• Title/Summary/Keyword: gaseous helium

Search Result 26, Processing Time 0.019 seconds

Electrical Breakdown and Flashover Characteristics of Gaseous Helium at Cryogenic Temperature (극저온 헬륨가스의 절연파괴 및 연면방전 특성)

  • Kwag, Dong-Soon
    • Progress in Superconductivity and Cryogenics
    • /
    • v.14 no.3
    • /
    • pp.38-42
    • /
    • 2012
  • Fixtures such as bushings in terminations of high temperature superconducting(HTS) power cable systems are subjected to high voltages, which have to transition from ambient to cryogenic temperatures. As such it is imperative to ensure the integrity of the dielectrics under all operating conditions, including thermal aspects brought about by the passage of current. Gaseous helium(GHe) at high pressure is regarded as a potential coolant for superconducting cables. The dielectric aspects of cryogenic helium gas are both complex and demanding. In this experimental study we looked at the interface between a smooth epoxy surface and high pressure helium gas in a homogeneous electric field. The alternating current(AC) flashover voltages of epoxy samples are presented. The results have been analyzed by using Weibull statistics. In addition to the behavior of the epoxy in gaseous helium as a function of pressure and temperature we also present data of the characteristics of the epoxy in mineral oil and in liquid nitrogen($LN_2$). The breakdown characteristics of a uniform field gap in gaseous helium as a function of pressure and temperature under AC, direct current(DC) and lightning impulse voltages are also given. Electric field calculations have been made for one of the experimental geometries in an attempt to explain some of the anomalies in the experimental results.

Flame Extinguishing Characteristics of Clean Gaseous Agents and Effects of Additives (가스계 청정소화약제의 소화특성과 첨가제에 따른 영향)

  • Shin, Chang-Sub;Kim, Sung-Min
    • Journal of the Korean Society of Safety
    • /
    • v.23 no.6
    • /
    • pp.95-99
    • /
    • 2008
  • Halon was known as a cause of the ozone layer destruction. In 1987, it was designated as one of the ozone-layer-destroying materials in the Montreal Protocol. Therefore substitutes of Halon agent has been developed including inert gas extinguish system, which is one of the most widely used fire extinguishing system. This study intended to increase the efficiency of inert gas extinguishing agent by using inert gas additives. As IG-541 shows high extinguishing power, the experiment was performed to measure the effects of gaseous additives to it. Cup-burner fire extinguishing apparatus was used with n-Heptane fuel. Among many of pure inert gaseous agents, Helium showed the most excellent extinguishing power. When Helium was added to IG-541, fire extinguishing power was increased and the concentration of oxygen in chimney also risen. By adding Helium to IG-541, the effectiveness of inert gas fire extinguishing system is able to be increased.

REBCO coil operation in gaseous helium and solid nitrogen

  • Diev, D.N.;Makarenko, M.N.;Naumov, A.V.;Polyakov, A.V.;Shcherbakov, V.I.;Shutova, D.I.;Surin, M.I.
    • Progress in Superconductivity and Cryogenics
    • /
    • v.21 no.3
    • /
    • pp.47-50
    • /
    • 2019
  • The paper gives the results of the experiments with a model two-section REBCO solenoid cooled by either gaseous helium (GHe) or sub-cooled/solid nitrogen (SN2) in (50-77) K temperature range. The major cooling source was a single-stage cryocooler Sumitomo CH-110 with the cooling power of 175 W and 130 W at 77 K and 50 K respectively. The coil itself was not directly conduction cooled. We compare the time taken by both coolants to obtain the temperature of the magnet of about 50 K and the homogeneity of the temperature distribution within the cryostat. Test results for the coil operation in solid nitrogen together with the comparison of its critical properties in SN2 and GHe are also presented.

Development Test of Pyro-Valve for Cryogenic Gaseous Helium in Pressurization System of Launch Vehicle (발사체 가압시스템용 극저온 헬륨가스 파이로밸브 개발시험)

  • Chung, Yong-Gahp;Han, Sang-Yeop;Cho, In-Hyun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2009.11a
    • /
    • pp.293-297
    • /
    • 2009
  • Valves, which are used to supply or block the flow of cryogenic pressurant in the pressurization system of liquid-propellant propulsion system in a launch vehicle, are pneumo-actuated valve, solenoid valve, pyro-valve, etc. Both pneumo-actuated valve and solenoid valve have more complex structure and are heavier than pyro-valve. For this study, a couple of pyro-valves, which are applicable to cryogenic and high-pressure fluid (cryogenic gaseous helium), have a simple structure, and are comparably light, are designed, manufactured, and tested (proof-pressure/leakage tests, performance test, vibration test, helium supply tests).

  • PDF

Characteristic analysis and condenser design of gas helium circulation system for zero-boil-off storage tank

  • Jangdon Kim;Youngjun Choi;Keuntae Lee;Jiho Park;Dongmin Kim;Seokho Kim
    • Progress in Superconductivity and Cryogenics
    • /
    • v.25 no.4
    • /
    • pp.65-69
    • /
    • 2023
  • Hydrogen is an eco-friendly energy source and is being actively researched in various fields around the world, including mobility and aerospace. In order to effectively utilize hydrogen energy, it should be used in a liquid state with high energy storage density, but when hydrogen is stored in a liquid state, BOG (boil-off gas) is generated due to the temperature difference with the atmosphere. This should be re-condensed when considering storage efficiency and economy. In particular, large-capacity liquid hydrogen storage tank is required a gaseous helium circulation cooling system that cools by circulating cryogenic refrigerant due to the increase in heat intrusion from external air as the heat transfer area increases and the wide distribution of the gas layer inside the tank. In order to effectively apply the system, thermo-hydraulic analysis through process analysis is required. In this study, the condenser design and system characteristics of a gaseous helium circulation cooling system for BOG recondensation of a liquefied hydrogen storage tank were compared.

