• 제목/요약/키워드: High Pressure Turbine

검색결과 457건 처리시간 0.037초

초음속 충동형 터빈에 대한 시험적 고찰 (Experiments on Supersonic Impulse Turbine)

  • 정은환;김진한
    • 한국유체기계학회 논문집
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    • 제8권6호
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    • pp.26-32
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    • 2005
  • 1.6 MW class supersonic partial admission impulse turbine has been designed and tested in Korea Aerospace Research Institute for the liquid rocket engine application. The test has been performed using a high pressure air source facility in KARI. For the turbine power absorption, a hydraulic dynamometer has been used. Appropriate similarity relations are used for the determination of test condition. Various settings of turbine pressure ratio and rotational speed are tested to investigate global turbine characteristics. From measured data, parameters related to the turbine design are derived and validated.

초음속 충동형 터빈에 대한 시험적 연구 (Experiments on Supersonic Impulse Turbine)

  • 정은환;이은석;김진한
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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    • pp.125-131
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    • 2004
  • 1.6 MW class supersonic partial admission impulse turbine has been designed and tested in Korea Aerospace Research Institute for the liquid rocket engine application. The test has been performed using a high pressure air source facility in KARI. For the turbine power absorption, a hydraulic dynamometer is used. Appropriate similarity relations are used for the determination of test condition. Various settings of turbine pressure ratio and rotational speed are tested to investigate global turbine characteristics. From measured data, Parameters related to the turbine design are derived and validated.

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Effects of Turbine Inlet Temperature on Performance of Regenerative Gas Turbine System with Afterfogging

  • Kim, Kyoung-Hoon;Kim, Se-Woong;Ko, Hyung-Jong
    • International Journal of Air-Conditioning and Refrigeration
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    • 제17권4호
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    • pp.141-148
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    • 2009
  • Afterfogging of the regenerative gas turbine system has an advantage over inlet fogging in that the high outlet temperature of air compressor makes the injection of more water and the recuperation of more exhaust heat possible. This study investigates the effects of turbine inlet temperature (TIT) on the performance of regenerative gas turbine system with afterfogging through a thermodynamic analysis model. For the standard ambient conditions and the water injection ratios up to 5%, the variation of system performance including the thermal efficiency is numerically analyzed with respect to the variations of TIT and pressure ratio. It is also analyzed how the maximum thermal efficiency, net specific work, and pressure ratio itself change with TIT at the peak points of thermal efficiency curve. All of these are found to increase almost linearly with the increases of both TIT and water injection ratio.

터빈 운전 신뢰성 향상을 위한 응력부식균열 평가 (The Evaluation of the Stress Corrosion Cracking for Improvement of Reliability in Turbine Operation and Maintenance)

  • 강용호;송정일
    • 한국태양에너지학회:학술대회논문집
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    • 한국태양에너지학회 2008년도 추계학술발표대회 논문집
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    • pp.280-287
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    • 2008
  • In case of low pressure steam turbine used in power plant, it was operated in wet steam and high stress condition. Therefore, it is possible that the corrosion damage of low pressure was induced by this condition. According to previous study, about 30% of total blade failure correspond to corrosion fatigue or SCC(stress corrosion cracking) in low pressure turbine. Especially, LSB(last stage bucket) of low pressure turbine has a higher hardness to prevent erosion damage due to water droplet however, generally this is more dangerous for SCC damage. Therefore, to improve reliability of turbine blade. various methods for SCC evaluation has been developed. In this study, the crack found in LSB during in-service inspection was evaluated using microstructure analysis and stress analysis. From the stress analysis, the optimum size of fillet to remove the crack was proposed. And also, the reliability was evaluated for modified LSB using GOODMAN diagram.

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초음속 충동형 터빈의 팁간극에 따른 성능변화 연구 (Effect of Tip-Clearance on the Performance of a Supersonic Impulse Turbine)

  • 정은환;이항기;박편구;김진한
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년도 제31회 추계학술대회논문집
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    • pp.117-121
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    • 2008
  • 슈라우드가 장착된 초음속 충동형 터빈의 팁간극에 따른 성능변화를 시험적으로 고찰하였다. 시험은 30톤급 터보펌프용 터빈을 이용하였으며 고압공기를 이용하여 다양한 압력비 및 회전수 범위에서 이루어졌다. 터빈의 효율민감도는 기준시험점에서 0.05의 매우 작은 값을 나타내었다. 터빈효율변화는 간극의 크기에 다라 비선형적으로 변화하였으며 고정된 압력비에서 효율민감도는 회전수의 세제곱에 비례하는 것으로 나타났다. 아울러 회전수에 무관하게 효율민감도는 기준시험 압력비에서 최소값을 보이는 것으로 나타났다.

