• 제목/요약/키워드: Cryogenic Liquid

검색결과 415건 처리시간 0.027초

Flow Instability of Cryogenic Fluid in the Downstream of Orifices

  • Thai, Quangnha;Lee, Chang-Jin
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.413-418
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    • 2008
  • Flow instability in the rocket turbo pump system can be caused by various reasons such as valve, orifice and venturi, etc. The inception of cavitation, especially in the propellant feeding system, is the primary cause of the mass flow and pressure oscillation due to cyclic formation and depletion of cavitation. Meanwhile, the main propellant in liquid rocket engine is the cryogenic one, which is very sensitive to temperature variation, and the variation of propellant properties caused by thermodynamic effect should be accounted for in the flow analysis. The present study focuses on the formation of cryogenic cavitations by adopting IDM model suggested by Shyy and coworkers. Also, the flow instability was investigated in the downstream of orifice by using a developed numerical code. Calculation results show that cryogenic cavitations can lead to flow instability resulting in mass flow fluctuations due to pressure oscillations. And the prediction of cavitations in cryogenic fluid is of vital importance in designing feeding system of LRE.

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극저온 추진제 고밀도화 기술동향 및 적용방안 (Review of Cryogenic Propellant Densification Technology)

  • 조남경;한상엽;김영목;정상권
    • 한국추진공학회지
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    • 제9권3호
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    • pp.133-144
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    • 2005
  • 기존 발사체 시스템의 성능을 향상시키는 방법의 하나로 액체산소와 액체수소와 같은 극저온 추진제를 고밀도화하는 기술이 최근 활발히 개발되고 있다. 극저온 추진제 고밀도화를 통하여 발사체에서 추진제의 질량분율을 높임으로 보다 큰 유상하중을 괘도에 진입시킬 수 있다. 본 논문에서는 극저온 추진제 고밀도화의 원리 및 최근 기술동향을 소개한다. 주로 액체산소의 고밀도화에 초점을 맞추어 여러 고밀도화 방법들에 대해서 소개하였다. 고밀도화된 극저온 추진제를 탑재한 발사체의 엔진 및 발사체 전체 성능해석 결과를 통하여, 발사체 시스템의 성능 향상을 정량적으로 소개하였다 또한 향후 극저온 추진제 고밀도화 기술의 국내 위성발사체 적용을 위한 방안을 간략히 제시하였다.

극저온 환경에서 스트레인 게이지의 겉보기 변형률 특성에 관한 연구 (The Apparent Strains of Strain Gages in Cryogenic Environment)

  • 주진원;김갑순
    • 대한기계학회논문집
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    • 제16권6호
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    • pp.1099-1107
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    • 1992
  • 본 연구에서는 극저온에서의 스트레인 게이지의 특성을 결정하기 위하여 이태 리의 표준기관인 IMGC (Istituto Di Metrologia "G.Colonnett")를 중심으로 세계의 측 정표준 기관과 대학이 참여하는 라운드 로빈(round robin) 시험이 진행되고 있다. 국내에서도 이 계획에 참여하여 본 연구를 수행하였다. 라운드 로빈 시험계획의 궁 극적인 목적은 세계의 주요 스트레인 게이지에 대해 여러가지 험조건에 의한 시험결과 를 가지고 극저온 환경에서의 변형측정에 이용될 수 있는 최적의 스트레인 게이지, 시 험재료, 전선연결, 시험장치 등의 시험조건을 선택하는 것이다. 이 목적을 위하여 본 연구에서는 가장 널리 쓰이는 3종류의 스트레인 게이지-미국Micro-Measurement, 일본 Kyowa, 독일 Hottinger Baldwin Mestechnik-에 대한 겉보기 변형률 대 온도의 곡선을 시험을 통하여 4.2K로 부터 293K까지의 온도 범위에서 구한다. 사용된 시편 은 스테인레스 강(AISI 316LN), 구리(Cu), 알루미늄(Al)이고 온도는 액체헬륨과 액체 질소를 이용하여 변화시켰으며, 그외의 모든 시험조건은 국제 법정계량기구(OIML) 규 정에 따라 모든 기관이 통일되도록 하였다.통일되도록 하였다.

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

  • 김동락;오영국;정영수;이정민;최창호;임기학;허남일;김양수;박영민
    • 한국초전도저온공학회:학술대회논문집
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    • 한국초전도저온공학회 2001년도 학술대회 논문집
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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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Experimental study on natural circulation using liquid nitrogen for superconducting applications

  • Choi, Yeon Suk
    • 한국초전도ㆍ저온공학회논문지
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    • 제15권3호
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    • pp.49-52
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    • 2013
  • An experiment to investigate the natural circulation of a cryogen has been performed. The study is motivated mainly by our recent development of cryogenic cooling system for prototype superconducting cyclotron without any circulating pump. In the natural circulation loop system, a cooling channel is attached on the outer surface of the aluminium block and the liquid nitrogen passes through inside of the channel to cool the block indirectly. A cryocooler as a heat sink is located at the top to re-condense cryogenic vapor coming from the aluminium block in which electrical heater is installed as a heat source. The main dimensions are determined using the relevant analysis and the natural circulation loop is successfully fabricated. The temperature distributions in the loop are measured during initial cool-down process and in steady state, from which the modified Grashof numbers are calculated and compared with the existing correlation estimated with one-dimensional analysis for steady state flow.

