three shapes of the nozzle vane (6, 8, and 12 EA).
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