• Title/Summary/Keyword: pressure tube

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Experimental study on two-phase flow behavior inside a vertical tube evaporator under flashing phenomenon (후래시 현상을 수반하는 수직증발관내에서의 2상유동에 관한 실험적 연구)

  • 이상용;송시홍;이상호
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.12 no.4
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    • pp.833-846
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    • 1988
  • Two-phase flow heat transfer phenomena with flash evaporation inside a vertical tube were studied experimentally. Void fractions were measured using electrical probes, and the flow patterns were identified from the output voltage signal itself. The flow pattern as well as the beat transfer rates were changing along the axial distance from the tube inlet with the system pressure. As the pressure inside the tube decreases with fixed inlet temperature, the overall heat transfer coefficient through the tube wall and the boiling heat transfer coefficient inside the tube increase whereas the condensation heat transfer coefficient outside the tube decreases. The boiling heat transfer coefficient inside the tube measured by the experiments appeared to be somewhat larger than the value obtained from the Chen's correlation. Also, the flow patterns identified from present experiments are at the larger quality region of the low pattern map based on the transition criteria of Mishima and Ishii. This may be due to the non-equilibrium flashing phenomenon occurred at the nozzle exit and the tube inlet ; this also implies that the flow pattern of the two-phase flow depends strongly on the inlet conditions.

Pool boiling performance of an enhanced tube used in flooded refrigerant evaporator for turbo-refrigerator (터보냉동기용 만액식 증발기에 사용되는 성형가공관의 풀비등 성능)

  • 김태형;김내현
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.11 no.6
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    • pp.808-814
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    • 1999
  • Pool boiling performance of a metal-formed enhanced tube for a flooded refrigerant evaporator was experimentally investigated. Tests were performed for three different refrigerants(R-11, R-123, R-l34a), at two different saturation temperatures $4.4^{\circ}C \;and \;26.7^{\circ}C$ .Heat flux was varied from 10㎾/$m^2\;to\ 50㎾/$m^2$. Compared with the heat transfer coefficients of the smooth tube, the heat transfer coefficients of the enhanced tube were 6.6 times higher for R-11, 6.0 tines higher for R-123 and 3.5 times higher for R-l34a. The enhancements are comparable with those of foreign products. The heat transfer coefficients of R-l34a were higher than those of R-11 and R-123, either for the enhanced tube or for the smooth tube. At $4.4^{\circ}Csaturation temperature, however, the heat transfer coefficients of R-l34a were approximately the same as those of R-11, The effect of the saturation pressure on the boiling performance was similar to that of the smooth tube - the heat transfer coefficient increases as the saturation pressure increases.

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An Experimental Study on Performance of the Inertance Pulse Tube Refrigerator using a Small Compressor (소형 압축기를 이용한 관성관형 맥동관 냉동기의 성능 특성에 대한 실험적 연구)

  • Kim Hongseong;Jeong Sangkwon
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.17 no.6
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    • pp.552-559
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    • 2005
  • This paper describes an experimental study on the inertance pulse tube refrigerator using a small compressor. The purpose of this experimental study is to identify the performance of the inertance pulse tube refrigerator for various operating conditions and to obtain the optimum configuration. The dead volume effect is verified by two experimental apparatuses with different dead volumes between the compressor and the aftercooler. The refrigerator of the smaller dead volume shows better performance. The influence of operating frequency and charging pressure on the performance of the refrigerator is experimentally investigated. Reducing the regenerator mesh size improves the performance of the refrigerator. Finally, the inertance pulse tube refrigerator has maximum cooling capacity at the specific combination of the pulse tube length and the inertance tube length. The loss analysis is used to analyze and predict the optimum condition of the pulse tube refrigerator.

Design of Low Noise Axial-Tube Fan (저소음 축류형 소형홴의 개발)

  • Kim, K.-H.;Lee, S.;Kim, B.-H.
    • 유체기계공업학회:학술대회논문집
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    • 2001.11a
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    • pp.17-22
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    • 2001
  • Tube axial fans were designed to provide effective cooling for a personal computer by using $DasignFan^{TM}$ software. With basic input parameters of flow rate, pressure rise, rotating speed, and fan diameter, three dimensional geometry of blade is automatically generated and its performance and overall sound pressure level are predicted. In this steady, the newly developed fans of 60 mm and 80 mm diameters were proved to provide a very promising mode of low noise, compared with manufactured products.

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Performance Evaluation in Fin-Tube Heat Exchanger by Tow-In Winglet Pairs (Tow in 와류발생기에 의한 핀-관 열교환기의 성능실험)

  • ;Kahoru Torii
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.15 no.2
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    • pp.87-94
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    • 2003
  • To reduce the air side pressure drop in air-cooled heat exchanger, tow-in type winglet vortex generators are applied. A specially designed multiple-channel test core was used in the experiments for the various geometry of winglet vortex generators. The proposed tow-in type vortex generator gives significant separation delay, reduces form drag, and removes the zone of poor heat transfer from near-wake of the tubes. The results show the significant pressure drop reduction for the tow-in win91e1 vortex generators with the similar enhancement of the heat transfer as other vortex generator applications in heat exchanger. In the range of Reynolds number of 350 to 2100 the pressure drop decrease 8∼15% and 34∼55% for the in-line and staggered tube banks, respectively, compared to those without vortex generators.

