• 제목/요약/키워드: Cryogenic liquid

검색결과 413건 처리시간 0.034초

Performance evaluation of 80 GHz FMCW Radar for level measurement of cryogenic fluid

  • Mun, J.M.;Lee, J.H.;Lee, S.C.;Sim, K.D.;Kim, S.H.
    • 한국초전도ㆍ저온공학회논문지
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    • 제23권4호
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    • pp.56-60
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    • 2021
  • The microwave Radar used for special purposes in the past is being applied in various areas due to the technological advancement and cost reduction, and is particularly applied to autonomous driving in the automobile field. The FMCW (Frequency Modulated Continuous Wave) Radar can acquire level information of liquid in vessel based on the beat frequency obtained by continuously transmitting and receiving signals by modulating the frequency over time. However, for cryogenic fluids with small impedance differences between liquid medium and gas medium, such as liquid nitrogen and liquid hydrogen, it is difficult to apply a typical Radar-based level meter. In this study, we develop an 80 GHz FMCW Radar for level measurement of cryogenic fluids with small impedance differences between media and analyze its characteristics. Here, because of the low intrinsic impedance difference, most of the transmitted signal passes through the liquid nitrogen interface and is reflected at the bottom of the vessel. To solve this problem, a radar measurement algorithm was designed to detect multiple targets and separate the distance signal to the bottom of the vessel in order to estimate the precise position on the liquid nitrogen interface. Thereafter, performance verification experiments were performed according to the liquid nitrogen level using the developed radar level meter.

밀폐된 공간에서 초저온 액화가스의 거동 (Behavior of cryogenic gases in a closed space)

  • 이현철;강형석;박두선;손무룡
    • 한국초전도저온공학회:학술대회논문집
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    • 한국초전도저온공학회 2000년도 KIASC Conference 2000 / 2000년도 학술대회 논문집
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    • pp.48-51
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    • 2000
  • The behavior of cryogenic liquid stored in a closed cryogenic tank has been studied at various liquid levels, as a function of pressure and temperature on time, assuming heat leak(NER) is 0.7%/day. The pressure depends, as expected, on the liquid-vapor ratio in a tank. The calculation shows that if liquid level is as high as 90%,much higher than the critical volume ration, in a closed tank of designed pressure 11 bar, it takes 5.4 to 15days for the entire volume of the tank to be filled with liquid and 11 to 22 days for the tank to be exploded. If a closed tank is full of liquid, it is extremely dangerous because of abrupt pressure increase so that the safety devices are necessary to vent out pressurized gas. These phenomena can be explained with the liquid heat capacity, latent heat and compressibility.

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대용량 액체수소 인수기지 쿨다운 해석 기술 연구 (Study on Cool-down Analysis Technology for Large Scale Liquid Hydrogen Receiving Terminal)

  • 박창원;김동혁;이영범;서흥석;권용수
    • 한국수소및신에너지학회논문집
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    • 제35권1호
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    • pp.34-39
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    • 2024
  • Korea government is trying to supply liquid hydrogen from another country to domestic The research for liquid hydrogen transportation and liquefaction plant of hydrogen underway for several years, and empirical research is also planned in the future. Along with the development of liquid hydrogen transport ship/liquefaction plant technology, the development of liquid hydrogen reception base technology must be carried out. In this study, a concept level liquid hydrogen receiving terminal is constructed based on the process of the LNG receiving terminal. Based on this, a study is conducted on the development of analysis technology for the amount of BOG (pipe, tank) generated during cooldown and unloading in the liquid hydrogen unloading line (loading arm to storage tank). The research results are intended to be used as basic data for the design and liquid hydrogen receiving terminal in the future.

