• Title/Summary/Keyword: Helium-3

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Evolutionary Models for Helium Giant Stars as Type Ibn Supernova Progenitors.

  • Kim, Jihoon;Yoon, Sung-Chul
    • The Bulletin of The Korean Astronomical Society
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    • v.43 no.2
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    • pp.40.1-40.1
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    • 2018
  • Among Type I supernovae, which show no evidence for hydrogen lines in spectra, Type Ib/c supernovae lack of strong Si absorption lines and are involved with massive progenitors. While strong helium absorption lines are present in Type Ib supernovae, narrow helium emission lines also can appear in some Type Ib that are often called Type Ibn supernovae (SNe Ibn). We consider helium giant stars as a promising progenitor candidate for SN Ibn and suggest the evolutionary scenario through binary systems using MESA code. In our models the range of primary mass is 11 - 20 solar mass, mass ratio is 0.5 - 0.9, and initial period is 1.5 / 1.7 / 2.0 / 2.5 / 3.0 day. In particular, we find that the evolution of the secondary star can overtake the primary through mass transfer from the secondary to the primary, which is so-called 'reverse case B' mass transfer. In such systems the secondary star may undergo a supernova explosion earlier than the primary star. In this case, the primary star evolves towards a single helium giant to become a SN Ibn progenitor. These cases are more frequent in relatively low initial primary mass.

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Helium Leak Test for the PLS Storage Ring Chamber (포항가속기 저장링챔버의 헬륨누설검사)

  • Choi, M.H.;Kim, H.J.;Choi, W.C.
    • Journal of the Korean Society for Nondestructive Testing
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    • v.13 no.3
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    • pp.31-38
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    • 1993
  • The storage ring vacuum system for the Pohang Light Source (PLS) has been designed to maintain the vacuum pressure of $10^{-10}Torr$ which requires UHV welding to have helium leak rate less than $1{\times}10^{-10}Torr{\cdot}{\ell}/sec$. In order to develop new technique (PLS) welding technique), a prototype vacuum chamber has been welded by using Tungsten Inert Gas welding method and all the welded joints have been tested with a non-destructive method, so called helium leak detection, to investigate the vacuum tightness of the weld joints. The test was performed with a detection limit of $1{\times}10^{-10}Torr{\cdot}{\ell}/sec$ for helium and no detectable leaks were found for all the welded joints. Thus the performance of welding technique is proven to meet the criteria of helium leak rate required in the PLS Storage Ring. Both the principle and the procedure for the helium leak detection are also discussed.

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First-principles investigations on helium behaviors in oxide-dispersion- strengthened nickel alloys with Hf additions

  • Yiren Wang;Fan Jia;Yong Jiang
    • Nuclear Engineering and Technology
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    • v.55 no.3
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    • pp.895-901
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    • 2023
  • Oxide-dispersion- strengthened nickel alloys with Hf additions are expected to present high temperature mechanical properties and durable helium resistance based on first-principles density functional theory (DFT) calculations. Energetic and charge density evaluations of the helium behaviors were performed in Ni matrix, Y2Hf2O7 oxide and the oxide/matrix interface. With the presence of coherent Y2Hf2O7 in Ni matrix, chances of helium bubbles in Ni can be greatly diminished. The helium atoms shall occupy the interfacial site initially, then diffuse into in the octahedral sites of Y2Hf2O7, and these oxide-captured He atoms prefer to separate individually. Much higher diffusion barrier of He in Y2Hf2O7 than in nickel is related to the strong hybridization between interstitial He-1s and nearest-neighboring O-2p orbitals.

Simulation Study of Hydrogen Liquefaction Process Using Helium Refrigeration Cycle (헬륨 냉동사이클을 이용한 수소액화 공정모사 연구)

  • Park, Hoey Kyung;Park, Jin-Soo
    • Applied Chemistry for Engineering
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    • v.31 no.2
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    • pp.153-163
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    • 2020
  • Compared to gaeous hydrogen, liquid hydrogen has approximately 1/800 volume, 800 times higher volumetric energy density at the same pressure, and the advantage of lower explosion risk and easier transportation than gaseous hydrogen. However, hydrogen liquefaction requires larger scale facility investment than simple compression storage method. Therefore, the research on energy-saving hydrogen liquefaction processes is highly necessary. In this study, helium/neon (mole ratio 80 : 20) refrigeration cycle was investigated as the main refrigeration process for hydrogen liquefaction. Process simulation for less energy consumption were carried out using PRO/II with PROVISION V10.2 of AVEVA. For hydrogen liquefaction, energy consumption was compared in three cases: Using a helium/neon refrigerant cycle, a SMR+helium/neon refrigerant cycle, and a C3-MR+helium/neon refrigerant cycle. As a result, the total power consumptions of compressors required to liquefy 1 kg of hydrogen are 16.3, 7.03 and 6.64 kWh, respectively. Therefore, it can be deduced that energy usage is greatly reduced in the hydrogen liquefaction process when the pre-cooling is performed using the SMR process or the C3MR process, which have already been commercialized, rather than using only the helium/neon refrigeration cycle for the hydrogen liquefaction process.