Spray Angle and Break-up Characteristics of Supersonic Liquid Jets by an Impinging Methods with High Speed Projectile (초고속 발사체의 액체 저장부 충돌에 의한 초음속 액체 제트의 분무 속도 및 분열 특성)

  • Lee, In-Chul;Shin, Jeung-Hwan;Kim, Heuy-Dong;Koo, Ja-Ye
    • Journal of the Korean Society of Visualization
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    • v.9 no.1
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    • pp.55-60
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    • 2011
  • Pulsed supersonic liquid jets injected into an ambient air are empirically studied by using a high pressure ballistic range system. Ballistic range systems which are configured with high-pressure tube, pump tube, launch tube and liquid storage nozzle. Experimental studies are conducted to use with various impact nozzle geometry. Supersonic liquid jets are generated by an impact of high speed of the projectile. High speed liquid jets are injected with M = 3.2 which pressure is 1.19 GPa. Multiple jets which accompany with shock wave and pressure wave in front of the jet were observed. The shock-wave affects significantly atomization process for each spray droplets. As decreasing orifice diameter, the averaged SMD of spray jets had the decreasing tendency.

Application of FAD on Pressure Tube for the Probabilitic Integrity Assessment (파손평가선도를 이용한 압력관 결함의 확률론적 건전성 평가)

  • Kwak, Sang-Log;Wang, Jong-Bae;Park, Youn-Won;Lee, Joon-Seong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.28 no.3
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    • pp.289-295
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    • 2004
  • Pressure tubes are major component of nuclear reactor, but only selected samples are periodically examined due to numerous numbers of tubes. Current in-service inspection result show there is high probability of flaw existence at uninspected pressure tube. Probabilistic analysis is applied in this study for the integrity assessment of uninspected pressure tube. All the current integrity evaluations procedures are based on conventional deterministic approaches. So it is expected that the results obtained are too conservative to perform a rational evaluation of lifetime. More realistic failure criteria, based on FAD are also proposed for the probabilistic analysis. As a result of this study failure probabilities for various conditions are calculated, and examined application of FAD and LBB concept.

Hydride Embrittlement Behavior at the LBB Evaluation of PHWR Pressure Tube (중수로 압력관 LBB 평가에서의 수소화물에 의한 취화거동)

  • Oh, Dong-Joon;Kim, Young-Suk
    • Proceedings of the KSME Conference
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    • 2003.11a
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    • pp.1192-1197
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    • 2003
  • The aim of this study is to investigate the hydride embrittlement when the LBB evaluation is carried out for the integrity of PHWR Pressure Tubes. The transverse tensile and CCT tests were performed at three hydrogen concentrations while the test temperatures were changed (RT to $300^{\circ}C$). The specimens were directly machined from the pressure tube retaining original curvature. Both the transverse tensile and the fracture toughness tests showed the hydrogen embrittlement clearly at RT but this phenomenon was disappeared while the test temperature arrived over $250^{\circ}C$. Using the DHC test results, the CCL and LBB time were calculated and compared. The hydride embrittlement behavior at the LBB evaluation was definitely showed.

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A Study on FAD Development for Probabilistic Pressure Tube Integrity Assessment (압력관의 확률론적평가에 타당한 파손평가선도 작성에 관한 연구)

  • Kwak, Sang-Log;Wang, Jong-Bae;Choi, Young-Hwan;Park, Youn-Won
    • Proceedings of the KSME Conference
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    • 2003.11a
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    • pp.1211-1215
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    • 2003
  • Pressure tubes are major component of nuclear reactor, but only selected samples are periodically examined due to numerous numbers of tubes. Current in-service inspection result show there is high probability of flaw existence at un-inspected pressure tube. Probabilistic analysis is applied in this study for the integrity assessment of un-inspected pressure tube. But all the current integrity evaluations procedures are based on conventional deterministic approaches. So many integrity evaluation parameters are not directly apply to probabilistic analysis. As a result of this study failure assessment diagram are proposed based on test data.

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Self-ignition of high-pressure hydrogen gas released into tube (튜브내 고압수소가스 누출에 따른 자발점화 현상 유동가시화 연구)

  • Kim, Yeong Ryeon;Lee, Hyoung Jin;Kim, Sei Hwan;Jeung, In Seuck
    • 한국연소학회:학술대회논문집
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    • 2012.04a
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    • pp.247-248
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    • 2012
  • Unidentified self-ignitions were reported when the high-pressure hydrogen gas suddenly leaked out. This paper presents a flow visualization study to investigate the self-ignition mechanism in a test tube how the ignition process is initiated and the flame propagates with measurement of a number of pressure and light sensors installed in the tube supported the analysis of the self-ignition. The test result showed the location of the self-ignition taken place and critical static pressure at the boundary layer for self-ignition.

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