• 제목/요약/키워드: High-pressure turbine

검색결과 457건 처리시간 0.031초

증기터빈 1단 Shell 압력측정에 의한 교축유동 고찰 (A Study of Steam Turbine Throttle Flow from Measured First Stage Shell Pressure)

  • 윤인수;이재헌;유호선;문승재;이태구;허진혁
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.373-376
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    • 2008
  • Industrial Steam Turbine first stage shell pressure is related to throttle flow. Theoretically, first stage shell pressure could, therefore, be measured and used as an index of turbine throttle flow. However, accurate flow measurements show that this pressure is not a reliable index of the actual flow. Data analysis of steam turbinessubjected to ASME acceptance tests shows that the use of first stage shell pressure as an index of throttle flow produced errors as large as 9.6 %. The mean of the errors was +2.2% with a standard deviation of ${\pm}$2.8 %. Applications that require an accuratedetermination of turbine steam flow, such as turbine acceptance testing, should, therefore, not rely on this method. Therefore, First stage shell pressure measurement serves as a valid and economical indicator of turbine throttle flow in cases where a high degree of accuracy in throttle flow measurement is not required but repeatability is desired, such as for boiler control. Generally speaking, Steam turbine first stage shell pressure may also be a very useful monitor of turbine performance when used with certain other turbine measurements.

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증기터빈의 기동조건과 성능개선이 터빈의 진동에 미치는 영향 (Effect on Vibration of Start-up Condition and Retrofit of Steam Turbines)

  • 이혁순;정혁진;송우석
    • 한국압력기기공학회 논문집
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    • 제7권3호
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    • pp.1-7
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    • 2011
  • The analysis shows that the vibration is one of the main reasons of turbine failure. Especially, the problems caused by vibration occur right after retrofit of the turbine-generator and restarting the turbine. Through the case study of high vibration caused by after the turbine trip and restart, turbine vibration was identified to be influenced by startup condition. Turbine startup at high casing temperature right after unscheduled turbine trip cause radial expansion in rotor by contraction in axial direction, while casing continues to contract by steam flowing into casing. Consequently, gap between rotor and casing decrease until to metal contact to cause high vibration. Through the case study of high vibration of turbine-generator system after generator retrofit, it was identified that generator replacement could cause high vibration in turbine-generator system if the influence of generator replacement on entire system was not considered properly. To prevent startup delay caused by high vibration, it is important to keep the gaps at the design standard and start the turbine after thermal equilibrium.

3차원 가스터빈 블레이드의 연성 해석에 관한 연구 (A Study on Coupled Field Analysis of 3-D Gas Turbine Blade)

  • 박근형;민택기;박창수
    • 한국공작기계학회논문집
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    • 제15권2호
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    • pp.38-43
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    • 2006
  • A turbine blade operates under high temperature, high pressure, and the loads have the characteristics that the amplitudes change. Therefore, it is important to perform a stress analysis considering thermal and pressure loads. The purpose of this study is to investigate the effects of these loads on gas turbine blade through thermal stress analysis. The analysis results shows that pressure in gas fluid flow around blade is high in leading edge part, Gas temperature is connections with pressure of flow around blade. The distribution of stress from blade is appearing as is different at suction side and pressure side.

CFD에 의한 용적형수차의 압력맥동 및 내부유동 해석 (CFD Analysis of Pressure Pulsation and Internal Flow for a Positive Displacement Hydraulic Turbine)

  • 최영도;김유택;이영호
    • Journal of Advanced Marine Engineering and Technology
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    • 제31권6호
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    • pp.687-693
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    • 2007
  • It has been known that one of the main obstacles of improving the performance of positive displacement hydraulic turbine is pressure pulsation which occurs at the regions upstream and downstream of the turbine. In order to suppress the pressure pulsation. occurrence reason of the pressure pulsation should be understood in detail Therefore. this study aims to establish a CFD analysis method by which the phenomena of unsteady pressure pulsation can be examined with high accuracy. Internal flow field of the turbine is modeled simply to generalize the relation between the pressure pulsation and internal flow. The results show that the Present CFD method adopting unsteady calculation can be applied successfully to the analysis of the Phenomena of Pressure Pulsation. Occurrence of the Pressure pulsation is due to the difference of the rotational speed of turbine rotors When driving rotor rotates by uniform speed and fellowing rotor rotates by variable speed, very large Pressure pulsation occurs within the turbine periodically.

