• 제목/요약/키워드: 터빈 유량계

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터빈유량계를 이용한 유량 측정 시스템의 최적 설계 (Optimal Design of Flow Measurement System Using Turbine Flowmeter)

  • 김홍탁;김부일
    • 한국전자통신학회논문지
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    • 제13권1호
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    • pp.77-84
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    • 2018
  • 터빈유량계(Turbine flowmeter)는 유량 측정시 높은 정확도와 반복성을 위해 선택되지만 교정시의 표준 환경 조건과 현장에서의 환경 조건 차이로 다양한 측정 불확도 요인을 발생시킨다. 또한 교정된 측정값 외의 구간에서의 사용을 위해 신뢰성 높은 보간 기법(Interpolation method)이 필요하다. 따라서 본 논문에서는 유량 측정(Flow measurement) 신뢰성 향상을 위해 터빈유량계의 출력 신호의 정확한 측정과 교정된 결과값의 보간, 온도변화를 실시간 보정(correction)하는 장비를 설계 및 제작하고 성능 검증을 수행함으로 현장에서의 측정 신뢰도를 확보하였다.

현장여건에 따른 터빈 유량계와 오리피스 유량계의 정확도 비교 (A Comparison of Accuracy Between a Turbine and an Orifice Meter in the Field)

  • 안승희;허재영
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 1999년도 유체기계 연구개발 발표회 논문집
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    • pp.97-105
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    • 1999
  • Orifice flow meters are frequently used for measuring gas flow in gas industry. However, to insure the accuracy of the measurement, a certain length of the meter run at the upstream of the flow meter is required. The objective of this study is to analyze flow measurement errors of the orifice flow meter quantitatively for shorter lengths of the meter runs than those suggested in the standard manuals with variation of diameter ratio( $\beta$ ratio) and flow rate. The test results showed that the flow measurement errors of the orifice meter were inversely proportional to the diameter ratio. In other words, when the diameter ratio is 0.3 and 0.7, the measurement error is $-7.3\%$ and $-3.5\%$, respectively. the main reason of the measurement error is due to the swirl effect from the configuration of the meter run at the upstream of the flow meter. In case the length of the meter run is shorter than that suggested in the standard manuals, the swirl effect is not removed completely and it affects the flow meter's performance. As mentioned above, the less the pipe diameter ratio, the more the flow measurement error. It means that the swirl effect on the orifice meter increases as the $\beta$ ratio decreases.

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동기화 터보 챠저계를 이용한 터빈 반동도 예측에 관한 연구 (A Study on the Estimating the Degree of Reaction for a Turbine Using a Synchronizable Turbocharging System)

  • 김창훈
    • 수산해양기술연구
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    • 제33권3호
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    • pp.234-240
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    • 1997
  • 터보 챠저의 반동도와 터빈 노즐유량의 변화를 행하여 엔진의 성능을 향상시킬 수 있었다. 터빈의 에너지 손실과 그 영향을 미치는 반동도 및 터빈 입구의 유로의 변화, 그리고 블레이드에서 역 유동에 대한 개선 조건도 제시하였다.

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터빈 유량계를 사용한 이상유동의 측정

  • 심재우
    • 한국해양공학회지
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    • 제12권2호통권28호
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    • pp.147-152
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    • 1998
  • In this study turbine flowmeters were used to predict volumetric flow rate of each phase in two-phase, gas-liquid, flowing in a vertical tube. To determine volumetric flow rates of two-phase, air-water, flowing vertically upward through the polycarbonate tube(57mm ID-inside diameter), two turbine flow meters were used. For void fraction measurements, two gamma densitometers were used at each location of the turbine flow meter, one at the upstream and the other at the downstream. It was determined that the turbine flowmeter's outputs were a function of actual volumetric flow rate of each of the two phases. A two-phase flow model was developed.

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엔진 고공 시험에서 연료 유량 측정용 터빈 유량계의 측정 불확도 분석 (Measurement Uncertainty Analysis of a Turbine Flowmeter for Fuel Flow Measurement in Altitude Engine Test)

  • 양인영
    • 한국유체기계학회 논문집
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    • 제14권1호
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    • pp.42-47
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    • 2011
  • Measurement uncertainty analysis of fuel flow using turbine flowmeter was performed for the case of altitude engine test. SAE ARP4990 was used as the fuel flow calculation procedure, as well as the mathematical model for the measurement uncertainty assessment. The assessment was performed using Sensitivity Coefficient Method. 11 parameters involved in the calculation of the flow rate were considered. For the given equipment setup, the measurement uncertainty of fuel flow was assessed in the range of 1.19~1.86 % for high flow rate case, and 1.47~3.31 % for low flow rate case. Fluctuation in frequency signal from the flowmeter had the largest influence on the fuel flow measurement uncertainty for most cases. Fuel temperature measurement had the largest for the case of low temperature and low flow rate. Calibration of K-factor and the interpolation of the calibration data also had large influence, especially for the case of very low temperature. Reference temperature, at which the reference viscosity of the sample fuel was measured, had relatively small contribution, but it became larger when the operating fuel temperature was far from reference temperature. Measurement of reference density had small contribution on the flow rate uncertainty. Fuel pressure and atmospheric pressure measurement had virtually no contribution on the flow rate uncertainty.

소형 푸루버의 유량계 검증 오차 연구 (Study on Flowmeter Proving Errors of a Small Volume Prover)

  • 백종승;임기원;최용문
    • 대한기계학회논문집
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    • 제14권1호
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    • pp.259-266
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    • 1990
  • 본 연구에서는 지금까지 개발된 각종 소형 푸루버의 작동원리 및 장단점을 분 석 비교한 결과에 따라 이중 실린더형의 소형 푸루버를 직접 설계 제작하고, 개발된 소형 푸루버를 사용하여 펄스 주기 변동특성이 각각 다른 유량계를 대상으로 펄스보간 오차 시험을 실시하였다. 실험결과는 통계적 방법을 도입하여 분석함으로써 유량계 각각에 대하여 기대 검증 정확도 수준을 선정하였다. 또 기대검증 정확도가 좋지 않 게 예상되는 유량계에 대해서는 검증 정확도 향상 방안을 제시하였다.

터빈유량계의 3차원 유동에 관한 수치적 연구 (Numerical Study of Three-dimensional Flow Through a Turbine Flow Meter)

  • 김진범;고성호
    • 한국유체기계학회 논문집
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    • 제6권1호
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    • pp.44-50
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    • 2003
  • Flow through a turbine flow meter is simulated by solving the incompressible Navier-Stokes equations. The solution method is based on the pseudo-compressibility approach and uses an implicit-upwind differencing scheme together with the Gauss-Seidel line relaxation method. The equations are solved steadily in rotating reference frames, and the centrifugal force and the Coriolis force are added to the equation of motion. The standard $k-{\epsilon}$model is employed to evaluate turbulent viscosity. Computational results yield quantitative as well as qualitative information on the design of turbine flow meters by showing the distributions of pressure and velocity around the turbine blades.