• 제목/요약/키워드: Base Fluid

검색결과 424건 처리시간 0.024초

대화 Mo-W 열수 맥상 광상의 유체 진화 특성 (Evolution of Hydrothermal Fluids at Daehwa Mo-W Deposit)

  • 조진희;최상훈
    • 자원환경지질
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    • 제46권1호
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    • pp.11-19
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    • 2013
  • 대화광상은 경기육괴의 편마암류와 화강암류에 발달한 열극을 충진 발달한 함 Mo-W 열수 맥상 광상이다. 대화광상의 몰리브덴-텅스텐 광화작용과 관련된 주요 수반광물인 석영에서 관찰되는 유체포유물은 상온 ($20^{\circ}C$) 에서의 상(phase) 관계와 냉각 및 가열 실험을 통해 측정된 균일화 온도와 상변화를 기초로 하여 3가지 주요 유형 (Type I, 액상이 우세한 $H_2O$-NaCl 유형; Type II, 기상이 우세한 $H_2O$-NaCl 유형; Type III; $CO_2-H_2O$-NaCl 유형) 으로 분류된다. 또한, 함 $CO_2$ Type III 유체포유물은 $CO_2$ 균일화 및 최종 균일화 특성을 바탕으로 4가지 유형 (IIIa, IIIb, IIIc, IIId)으로 세분된다. 대화광상 Type I 유체포유물의 균일화 온도는 약 $374^{\circ}C{\sim}161^{\circ}C$로 넓은 범위를 보여주며, 염농도 역시 약 13.6~0.5 equiv. wt. % NaCl의 넓은 조성 범위를 보인다. Type III 유체포유물 냉각 실험 시 측정된 $CO_2$ 상의 용융 온도는 $-57.4{\sim}-56.6^{\circ}C$이며, $CO_2$ 균일화 온도는 $29.0{\sim}30.8^{\circ}C$이다. 또한 $CO_2$ clathrate 용융 온도는 $7.3{\sim}9.5^{\circ}C$로 염농도는 5.2~1.0 equiv. wt. % NaCl이고, 최종 균일화 온도는 $303^{\circ}C{\sim}251^{\circ}C$로 비교적 좁은 범위로 확인되었다. $CO_2-H_2O$-NaCl계 (Type III) 유체포유물의 경우 온도가 감소함에 따라 염농도 역시 감소하는데, 이는 높은 염농도를 가진 $H_2O$-NaCl계 유체와 낮은 염농도를 가진 $CO_2-H_2O$-NaCl계 유체의 불혼화에 의해 열수의 진화가 이루어졌음을 의미한다. Type I 유체포유물은 온도 감소와 염농도 사이의 뚜렷한 변화가 인지되지 않았다. 따라서, 대화 열수계의 함 몰리브덴-중석 광화작용은 $400^{\circ}C$, 5.2 equiv. wt.% NaCl의 염농도를 가진 광화유체로부터 시작되어, 약 $350^{\circ}C$ 부근에서 유체의 불혼화 용융에 의해 진행되었다. 이후 대화 열수계에 유입된 상대적으로 낮은 온도와 염농도를 갖는 유체 (천수 또는 상대적으로 높은 물/암석 비를 갖는 열수유체) 의 혼입 작용에 의해 후기 천금속 광화작용이 야기되었다.

경상남도 함안-군북지역의 동광화작용: 유체포유물 및 안정동위원소 연구 (Copper Mineralization in the Haman-Gunbuk Area, Gyeongsangnamdo-Province: Fluid Inclusion and Stable Isotope Study)

