• Title/Summary/Keyword: Cool-tip temperature

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Ablation Characteristics of Bovine Liver According to Cool-Tip Temperature of RFA Equipment (고주파 열치료 장비의 Cool-Tip 온도에 따른 소간의 소작 특성)

  • Choi, Young-Jae;Kim, Jeong-Koo
    • Journal of radiological science and technology
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    • v.38 no.2
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    • pp.155-161
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    • 2015
  • This study confirmed the correlation between the change of the cooling water in internal cooling system and the size of the ablation site of bovine liver in RF heat treatment equipment. The bovine liver was resection with $4{\times}4{\times}4cm^3$ in 2cm cool-tip and with $6{\times}6{\times}6cm^3$ in 3cm cool-tip for the experiments. Area and perimeter of the ablation site for bovine liver were measured by Freehand techniques of MRI. It showed area and perimeter decreased during cool-tip temperature rises 6 and 12 minutes ablation using a 2cm and 3cm cool-tip. The correlation of cool-tip temperature and area and perimeter was statistically significant the result are shown(p=.000). The measurements of area and perimeter were more accurate with MRI in actual measurements and MRI for ablation range. The statistical results using Paired sample T-test was also significant(p=.038). The ablation range of bovine liver decreased according as cooling water temperature increases in RF heat treatment equipment for reason of carbonization occurred due to does not accurately pass the RF energy. Therefore, it is considered the effect of RF heat treatment would be increased if the temperature of the cooling water consistently maintain the low temperature in order to reduce the generation of carbide at RF heat treatment and RF energy is delivered accurately.

A Study on Aircraft Structure and Jet Engine Part1 : Analysis of Heat Conduction on the Turbine Disk for Jet Engine (항공기 구조 및 제트 엔진에 관한 연구 제 1 절 : 제트엔진용 터어빈디스크의 열전도 해석)

  • Gil Moon Park;Hwan Kyu Park;Jong Il Kim;Jin Heung Kim;Moo Seok Lee;Nak Kyu Chung
    • Journal of Astronomy and Space Sciences
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    • v.2 no.2
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    • pp.153-174
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    • 1985
  • The one of critical factor in gas turbine engine performance is high turbine inlet gas temperature. Therefore, the turbine rotor has so many problems which must be considered such as the turbine blade cooling, thermal stress of turbine disk due to severe temperature gradient, turbine rotor tip clearance, under the high operating temperature. The purpose of this study is to provider the temperature distribution and heat flux in turbine disk which is required to considered premensioned problem by the Finite Difference Method and the Finite Element Methods on the steady state condition. In this study, the optimum aspect ratio of turbine disk was analysed for various heat conductivity of turbine disk material by Finite Difference Method, and the effect of laminating method with high conductivity materials to disk thickness direction by Finite Element Methods in order to cool the disk. The laminating method with high conductivity material on the side of the disk is effective.

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A Study on Thermal Environmental Performance Test of the Rotary Compressor Stirling Cryocooler (회전압축기형 스털링 냉동기의 열환경 성능시험에 관한 연구)

  • Park, Seong-Je;Hong, Yong-Ju;Kim, Hyo-Bong;Kimm, Dae-Woong
    • Proceedings of the KSME Conference
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    • 2007.05b
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    • pp.1953-1958
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    • 2007
  • This paper presents the results of a series of performance tests for the integral Stirling cryocooler. Infrared sensor systems incorporating cryocoolers are required to be qualified to the appropriate environmental specification. Integral Stirling cryocooler for thermal imaging system have matured to the stage of undergoing formal qualification test program. The thermal environmental test of the Stirling cryocooler is presented in this paper. We performed that low and high temperature keeping test from $-40^{\circ}C$ to $+71^{\circ}C$ and operating test at high and low temperature cyclic range with acceptance tests performed at scheduled intervals. Cooldown time to 80K and steady state input power at 80K were determined as a function of cooler components temperatures at the compressor, hot end and cold tip. Tests performed on this cooler have been successful with a measured cooldown time to 80K of less than 5 minutes 24seconds for $71^{\circ}C$ ambient temperature with input power of 11W

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Performance and Reliability Characteristics of the Free Piston Free Displacer Stirling Cryocooler

  • Park, Seong-Je;Hong, Yong-Ju;Kim, Hyo-Bong;Koh, Deuk-Yong;Kim, Yang-Hoon
    • Progress in Superconductivity and Cryogenics
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    • v.6 no.2
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    • pp.46-51
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    • 2004
  • This paper presents the results of a series of performance and reliability tests for the Stirling cryocooler. Infrared sensor systems incorporating cryocoolers are required to be qualified to the appropriate specification for the performance and reliability. FPFD Stirling cryocooler is currently under development for cooling infrared detector. Manufactured Stirling cryocooler delivers approximately 0.9W cooling at 80K for 30W∼40W of input power. It takes approximately 2 minutes to cool down to 80K at the ambient temperature of 23$^{\circ}C$. Performance characteristics for the vibration, acoustic noise, EMI and leak rate of the Stirling cryocooler are evaluated. We performed low and high temperature keeping test from -32$^{\circ}C$ to +52$^{\circ}C$ and operating test at high and low temperature cyclic range with acceptance tests performed at scheduled intervals. Cooling capacity is determined as a function of the temperatures at the compressor, hot end and cold tip at the expander. Finally, we describe the experimental facility for the MTTF evaluation and some typical results of the Stirling cryocooler.

A Study on the Characteristics of Delayed Hydride Cracking in Zr-2.5Nb Pressure Tube with the Heating-up and Heat-treatment (열처리 및 가열방식에 따른 Zr-2.5Nb 압력관의 수소지연균열 특성에 관한 연구)

  • Na, Eun-Young
    • Journal of Ocean Engineering and Technology
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    • v.23 no.2
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    • pp.69-73
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    • 2009
  • The objective of this study was to obtain a better understanding of the delayed hydride cracking (DHC) of Zr-2.5Nb alloy. The DHC model has some defects: first, it cannot explain why the DHC velocity (DHCV) becomes constant regardless of an applied stress intensity factor, even though the stress gradient is affected by the applied stress intensity factor at the notch tip. Second, it cannot explain why the DHCV has a strong dependence on the method of approaching the test temperature by a cool-down or a heating-up, even under the same stress gradient, and third, it cannot predict any hydride size effect on the DHC velocity. The DHC tests were conducted on Zr-2.5Nb compact tension specimens with the test temperatures reached by a heating-up method and a cool-down method. Crack velocities were measured in hydrided specimens, which were cooled from solution-treatment temperatures at different rates by being furnace-cooled, water-quenched, and liquid nitrogen-quenched. The resulting hydride size, morphology, and distributions were examined by optical metallography. It was found that fast cooling rates, which produce very finely dispersed hydrides, result in higher crack growth rates. This different DHC behavior of the Zr-2.5Nb tube with the cooling rate after a homogenization treatment is due to the precipitation of the $\gamma$-hydrides only in the water-quenched Zr-2.5Nb tube. This experiment will provide supporting evidence that the terminal solid solubility of a dissolution (TSSD) of $\gamma$-hydrides is higher than that of $\delta$-hydrides.