• Title/Summary/Keyword: 등엔트로피 노즐 효율

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A Numerical Investigation on the Isentropic Efficiency of Steam Turbine Nozzle Stage with Different Nozzle Vane Thickness and Mass Flow Rate (증기 터빈 노즐 베인의 두께 변화와 유량별 등엔트로피 효율 변화에 관한 수치해석)

  • Lee, Jong Hyeon;Park, Hee Sung;Jung, Jong Yun;Kim, Joon Seob;Jung, Ye Lim;Park, Sung Won
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.41 no.10
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    • pp.685-691
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    • 2017
  • In this study, the influence of mass flow rate on the isentropic efficiency of the steam turbine nozzle stage is investigated. A realistic three-dimensional numerical model, which is based on the compressible Navier-Stokes equations, is developed for the steam phase. The comprehensive conservation laws and a kinetic model for steam are investigated. With two different models for the three-dimensional geometry of the nozzle stage, the pressure and temperature distributions, velocity, Mach number. and Markov energy loss coefficient are calculated. A maximum efficiency of 96.66% is found at a mass flow rate of 0.9 kg/s in model A. In model B, a maximum efficiency of 97.32% is found at a rate of 1.6 kg/s. It is determined that the isentropic nozzle efficiency increases as the Markov energy loss coefficient decreases through a nearly linear relationship.

Influence of Performance and Internal Flow of a Radial Inflow Turbine with Variation of Vane Nozzle Exit Angles (베인노즐 출구각도에 따른 100kW급 구심터빈의 성능 및 내부유동의 영향)

  • Mo, Jang-Oh;Kim, You-Taek;Oh, Cheol;Lee, Young-Ho
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.6
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    • pp.757-764
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    • 2011
  • In this study, we analysed the influence of the performance and inflow flow of a radial inflow turbine with the variation of vane nozzle exit angles for a 100kW class turbine applicable in the waste heat recovery system. For this, three-dimensional CFD analysis was performed using commercial code called ANSYS Fluent 12.1. As the vane nozzle exit angle was more increased the reattachment region near blades of the vane nozzle got smaller, and also the Mach number at vane nozzle exit was observed to be 1 due to the effect of the cross section reduction. Through this study, we expect that the analysed results will be used as the design material for the composition of the turbine optimal design parameters corresponding to the target output power.

Performance Analysis by CFD and Aerodynamic Design of 100kW Class Radial Turbine Using Waste Heat from Ship (선박 폐열을 이용한 100kW급 구심터빈 공력설계 및 CFD에 의한 성능해석)

  • Mo, Jang-Oh;Kim, You-Taek;Kim, Mann-Eung;Oh, Cheol;Kim, Jeong-Hwan;Lee, Young-Ho
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.2
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    • pp.175-181
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    • 2011
  • The purpose of this study is to secure the design data for the optimization of the radial turbine and heat cycle system, by using the CFD analysis technique and the design of 100kW class radial turbine applicable to waste heat recovery generation system for ship. Radial turbine was comprised of scroll casing, vane nozzle with 18 blades and rotor with 13 blades, and analysis grid was used to about 2.3 million. Mass flow rate and rotational speed was 0.5kg/s, 75,0000rpm, respectively. Eight kinds of inlet pressure was set between 195 and 620kPa. As the flow accelerated through the nozzle passage to the throat, the pressure level at the pressure and suction sides becomed similar to about Mach number of 0.35. When the inlet temperature and pressure was $250^{\circ}C$, 352kPa respectively, the isentropic efficiency and mechanical power showed the analysis results of 74% and 108kW.