Heating Apparatus Development for Cryogenic Gaseous Helium (극저온 헬륨가스 가열장치 개발)

  • Chung, Yong-Gahp;Kwon, Oh-Sung;Cho, Nam-Kyung;Cho, In-Hyun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2009.11a
    • /
    • pp.363-367
    • /
    • 2009
  • For the liquid rocket propulsion system using liquid oxygen as oxidizer, helium for pressurizing LOX is usually stored in the LOX tank with cryogenic temperature. For that kind of pressurizing system, cryogenic helium is discharged from the immerged pressurant cylinder and passes through the heat exchanger downstream of gas generator. During the process, helium pressurant is heated from cryogenic temperature to high one and supplied to the ullage of propellant tank. To develop the pressurizing system, a cryogenic heating apparatus is needed to simulate the heat exchanger. In this paper, the cryogenic heating apparatus for development of the pressurization system is presented along with its heating test results with cryogenic helium.

  • PDF

Heating Apparatus Development and Tests for Cryogenic Gaseous Helium (극저온 헬륨가스 가열장치 개발 및 시험)

  • Chung, Yong-Gahp;Cho, Nam-Kyung
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.15 no.1
    • /
    • pp.63-68
    • /
    • 2011
  • For the liquid rocket propulsion system using liquid oxygen as oxidizer, helium for pressurizing LOX is usually stored in the LOX tank with cryogenic temperature. For that kind of pressurizing system, cryogenic helium is discharged from the immerged pressurant cylinder and passes through the heat exchanger downstream of gas generator. During the process, helium pressurant is heated from cryogenic temperature to high one and supplied to the ullage of propellant tank. To develop the pressurizing system, a cryogenic heating apparatus is needed to simulate the heat exchanger. In this paper, the cryogenic heating apparatus for development of the pressurization system is presented along with its heating test results with cryogenic helium.

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

  • Cho, Nam-Kyung;Jeong, Sang-Kwon
    • Progress in Superconductivity and Cryogenics
    • /
    • v.9 no.3
    • /
    • pp.72-82
    • /
    • 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.

Development and Test results of the Dielectric Evaluation System for a Helium Gas Cooled HTS Cable (헬륨가스 냉각 고온초전도 케이블의 절연특성 평가 시스템 개발 및 성능평가)

  • Kwag, Dong-Soon;Rodrigo, Horatio
    • Progress in Superconductivity and Cryogenics
    • /
    • v.14 no.1
    • /
    • pp.25-29
    • /
    • 2012
  • The novel type of cable under consideration is cooled by gaseous Helium at elevated pressure. Helium is known for having poor electric breakdown strength; therefore the dielectric capabilities of this type of cable must be tested under conditions similar to the envisaged operation. In order to study the dielectric performance we have designed and built a novel high pressure cryostat rated at 2.17 MPa which has been used for testing model cables of lengths of up to 1 m. The cryostat is an open system where the gas is not re-circulated. This allows maintaining a high purity of the gas. The target temperature range is between 40 K and 70 K. This substantially increases the critical current density of the HTS compared to 77 K, which is the typical temperature of cables cooled by liquid nitrogen. The cryostat presented allows for adjusting the temperature and keeping it constant for the time necessary to run a complete dielectric characterization test. We give a detailed description of the cryostat. Measurements of partial discharge inception voltages as well as the temperature distribution along the model cables as a function of time are presented.

Analysis on the Dielectric Characteristics of Various Insulation Gases for Developing a Sub-cooled Liquid Nitrogen Cooling System (과냉질소 냉각시스템 가압용 기체의 절연내력특성 분석)

  • Kang, H.;Ko, T.K.
    • Progress in Superconductivity and Cryogenics
    • /
    • v.13 no.1
    • /
    • pp.27-30
    • /
    • 2011
  • A sub-cooled liquid nitrogen cooling system is known as a most promising method to develop large scale superconducting apparatuses such as superconducting fault current limiters and superconducting cables [1]. Gaseous helium (GHe), gaseous nitrogen ($GN_2$) and sulfur hexafluoride ($SF_6$) are commonly used for designing an high voltage applied superconducting device as an injection gaseous medium [2, 3]. In this paper, the analysis on the dielectric characteristics of GHe, $GN_2$ and $SF_6$ are conducted by designing and manufacturing sphere-to-plane electrode systems. The AC withstand voltage experiments on the various gaseous insulation media are carried out and the results are analyzed by using finite element method (FEM) considering field utilization factors (${\xi}$). It is found that the electric field intensity at sparkover ($E_{MAX}$) of insulation media exponentially decreases according to ${\xi}$ increases. Also, the empirical expressions of the functional relations between $E_{MAX}$ and ${\xi}$ of insulation media are deduced by dielectric experiments and computational analyses. It is expected that the electrical insulation design of applied superconducting devices could be performed by using the deduced empirical formulae without dielectric experiments.