극저온 환경용 볼베어링 시험장치 개발 및 터보펌프용 볼베어링 시제품의 성능평가 (Development of Cryogenic Test Rig for Ball-Bearing and Evaluation of the Performance of the Prototype Ball-Bearing of Turbo pump)

  • 조준현;임윤철;이성철;김충현
    • Tribology and Lubricants
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    • 제28권4호
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    • pp.167-172
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    • 2012
  • The turbo pump of a liquid rocket engine is composed of three main parts: the oxidizer pump, fuel pump, and turbine. Liquid oxygen ($LO_X$) is the working fluid in the cryogenic environment in the oxidizer pump, but tests are usually performed using liquid nitrogen ($LN_2$), which has a boiling point similar to that of $LO_X$ but is comparatively safer and easier to use for the test. In this study, a bearing test rig is developed and its performance is evaluated using a cryogenic ball bearing with $LN_2$ as the working fluid. Verifying the performance of the bearing test rig is crucial for ensuring correct working of the turbo pump unit in the liquid rocket engine. A stable test rig for the bearing in a cryogenic environment makes the bearing technology enhance its reliability. The test results show that the system operates stably and the requirement of performance time of 500 s is met. The test results of temperature, motor speed, and torque are discussed. The developed cryogenic bearing test rig is expected to help in widening knowledge and expanding research on ball bearings in the future.

액체질소 냉각용 극저온 열교환기의 최적설계를 위한 열전달 및 압력강하 특성 분석 (An Analysis of Heat Transfer and Pressure Drop Characteristics for Optimum Design of Cryogenic Heat Exchanger used for Liquid Nitrogen Cooling)

  • 고지운;전동순
    • 설비공학논문집
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    • 제30권1호
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    • pp.24-32
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    • 2018
  • In this paper, analytical studies were conducted to obtain optimal design factors and analysis parameters of liquid nitrogen cooling exchanger applied in cryogenic refrigerator. The target value of heat transfer rate was more than 1 kW and pressure drop was less than 40 kPa. Design factors of cryogenic heat exchanger included width of channel and configuration of paths. Analytical factors of liquid nitrogen cooling exchanger included temperatures of coolant header surface and inlet liquid nitrogen. The width and number of channels in the design parameters were 0.0050~0.0150 m and 4~8, respectively. The configuration of channel path was 4 ways. Temperatures of coolant header surface and inlet liquid nitrogen in analytical parameters were 74 to 78K and 82 to 86K, respectively. As result, the design factor and analysis parameter satisfying the target values were obtained. The biggest heat transfer rate was 1.36 kW with pressure drop of 32.26 kPa.

Development and performance test of a liquid nitrogen circulation pump for HTS power cable

  • Seok, Jihoon;Kim, Dongmin;Lee, Changhyeong;Kim, Manryeol;Choi, Jeongdong;Kim, Seokho
    • 한국초전도ㆍ저온공학회논문지
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    • 제20권3호
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    • pp.28-33
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    • 2018
  • With the continuous performance improvement and commercialization of HTS wires, there have been many efforts to commercialize HTS power cables recently. Unlike conventional power cables, a cryogenic cooling system is required for a HTS power cable and a cryogenic pump is one of the essential components to circulate subcooled liquid nitrogen and cool the HTS power cable. Especially, the development of a reliable and high-efficiency cryogenic pump is an important issue for the commercialization of HTS power cables of several kilometers or more. In this study, we designed and fabricated a cryogenic pump for subcooled liquid nitrogen with a mass flow rate of 1.2 kg/s, a differential pressure of 5 bar, and evaluated the hydraulic performance of the pump. Impeller design was conducted to meet the target design performance with 1 D analysis model and CFD analysis. The pump performance parameters such as pressure heads, mass flow rates, and efficiencies in accordance with rotating speeds were assessed using a laboratory's performance evaluation system.

