• 제목/요약/키워드: Total Efficiency of Turbine

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스윕과 린을 적용한 부분흡입형 초음속 터빈의 성능 특성에 관한 수치적 연구 (Numerical Analysis on the Effect of Blade Sweep and Lean on the Performance of a Partial Admission Supersonic Turbine)

  • 권태운;정수인;조종재;김귀순;정은환
    • 한국추진공학회지
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    • 제15권2호
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    • pp.36-43
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    • 2011
  • 본 논문에서는 스윕과 린의 각도에 따른 부분흡입형 초음속 터빈의 성능 특성을 분석하기 위하여 유동해석을 실시하였다. 유동해석은 스윕과 린의 3가지 각도($5^{\circ}$, $10^{\circ}$, $15^{\circ}$)에 대해 수행되었다. 해석결과, 전반적으로 스윕 각도에 커질수록 효율이 증가하였다. 다만, 스윕 각도가 $5^{\circ}$일 때에는 기본익형보다 효율이 더 떨어졌다. 린 각도가 커질수록 전압력 손실은 줄어들었지만 정효율은 감소하였다.

스윕과 린을 적용한 부분흡입형 초음속 터빈의 성능 특성에 관한 수치적 연구 (Numerical Analysis on the Effect of Blade Sweep and Lean on the Performance of a Partial Admission Supersonic Turbine)

  • 권태운;정수인;조종재;김귀순;정은환
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제35회 추계학술대회논문집
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    • pp.786-792
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    • 2010
  • 본 논문에서는 스윕과 린의 각도에 따른 부분흡입형 초음속 터빈의 성능 특성을 분석하기 위하여 유동해석을 실시하였다. 유동해석은 스윕과 린의 3가지 각도($5^{\circ}$, $10^{\circ}$, $15^{\circ}$)에 대해 수행되었다. 해석결과, 전반적으로 스윕 각도에 커질수록 효율이 증가하였다. 다만, 스윕 각도가 $5^{\circ}$일 때에는 기본익형보다 효율이 더 떨어졌다. 린 각도가 커질수록 전압력 손실은 줄어들었지만 정효율은 감소하였다.

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1.5단 축류 터빈의 익단 유동 특성에 관한 수치해석 (A Numerical Analysis of Tip Flow Characteristics in An 1.5 Stage Axial Turbine)

  • 황동하;정요한;백제현;이동호
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년도 제31회 추계학술대회논문집
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    • pp.157-160
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    • 2008
  • 터빈의 익단 간극은 블레이드와 케이싱간 마찰을 줄이기 위한 중요한 부분이다. 수치 해석을 통해 익단 간극이 직접적으로 터빈에 미치는 영향을 판단하기 위하여 UTRC 터빈을 익단 간극이 있는 경우와 없는 경우로 나눠 계산을 수행하였다. CFX를 통해 도출된 해석결과는, 익단 간극이 있는 경우 생성된 와류가 터빈 전반에 걸친 손실을 일으키고 그 결과 익단 간극이 없는 터빈에 비해 더 낮은 전압효율을 보인다.

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ORC 반경류터빈의 예비설계프로그램 개발 및 OTEC용 반경류터빈의 설계 (The development of a preliminary designing program for ORC radial inflow turbines and the design of the radial inflow turbine for the OTEC)

  • 김도엽;강호근;김유택
    • Journal of Advanced Marine Engineering and Technology
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    • 제38권3호
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    • pp.276-284
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    • 2014
  • 본 연구의 목적은 ORC(Organic Rankine Cycle) 반경류터빈의 설계기법을 확립하는 것이다. 이를 위하여 반경류터빈의 예비설계프로그램인 RTDM(Radial Turbine Design Modeler) Ver.2.1를 개발하였다. RTDM Ver.2.1의 정확성을 검증하기 위해 R32를 이용한 200kW급 OTEC(Ocean Thermal Energy Conversion)용 반경류터빈을 설계하였고 이에 대해 CFD(Computational Fluid Dynamics) 수치해석을 수행하였다. 그 결과 RTDM Ver.2.1의 정확성은 설계한 반경류터빈의 전엔탈피 강하를 기준하여 약 94.6%로 나타났다. 본 연구에서는 반경류터빈의 설계요구조건인 출력조건과 로터출구조건을 충족시키기 위해 질량유량조정 방법을 도입하였다. 이에 따라 RTDM Ver.2.1을 이용하여 설계한 200kW급 OTEC용 반경류터빈의 질량유량은 21.2kg/s이며 이 때 Total to Total과 Total to Static 효율은 각각 89.8%, 85.3%이다.

