• Title/Summary/Keyword: 입출구 배관

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A Study on the Temperature Characteristics at the Inlet and the Outlet Pipes of a Refrigerator Drain Condenser (냉장고 배출수 응축기 입출구 배관에서의 온도 특성에 관한 연구)

  • Ha, Ji Soo;Kim, Tae Kwon
    • Journal of Energy Engineering
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    • v.23 no.4
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    • pp.247-255
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    • 2014
  • The present study was conducted to elucidate the characteristics of temperature at the inlet and outlet pipes of a refrigerator drain condenser and suggest the method to predict the temperature of the refrigerant at the inlet and outlet pipes of the drain condenser. For this purpose, a built in style refrigerator was installed in a constant temperature chamber to measure temperatures at the inlet and outlet pipes of the drain condenser. From the results of the present analysis, it could be seen that the measured temperatures changed from $37^{\circ}C$ to $46^{\circ}C$ and the actual refrigerant temperatures were higher than the measured temperatures with the difference magnitude of $8^{\circ}C$ to $22^{\circ}C$. The present study suggested that the temperatures of the refrigerator could be calculated with the measured temperatures by introducing curve fitting of the measured temperature. The predicted refrigerant temperatures by the present study had the accuracy within 6% error of the actual refrigerant temperatures.

High Frequency Signal Analysis of LOx Pump for Liquid Rocket Engine under Cavitating Condition (캐비테이션 환경에서의 액체로켓엔진용 산화제펌프의 고주파 신호 분석)

  • Kim, Dae-Jin;Kang, Byung Yun;Choi, Chang-Ho;Bae, Joon-Hwan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.4
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    • pp.61-67
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    • 2018
  • High-frequency signals are analyzed at the inlet/outlet pipeline and pump casing during cavitation tests of the LOx pump for liquid rocket engines. Root-mean square values of all data are investigated with respect to cavitation number. The values of synchronous, harmonic, and cavitation instability frequencies are also calculated. Pressure pulsations of the inlet and outlet pipelines are affected by cavitation instabilities. The 3x component (i.e., the blade-passing frequency of the inducer) is predominant in the outlet pulsation sensor. This seems to be related to the fact that the number of impeller blades is a multiple of the number of the inducer blades. The cavitation instability is also measured at the accelerometer of the pump casing.

Effect of Reynolds Number on the Flow Characteristics of a Control Valve (제어밸브 유량특성에 레이놀즈 수가 미치는 영향)

  • Jung, Taekyu
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.995-999
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    • 2017
  • The factors affecting the flow coefficient of a control valve were identified and analyzed. The flow coefficient of a control valve are affected by not only Reynolds Number but also the figure and the roughness of the inlet/outlet pipes. Therefore, the flow coefficient is not a constant value. For the purpose of use in the system such as LRE, requiring the exact flow-coefficient of a control valve, the flow-coefficient should be measured under similar Reynolds Number using the inlet and outlet pipes which have the same figure and roughness with a real system.

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High Frequency Signal Analysis of LOx Pump for Liquid Rocket Engine under Cavitating Condition (캐비테이션 환경에서의 액체로켓엔진용 산화제펌프의 고주파 신호 분석)

  • Kim, Dae-Jin;Kang, Byung Yun;Choi, Chang-Ho
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.1093-1098
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    • 2017
  • High frequency signals are analyzed which are measured at the inlet / outlet pipeline and pump casing during cavitation tests of the LOx pump for the liquid rocket engine. RMS values of data are shown according to the cavitation number. RMS values of the synchronous frequency, its harmonic frequencies and frequencies of cavitation instabilities are also calculated. The pressure pulsations of the inlet and outlet pipeline are affected by cavitation instabilities. 3x component is predominant in the outlet pulsation sensor since 3x component generated at the inducer is amplified at the impeller. The cavitation instability is also found at the accelerometer signal of the casing.

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Numerical Study for The Critical-Flow-Characteristics of The Pressure Regulator and Considerations as a Pipe Network Element (I);Influence of the Inlet-Outlet Pressure Ratio (정압기 임계유동특성 및 배관망해석 요소로서의 고려에 관한 수치해석적 연구 (I);입출구 압력비 변화 영향)

  • Shin, C.H.;Ha, J.M.;Lee, C.G.;Her, J.Y.;Im, J.H.;Joo, W.G.
    • Proceedings of the KSME Conference
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    • 2004.11a
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    • pp.1448-1453
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    • 2004
  • The major parameters governing the fluid dynamical and thermo-dynamical behavior in the large pipeline network system are friction loss and the pipeline length. But in local pipeline networks and relatively short distance pipeline system, secondary loss and the considerations of the moving states of the fluid machine are also important. One of the major element in local pressure control system is pressure regulator. It causes the variations of the physical properties in that pipeline system. Especially, as there is not enough information to obtain reliable physical property values such as density, temperature etc. at the downstream of the pressure regulator, It is hard to calculate accurate solution in the pipeline network analysis. In this study, some numerical approaches to investigate the critical-flow-characteristics of the pressure regulator have been done and the detail examinations and considerations of the pressure regulator as a pipeline network elements according to the variations of the inlet-outlet pressure ratio have been carried. Finally the flow-flied distributions, relations and critical-flow-characteristics have been studied. in detail and the 1D analytic method to analyze critical pipe flow have been investigated

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High Frequency Signal Analysis of Fuel Pump for Liquid Rocket Engine under Cavitating Condition (캐비테이션 환경에서의 액체로켓엔진용 연료펌프의 고주파 신호 분석)

  • Kim, Dae-Jin;Kang, Byung Yun;Choi, Chang-Ho
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.1099-1102
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    • 2017
  • High frequency signals are analyzed which are measured at the inlet / outlet pipeline and pump casing during cavitation tests of the fuel pump for the liquid rocket engine. RMS values of each data are shown according to the cavitation number and compared with those of the LOx pump tests and the impact of the cavitation instability is also explored. Analogies about the cavitation number are confirmed between high frequency data of both pumps. In addition, the cavitation instability is found in all the signals and has an affect on the outlet pressure pulsation of the fuel pump.

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