확산동기 증발에 의한 극저온 액체 과냉각 (Subcooling of cryogenic liquid by diffusion-driven evaporation)

  • 조남경;정상권
    • 한국초전도ㆍ저온공학회논문지
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    • 제9권3호
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    • pp.72-82
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    • 2007
  • This paper relates to reducing the temperature of a cryogenic liquid by contacting it with gas bubbles, which can be characterized by diffusion-driven evaporative cooling, The characteristic of diffusion-driven evaporative cooling is thoroughly examined by theoretical. analytical and experimental methods specifically for the case of helium injection into liquid oxygen. The results reveal that if the gaseous oxygen partial pressure in helium bubbles is lower than the liquid oxygen vapor pressure, cooling occurs autonomously due to diffusion mass transfer. The method of lowering the injected helium temperature turns out to be very effective for cooling purpose.

액체 수소를 활용한 극저온 부품의 냉각 과정에서 발생하는 BOG에 관한 이론적 연구 (A Theoretical Study on Boil-off Gas Generated from Cooling Process for Cryogenic Components Using Liquid Hydrogen)

  • 하동우;노현우;서영민;구태형;고락길
    • 한국수소및신에너지학회논문집
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    • 제34권6호
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    • pp.615-622
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    • 2023
  • In this study, the theoretical analysis focused on the quantity of liquid hydrogen required for cooling down to 20 K, as well as the generation of boil-off gas (BOG) from the cooling process of the cryogenic components. The study involved calculating the amount of liquid hydrogen needed to achieve the desired temperature for the cryogenic components and subsequently determining the resulting BOG production at various reference temperatures. It was shown that it was important to efficiently lower the temperature of cryogenic parts through preliminary cooling. As a result, the reference temperature and pressure had an influence on the BOG generation on the cooling of cryogenic components using liquid hydrogen.

액체질소를 이용한 산화제펌프의 극저온 성능시험 (Cryogenic Performance Test of LOX Turbopump in Liquid Nitrogen)

  • 김진선;홍순삼;김대진;최창호;김진한
    • 대한기계학회논문집B
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    • 제34권4호
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    • pp.391-397
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    • 2010
  • 액체질소를 작동유체로 한 극저온 시험설비를 이용하여 산화제펌프의 성능시험을 수행하였다. 설계회전수의 30~55%영역에서 시험을 수행하였으며, 그 결과를 작동유체로 물을 이용한 상온수류시험의 결과와 비교/분석하였다. 수력성능에 있어서는 회전수에 대한 상사성을 만족시킴으로써, 설계회전수인 20000rpm에서의 성능예측을 가능하게 했다. 펌프의 극저온 흡입성능에서는 설계유량에서 극저온 임계 캐비테이션 수가 0.012으로 나타났으며, 상온수류시험의 경우는 0.024를 보이면서, 모든 시험회전수와 시험유량영역에서 수류시험의 경우보다 향상된 결과를 보였다. 이러한 향상된 극저온 환경에서의 흡입성능은 극저온 유체에서 펌프의 열역학적인 효과로부터 기인하는 것으로 판단된다.

다공성 매질에서 액화질소의 거동에 대한 연구 (STUDY ON BEHAVIOR OF LIQUID NITROGEN IN POROUS MEDIA)

  • 최성웅;이우일
    • 한국전산유체공학회지
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    • 제18권2호
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    • pp.17-25
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    • 2013
  • The process of flow through porous media is of interest a wide range of engineering fields and areas, and the importance of fluid flow with a change in phase arises from the fact that many industrial processes rely on these phenomena for materials process, energy transfer. Especially, the flow phenomena of cryogenic liquid subjected to evaporation is of interest to investigate how the cryogenic liquid behaves in the porous structure. In this study, thermo physical properties, morphological properties of the glass wool with different bulk densities in terms of its temperature-dependence and permeability behaviors under different applying pressure are discussed. Using the experimentally determined properties, characteristics of two main experimental results are investigated. In addition, simulation results are used to realize the cryogenic liquid's flow in porous media, and are compared with experimental results. By using the experimentally determined properties, more reasonable results can be suggested in dealing with porous media flow.