터빈 로터 반사각에 따른 의료용 에어터빈 핸드피스의 성능에 관한 수치 해석 (Numerical Analysis on Performance of Dental Air Turbine Handpiece for Various Reflection Angles of Turbine Rotor)

  • 이정호;이상도;김귀순
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.29-32
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    • 2008
  • Dental high-speed air turbine handpieces have been used as a dental cutting tool in clinical dentistry for over 50 years, yet little study has been reported on their flow and performance analysis. Therefore it is necessary to investigate turbine for the performance improvements of an air turbine handpiece. This paper presents pressure on turbine rotor and flow analysis in air turbine handpiece using CFD (computational fluid dynamics). Characteristics on each flow and pressure for four various reflection angles of turbine rotor are presented, and then performance change is analyzed about air turbine handpieces by CFD results.

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터보팬 엔진에서 터빈 냉각이 성능에 미치는 영향에 대한 수치적 해석 (Parametric Cycle Analysis of a Turbofan Engine with Turbine Cooling)

  • 황진석;문희장;구자예
    • 한국항공운항학회지
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    • 제14권1호
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    • pp.15-21
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    • 2006
  • Parametric cycle analysis of a dual-spool, mixed exhaust turbofan engine with turbine blade cooling were described to investigate the effect of turbine blade cooling on the engine performance such as specific thrust and thrust specific fuel consumption. Coolant of low pressure turbine triggers high engine performance loss and cooling effect loss in high pressure turbine. Therefore low pressure turbine coolant should be much more considered for effective design.

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가스 터빈 블레이드의 유동 및 응력 해석에 관한 연구 (Study on Flow and Stress Analysis of Gas Turbine Blade)

  • 조재웅;한문식
    • 한국기계가공학회지
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    • 제10권3호
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    • pp.67-72
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    • 2011
  • Turbine blades operate under high temperature and pressure. The influence changes according to its width and angle. Thermal stress and pressure are important factors to analyze the stress distribution. The purpose of this study is to investigate the effects of loads on the gas turbine blade using thermal stress analysis. These analysis results show the gas fluid flow with a high pressure around the surface of blade. Gas temperature is related to the pressure of flow around the blade. The stress concentration around blade is shown and the concentration is due to the difference between suction side and pressure side of combustion gas.

주파수 응답해석을 통한 제작공차를 가지는 저압터빈 케이싱의 고진동 원인 규명 (Investigation of the Cause of High Vibration in a Low Pressure Turbine Casing with Manufacturing Defects by Frequency Response Analysis)

  • 윤희철;우창기;황재곤
    • 한국생산제조학회지
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    • 제24권4호
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    • pp.463-468
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    • 2015
  • High vibration of a low pressure (LP) turbine casing caused safety problems and life at the facility it was housed in. The main focus of this study was the cause of the high vibration in a low pressure turbine casing with manufacturing defects by frequency response analysis, compared with the results of experiments. Therefore, excited accelerations were obtained from the LP casing fundamental, and frequency responses were analyzed. The measurement and the modal analysis showed that the natural frequency of the LP turbine casing was 61.26 Hz and the excited frequency of the turbine rotor was 60.25 Hz. The manufacturing defect caused a decrease in the casing natural frequency and resulted in the high vibration of the casing because it moved close to the resonant frequency.

노즐형상변화에 따른 횡류수차의 압력과 속도 분포 (Pressure and Velocity Distributions of Cross-flow Hydroturbine by Nozzle Shape)

  • 임재익;최영도;임우섭;김유택;이영호
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2833-2838
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    • 2007
  • Recently, small hydropower attracts attention because of its clean, renewable and abundant energy resources to develop. However, suitable turbine type is not determined yet in the range of small hydropower and it is necessary to study for the effective turbine type. Moreover, relatively high manufacturing cost by the complex structure of the turbine is the highest barrier for developing the small hydropower turbine. Therefore, a cross-flow turbine is adopted because of its simple structure and high possibility of applying to small hydropower. The purpose of this study is to examine the optimum configuration of nozzle shape to further optimize the cross-flow hydraulic turbine structure and to improve the performance. The results show that pressure on the runner blade in Stage 1 and velocity at nozzle outlet have close relation to the turbine performance.

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30톤급 액체로켓 엔진용 터보펌프 터빈 성능시험 (Performance Test of the 30-ton Class Liquid Rocket Engine Turbopump Turbine)

  • 정은환;박편구;김진한
    • 한국추진공학회지
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    • 제12권1호
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    • pp.1-6
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    • 2008
  • 실매질 시험용 30톤급 터보펌프 터빈의 성능시험을 수행하였다. 날카로운 익단의 동익과 원호 익단의 동익을 가진 두 종류의 터빈로터에 대한 성능시험을 수행하였으며 아울러 다양한 압력비와 회전수에 따른 터빈 축추력의 변화를 동시에 측정하였다. 시험결과, 날카로운 익단의 터빈로터가 원호익단을 가진 터빈로터에 비해 설계 상사점에서 약 1% 높은 효율을 나타내는 것으로 측정되었다. 터빈 축추력은 회전수에 따라 선형적으로 변화하며 터빈 압력비에 큰 영향을 받는 것으로 나타났다.