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유동해석을 이용한 고압증기터빈 단효율 변화 예측 (Rediction of Stage Efficiency Variation of a USC High Pressure Steam Turbine by Computational Fluid Dynamics)

  • 강수영;장혁준;이정진;김동섭;박성진;홍기원
    • 한국유체기계학회 논문집
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    • 제20권2호
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    • pp.17-25
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    • 2017
  • Prediction of performance and operating characteristics of a state-of-the-art ultra-supercritical (USC) steam turbine is an important issue in many ways. Theoretical and empirical correlation equations, developed a few decades ago, have been widely used in commercial programs for a prediction of performance. To improve of these correlation equations and apply them to the high pressure turbine of a USC steam turbine, computational fluid dynamic analysis was carried out and correlation equations to calculate efficiency variation of each stage were made. Both fluid dynamic characteristic and thermodynamic performance was analyzed for the development of the correlation equations. In particular, the impact of flow addition through an overload valve (OLV) between stages was examined throughly. The trend of pressure drop due to the flow mixing by the OLV flow addition was analyzed and an efficiency correlation equation considering the OLV flow was also made.

APU용 구심터빈의 공력리그시험 (Aerodynamic Rig Test of Radial Turbine for APU)

  • 강정식;임병준;안이기
    • 대한기계학회논문집B
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    • 제37권1호
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    • pp.1-7
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    • 2013
  • 본 연구는 보조동력장치에 적용되는 구심터빈의 공력성능시험을 한국항공우주연구원의 고온 터빈 시험리그에서 수행한 결과이다. 리그시험을 위하여 터빈의 형상은 동일하되 팽창비, 마하수 및 유량계수는 실제 엔진과 동일한 값이 되도록 상사법칙을 적용하여 시험하였다. 설계 팽창비는 3.096이며, 상사된 설계회전수는 34909 rpm이고 상사된 터빈 입구온도는 $160^{\circ}C$이다. 터빈의 입구에는 익형 형상의 노즐이 설치되었으며 터빈 휠의 직경은 175.74mm이다. 시험을 통하여 터빈의 성능지도가 생성되었으며 터빈 입구에서의 상세 유동이 측정되었다. 노즐의 허브면에서 측정한 압력과 노즐의 쉬라우드 면과 터빈 휠 케이싱에서 측정한 압력 분포를 볼 때 터빈 내부에서의 팽창과정이 적절함을 확인할 수 있었다.

고압형 급수가열기 동체 감육 완화에 관한 연구 (A Study on the Relief of Shell Wall Thinning of High pressure Feedwater Heater)

  • 김형준;박상훈;서혁기;김경훈;황경모
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회B
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    • pp.2664-2669
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    • 2008
  • Feedwater heaters of many nuclear power plants have recently experienced severe wall thinning damange, which will increase as operating time progresses. Several nuclear power plants in Korea have experienced wall thinning damage in the area around the impingement baffle-installed downstream of the high pressure turbine extraction stream line- inside number 5A and 5B feedwater heaters. At that point, the extracted steam from the high pressure turbine is two phase fluid at high temperature, high pressure, and high speed. Since it flows in reverse direction after impinging the impingement baffle, the shell wall of the number 5 high pressure feedwater heater may be affected by flow-accelerated corrosion. This paper describes operation of experience and numerical analysis composed similar condition with real high pressure feedwater heater. This study applied squared, curved and new type impingement baffle plates to feedwater heater same as previous study. In addition, it shows difference of pressure distribution and value between single phase and two phase based on experience and numerical analysis.

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화력발전소의 축밀봉장치의 개선을 통한 터빈효율의 평가에 관한 연구 (A Study on the Turbine Efficiency through the shaft packing improvement of New Fossil Power Plant)

  • 권영수;서정세
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.715-720
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    • 2001
  • The main reason for applying positive pressure variable clearance packing in fossil power plant is high efficiency and energy saving movement in the government. This study intends to analyze the turbine efficiency through the shaft packing improvement in thermal power plant and makes its comparison to that of the used packing.

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고압터빈 노즐 압력면에서의 확장 형상 막냉각 홀 배열 최적설계 (Design Optimization of Fan-shaped Film Cooling Hole Array on Pressure Side Surface of High Pressure Turbine Nozzle)

  • 이상아;이동호;강영석;김진욱;서도영;이관중
    • 한국유체기계학회 논문집
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    • 제17권6호
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    • pp.52-58
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    • 2014
  • In the present work, design optimization of film-cooling hole array on the pressure side of high pressure turbine nozzle was conducted. There are four rows of fan-shaped film cooling holes on the nozzle pressure side surface and each row has a straight array of holes in the spanwise direction for baseline model. For design optimization, hole distributions in streamwise and spanwise directions for three rows of holes except first row are parameterized as a 2nd-order shape function. Three-dimensional compressible RANS equations are used for flow and thermal analysis around the nozzle surface and optimization technique using Design of Experiment, Kriging surrogate model and Genetic Algorithm is used. The results shows that averaged adiabatic wall temperature at the whole nozzle surface decreases about 2.7% and averaged film cooling effectiveness at the pressure side of nozzle increased about 8.2%.