증기터빈 열병합 시스템에 대한 에너지 및 엑서지 해석 (Energy and Exergy Analysis of a Steam Turbine Cogeneration System)

  • 조성철
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2009년도 하계학술발표대회 논문집
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    • pp.1397-1405
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    • 2009
  • In recent decades, exergy analysis has been holding spotlight as a useful tool in the design, assessment, optimization, and improvement of energy system. This paper presents the results of the energy and exergy analysis of a steam turbine cogeneration system for industrial complex using two efficiency concepts of conventional one and exergetic one. In order to obtain the destroyed exergy of each component, mathematical analysis is conducted by using exergy balance and the second law of thermodynamics, according as the parameters are changed, such as the ratio of returned process steam, process steam supplied, temperature and pressure of boiler and power. The computer program developed in this study can determine the efficiencies and exergy destroyed at each component of cogeneration system. As a result of this study, a component having the largest destroyed exergy was boiler. And closed and opened feedwater heater had the lowest one. The affects to the cogeneration system due to the variation of process steam flow and return rate of condensed water is shown that the total electric power efficiency(${\eta}_E$) is decreased as increasing the return rate of condensed water under constant process steam flow. As the boiler pressure is increased for the more production of electricity, the efficiency of cogeneration system was decreased.

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에너지 저장장치를 이용한 마이크로 그리드의 최적운영 및 신뢰도 지수 개선 (Optimal Operation Scheme and Reliability Index Improvement of Micro Grid Using Energy Storage Systems)

  • 김규호
    • 전기학회논문지
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    • 제63권2호
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    • pp.205-210
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    • 2014
  • The micro grid considered in this paper consists of a diesel generator, a photovoltaic array, a wind turbine, a fuel cell, and a energy storage system. This paper explains and simulates the micro grid components in terms of accuracy and efficiency of having a system model based on the costs of fuel as well as operation and maintenance. For operational efficiency, the objective function in a diesel generator consists of the fuel cost function similar to the cost functions used for the conventional fossil-fuel generating plants. The wind turbine generator is modeled by the characteristics of variable output. The optimization is aimed at minimizing the cost function of the system while constraining it to meet the customer demand and safety of micro grid. The operating cost in fuel-cell system includes the fuel costs and the efficiency for fuel to generate electric power. To develop the overall system model gives a possibility to minimize of the total cost of micro grid. The application of optimal operation can save the interruption costs as well as the operating costs, and improve reliability index in micro grid.

Thermodynamic analysis of a combined gas turbine power plant with a solid oxide fuel cell for marine applications

  • Welaya, Yousri M.A.;Mosleh, M.;Ammar, Nader R.
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제5권4호
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    • pp.529-545
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    • 2013
  • Strong restrictions on emissions from marine power plants (particularly $SO_x$, $NO_x$) will probably be adopted in the near future. In this paper, a combined solid oxide fuel cell (SOFC) and gas turbine fuelled by natural gas is proposed as an attractive option to limit the environmental impact of the marine sector. It includes a study of a heat-recovery system for 18 MW SOFC fuelled by natural gas, to provide the electric power demand onboard commercial vessels. Feasible heat-recovery systems are investigated, taking into account different operating conditions of the combined system. Two types of SOFC are considered, tubular and planar SOFCs, operated with either natural gas or hydrogen fuels. This paper includes a detailed thermodynamic analysis for the combined system. Mass and energy balances are performed, not only for the whole plant but also for each individual component, in order to evaluate the thermal efficiency of the combined cycle. In addition, the effect of using natural gas as a fuel on the fuel cell voltage and performance is investigated. It is found that a high overall efficiency approaching 70% may be achieved with an optimum configuration using SOFC system under pressure. The hybrid system would also reduce emissions, fuel consumption, and improve the total system efficiency.