Test of evaluating performance of Helium recondensing type cryostat with 4 K GM cryocooler (4 K GM 극저온냉동기를 이용한 헬륨 재응축형 극저온용기의 성능 평가시험)

  • 김형진;김성래;심기덕;진홍범;권영길;장호명;이봉근
    • Proceedings of the Korea Institute of Applied Superconductivity and Cryogenics Conference
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    • 2002.02a
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    • pp.77-81
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    • 2002
  • The helium recondensing type cryostat with 4 K GM cryocooler is fabricated in order to keep cryogenic state of two saddle type superconducting magnet opposite to each other designed maximum 0.3 T magnetic field, and 1270 mm diameter open bore. The current leads which consist of metal current leads made for brass sheet and HTS current leads made in American Superconductor$^{TM}$ intermediate cool down with cryocooler Thus , the cryocooler for helium recondensing is a 1.5W/4.2 K GM SUMITOMO cryocooler. While superconducting magnet is working of 1600 gauss to 200 A, the cryostat keep constantly the level of liquid helium at 0.05 bar gauge pressure.e.

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An Experimental Study on Calibration Method of Heat Flux Sensor by using Helium Gas (헬륨을 이용한 열유속센서 검정방법의 실험적 연구)

  • Yang, Hoon-Cheul;Song, Chul-Hwa;Kim, Moo-Hwan
    • Proceedings of the KSME Conference
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    • 2004.11a
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    • pp.1219-1224
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    • 2004
  • The objective of this study is to propose an experimental calibration facility in which a heat flux sensor can be calibrated under conductive condition by using helium gas. The heat flux calibration facility was designed, simulated and manufactured for use in a high heat transfer condition. It delivers heat fluxes up to a maximum of 35 KW $m^{-2}$. A copper block heated electrically with 3.5 KW power is designed to produce uniform temperature up to 600 K across its face. High heat fluxes are provided between hot plate and cold plate by 1 mm height helium filled gap. A cold plate is maintained around 300 K through pool boiling using a refrigerant and water-cooled heat exchanger. A simulation was conducted to verify the design of the main test section. To verify the performance of calibration facility, a heat flux sensor was examined. The measured heat fluxes were compared to the calculated one.

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The Design of Cryogenic System for KSTAR TOKAMAK (KSTAR TOKAMAK을 위한 저온시스템의 설계)

  • 김동락;오영국;정영수;이정민;최창호;임기학;허남일;김양수;박영민
    • Proceedings of the Korea Institute of Applied Superconductivity and Cryogenics Conference
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    • 2001.02a
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    • pp.48-49
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    • 2001
  • Cryogenic technology is one of the key technologies for fusion reactor equipped with superconducting coil for plasma confinement. The KSTAR(Korea Superconducting Tokamak Advanced Research)Project is in progress since 1996. Major parameters of the KSTAR tokamak are : major radius 1.8m, minor radius 0.5m, toroidal field 3.5 Tesla and plasma current 2MA with a strongly shaped plasma cross-section and double -null diverter. Considering practical engineering constraints, the KSTAR device is designed for a pulse length of 300 sec in up-graded operation mode but in the initial configuration would provide a pulse length of 20 sec provided by the poloidal coil system in base-line operation mode. The cryogenic system is composed as follows : cold box, helium compressor system, distribution box, helium gas buffer tank, helium gas purifying system, gas recovery system, liquid helium storage dewar, current lead box, current bus line and liquid nitrogen storage tank.

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The effect of helium thermal treatment using ZnO thin films (Zno 박막의 Helium 열처리에 대한 효과)

  • Ryu, Kung-Yul;Baek, Kyung-Hyung;Park, Hyeong-Sik;Jang, Kyung-Soo;Jung, Sung-Wook;Jeong, Han-Uk;Yun, Eui-Jung;Yi, J.
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2010.06a
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    • pp.145-145
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    • 2010
  • It is observed from SEM images that many voids were created after annealed by helium gas. The PL spectra of the ZnO samples revealed the strong violet emission peaks at 3.05 eV with the relative weak near band edge UV emissions. It was concluded from experiment results that native $Zn_i$ and $V_o$ donor defect levels can be generated below the conduction band edge due to the incorporation of helium atoms decomposed from helium gas into the ZnO matrix. He atoms in ZnO matrix will affect the interface trap existing in depletion regions located at the grain boundaries, which leads to the creation of $Zn_i$ and $V_o$ donor defect levels.

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A Study on Steady and Unsteady Behavior of Helium Jet in the Stationary Atmosphere (헬륨 기체분류의 정상적 비정상적 거동에 관한 연구)

  • Kim, B.G.;Suh, Y.K.;Ha, J.Y.;Kwon, S.S.
    • Transactions of the Korean Society of Automotive Engineers
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    • v.1 no.3
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    • pp.34-45
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    • 1993
  • This study aims to analyze the mixing characteristics of hydrogen considered as a new fuel for internal combustion engines. As the physical property of helium gas is similar to that of hydrogen, helium gas was used in this study. To analyze the steady and unsteady behavior of jet, helium gas was injected into the stationary atmosphere at the normal temperature and pressure. Concentration of helium gas in the center of jet flow is in inverse proportion with axial distance from the nozzle tip. This agrees with the free jet theory of Schlichting. The relative equation for dimensionless concentration to radial/axial distance the axial distance of potential core region, the cone angle a of the jet flow and the relative equation for arriving distance of the front of jet flow to the lapse of time are obtained. But free jet theory of Schlichting in the dimensionless concentration is not in agreement with the present experimental results of the distance of the radial direction. It needs more study. When the arrival frequency of jet flow is used as a parameter, the transition area changing from unsteady flow area into steady flow area becomes gradually wider downstream, but its ratio for the whole unsteady flow area gradually decreases.

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