Mechanical Behavior of $Al_2O_3$ Dispersed CFRP Hybrid Composites at Room and Cryogenic Temperature

  • Manwar Hussain;Choa, Yong-Ho;Koichi Niihara
    • The Korean Journal of Ceramics
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    • 제5권4호
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    • pp.390-394
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    • 1999
  • Al2O3 particles were dispersed into carbon fiber reinforced epoxy composites to fabricate hybrid epoxy based composites. Interface behavior and mechanical properties of these hybrid composites were studied at room and liquid nitrogen temperature and liquid nitrogen temperature and the results were compared with the those of carbon fiber reinforced composites to investigate their applicability at room and cryogenic temperature. Young's modulus in-perpendicular to fiber direction and interlaminar shear strength at room temperature and the thermal contraction down to cryhogenic temperature were improved significantly by the addition of AL2O3 filler into the epoxy matrix. The effect of Al2O3 particle addition on mechanical properties were discussed.

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SINDA/FLUINT를 활용한 발사체 추진기관 공급계 해석 (Analysis of Propellant Feeding Sub-Systems for Liquid Rocket)

  • 조남경;정용갑;한상엽;김영목
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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    • pp.241-244
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    • 2006
  • The analysis of propellant feeding sub-system is performed using a commercial code SINDA/FLUINT, the comprehensive finite-difference, one-dimensional, lumped parameter tool. With the code, cryogenic helium supply system, liquid oxygen supply system, helium injection cooling system are evaluated. The code gave satisfactory estimation scheme for propulsion system characterized by cryogenic temperature and high pressure, two phase flow. This paper focuses on presenting calculation scheme of propulsion sub-system using one-dimensional code like SINDA/FLUINT.

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극저온 절삭공구에 의한 가공특성의 규명과 예측 (Searching and Prediction of Cutting Characteristics Using Cryogenic Tool)

  • 오석영;정우섭;김칠수;이소영
    • 한국정밀공학회지
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    • 제15권4호
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    • pp.36-43
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    • 1998
  • We experimented turning SCM440, called difficult-to-cut materials in general, using tungsten carbon tool(PIO) in order to elevate machinability by a new cutting method. The cutting tool designed and made to study was cooled to -17$0^{\circ}C$ in about 1 minute by liquid nitrogen. Then, we operated cryogenic cutting by cooling tool with liquid nitrogen and stuided the effect about cutting force, chip thickness, surface roughness, behavior of tool wear and cutting temperature. In addition, we investigated the possibility that sur face roughness of workpiece can be predicted analyzing cutting characteristics.

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왕복선 연료탱크 적용을 위한 탄소/고분자 복합재료의 극저온-고온 싸이클링 (CRYOGENIC AND ELEVATED TEMPERATURE CYCLING OF CARBON / POLYMER COMPOSITES FOR RESUABLE LAUNCH VEHICLE CRYOGENIC TANKS)

  • 예병한;원용구
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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    • pp.151-155
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    • 2003
  • An apparatus was developed to repetitively apply a -196 $^{\circ}C$ thermal load to coupon-sized mechanical test specimens. Using this device, IM7/5250-4 (carbon / bismaleimide) cross-ply and quasi-isotropic laminates were submerged in liquid nitrogen (L$N_2$) 400 times. Ply-by-Ply micro-crack density, laminate modulus, and laminate strength were measured as a function of thermal cycles. Quasi-isotropic samples of IM7/977-3 (carbon / epoxy) composite were also manually cycled between liquid nitrogen and an oven set at 120 $^{\circ}C$ for 130 cycles to determine whether including elevated temperature in the thermal cycle significantly altered the degree or location of micro-cracking. In response to thermal cycling, both materials micro-cracked extensively in the surface plies followed by sparse cracking of the inner plies. The tensile modulus of the IM7/5250-4 specimens was unaffected by thermal cycling, but the tensile strength of two of the lay-ups decreased by as much as 8.5 %.

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액체질소의 절연파괴특성 (Characteristics of Dielectric Breakdown in Liquid Nitrogen)

  • 추영배;류경우;류강식;김상현
    • 대한전기학회논문지
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    • 제37권12호
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    • pp.872-878
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    • 1988
  • During the past few years, a great deal of attention has been directed to the application of superconductivity to the electrical systems such as superconducting power transmission lines, superconducting magnet energy storage and so on. Yet in order to develop the practical model of these electrical equiqments utilizing suprconductivety and other phenomena at cryogenic temperautre, it is necessary to know the dielectric behaviour of insulating materials at cryogenic temperature in view of reliability, safety and economy of these machines. Investigation of dielectric properties of cryogenic liquids is very important due to the dual role of those as the dielectric and cooling medium. In this study, we investigated results measured over several kinds of dielectric characteristics of liquid nitrogen taking into consideration for application of high Tc superconductor. Dependence of breakdown voltage of gap width, polarity and pressure is reported in this paper and time delay characteristics of breakdown is also the subject of this discussion.

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