Numerical Predictions of Roughness Effects on the Performance Degradation of an Axial-Turbine Stage

  • Kang Young-Seok;Yoo Jae-Chun;Kang Shin-Hyoung
    • Journal of Mechanical Science and Technology
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    • 제20권7호
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    • pp.1077-1088
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    • 2006
  • This paper describes a numerical investigation on the performance deteriorations of a low speed, single-stage axial turbine due to use of rough blades. Numerical calculations have been carried out with a commercial CFD code, CFX-Tascflow, by using a modified wall function to implement rough surfaces on the stator vane and rotor blade. To assess the stage performance variations corresponding to 5 equivalent sand-grain roughness heights from a transition ally rough regime to a fully rough regime, stage work coefficient and total to static efficiency were chosen. Numerical results showed that both work coefficient and stage efficiency reduced as roughness height increased. Higher surface roughness induced higher blade loading both on the stator and rotor which in turn resulted in higher deviation angles and corresponding work coefficient reductions. Although, deviation angle changes were small, a simple sensitivity analysis suggested that their contributions on work coefficient reductions were substantial. Higher profile loss coefficients were predicted by higher roughness heights, especially on the suction surface of the stator and rotor. Furthermore sensitivity analysis similar to the above, suggested that additional profile loss generations due to roughness were accountable for efficiency reductions.

1-D Mean Line Flow Model을 이용한 엔진 배기에너지 회수를 위한 터보컴파운드 시스템용 터빈 설계 (Turbine Design for Turbo-compound System to Recover Exhaust Gas Energy Using 1-D Mean Line Flow Model)

  • 장진영;윤정의
    • 한국자동차공학회논문집
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    • 제24권1호
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    • pp.74-81
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    • 2016
  • The aim of this study was to find the initial design value of turbine blade for electrical type turbocompound system generating 10 kW. Turbocompound is one of the waste heat recovery system applying to internal combustion engine to recover exhaust gas energy that was about 30 % of total input energy. To design the turbine blade, 1-D mean line flow model was used. Exhaust gas temperature, pressure, flow rate and turbine rotating speed was fixed as primary boundary conditions. The velocity triangles was defined and used to determine the rotor inlet radius and width, the rotor outlet radius at shroud and radius at hub, the rotor flow angles and the number of blades.

운전조건에 따른 R744용 해양온도차 발전 사이클의 성능 특성 (Performance Characteristics of R744 OTEC Power Cycle with Operation Parameters)

  • 윤정인;손창효;백승문;김현주;이호생
    • Journal of Advanced Marine Engineering and Technology
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    • 제36권5호
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    • pp.580-585
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    • 2012
  • R744용 해양온도차 발전 시스템의 작동변수에 대한 기초 설계자료를 제공하고자 증발열량, 응축열량, 전체일량, 효율에 대한 사이클 성능을 분석하였다. 본 연구에서 고려된 작동변수는 R744 해양온도차 발전 사이클의 과열도, 과냉각도, 응축온도, 증발온도 등이다. 주요 결과를 요약하면 다음과 같다. R744의 증발열량은 과열도와 과냉각도가 증가할수록 증가하는 반면, 응축온도가 증가할수록 감소한다. 전체일량은 R744의 과열도와 과냉각도와 함께 증가하나 증발온도는 증가할수록 감소한다. 그리고 효율은 과열도와 과냉각도가 증가할수록 증가하는 반면, 응축온도는 감소한다. 그러므로 R744용 해양온도차 발전 시스템의 증발열량, 응축열량, 전체일량, 효율은 과열도, 과냉각도, 응축온도, 증발온도, 펌프와 터빈 효율에 영향을 받는 것을 알 수 있었다. 따라서 R744용 해양온도차 발전 시스템의 설계시에는 이러한 영향을 면밀하게 파악하여야 한다.