  • 허철호;윤성택;최상훈;최선규;소칠섭
    • 자원환경지질
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    • 제36권2호
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    • pp.75-87
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    • 2003
  • 함안-군북 광화대는 한반도 남동부의 백악기 경상분지내에 위치해있다. 자철석, 회중석, 휘수연석, 황동석의 주광석 광물과 천금속 및 소량의 황염광물이 백악기 퇴적암, 화산암, 화강섬록암(118${\pm}$3.0 Ma)내에 발달된 열극을 충진한 전기석, 석영 및 탄산염맥내에서 산출된다. 광석 및 맥석광물들은 세 개의 광화시기로 구분될 수 있다: 광화 1기, 전기석+석영+철-동광석: 광화 2기, 석영+황화광물+황염광물+탄산염광물; 광화 3기, barren한 방해석. 광화 1기 및 2기의 초기 유체는 고염농도(35~70 equiv. wt.% NaCl+KCl)이며, 기상이 풍부하고 약 300$^{\circ}$~50$0^{\circ}C$의 온도에서 균질 되었다. 비록 황화물 광물이 상기유체에 의해 생성된 초기광물조합과 연관성이 없을지라도, 고염농도의 유체는 상당량의 나트륨, 칼륨, 철, 동, 황을 함유하는 염화물복합체 염수로 사료된다. 후기 용액은 새롭게 생성된 열극 및 맥을 따라 순환되었으며, 낮은 염농도($\leq$20 equiv. wt.% NaCl)이며 약200$^{\circ}$~40$0^{\circ}C$에서 균질화되었다. 할안-군북 열수계 유체의 산소-수소 동위원소조성은 광화초기에는 마그마성 열수의 특징을 보이다가 점차 광화후기로 가면서 순환수성 열수의 특징을 보여주고 있다. 함안-군복지역의 광체가 부존된 화강섬록암내에서 손환하고 있는 초기 열수성유체는 정출마그마에서 용리된후 고염농도의 액상을 함유한 유체와 $H_2O$-NaCl계의 기상으 함유한 유체로 불혼화되었다. 상기 마그마유체가 열극을 따라 이동하면서, 다른 황화광물과 황염광물의 침전없이 전기석 및 초기 철, 텅스텐, 몰리브데늄, 동 광화작용을 유발시켰다. 순환수기원의 후기광화용액은 동과 천금속 황화물, 황염광화작용을 촉발시켰다.

원형관내 나노유체의 강제대류에 관한 수치적 연구 (NUMERICAL STUDY OF NANOFLUIDS FORCED CONVECTION IN CIRCULAR TUBES)

  • 최훈기;유근종
    • 한국전산유체공학회지
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    • 제19권3호
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    • pp.37-43
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    • 2014
  • In this paper, hydraulic & thermal developing and fully developed laminar forced convection flow of a water-$Al_2O_3$ nanofluid in a circular horizontal tube with uniform heat flux at the wall, are investigated numerically. A single phase model employed with temperature independent properties. The thermal entrance length is presented in this paper. The variations of the convective heat transfer coefficient and shear stress are shown in the entrance region and fully developed region along different nanoparticles concentration and Reynolds numbers. Convective heat transfer coefficient for nanofluids is larger than that of the base fluid. It is shown that heat transfer is enhanced and shear stress is increased as the particle volume concentration increases. The heat transfer improves, as Reynolds number increases.

반응표면법을 이용한 평행류 열교환기의 형상 최적화 (Optimal Shape of a Parallel-Flow Heat Exchanger by Using a Response Surface Method)

  • 오석진;이관수
    • 대한기계학회논문집B
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    • 제28권3호
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    • pp.296-303
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    • 2004
  • The heat and flow characteristics in a single-phase parallel-flow heat exchanger was examined numerically to obtain its optimal shape. A response surface method was introduced to approximately predict its performance with respect to the design parameters over the design domain. The inflow/outflow angle of the working fluid, the location of inlet/outlet, the protruding height of flat tube and the height of header were chosen as a design parameter The evaluation of the relative importance of the design parameters was performed based on a sensitivity analysis. An efficiency index was used as an evaluation characteristics value to simultaneously consider both the heat transfer and the pressure drop. The efficiency index of the optimum model, compared to that of the base model, was increased by 9.3%.

수중펌프의 Leakage-free 자동탈착장치 개발 (Development of Leakage-free Automatic Discharge Connect in a Submersible Pump.)

  • 최영석;이경용;이창한;이종훈
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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    • pp.63-68
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    • 2002
  • ADC(Automatic Discharge Connector) is commonly used for the easy maintenance of the submersible pumps. However, the small gap between the flange of the base plate and that of the pipe due to the head rise, the flow momentum change and the mis-installation makes leakage flow that may be a great loss to the pumping system. In this study, the performance degradation was predicted with the simple leakage flow model through the gap. The newly developed ADC was tested and the leakage performance was compared with the old one and also no-leakage piping system. The newly developed ADC reduced the leakage flow in a satisfactory way in comparison with the old model.

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카본나노튜브 나노유체의 동점성계수 증가로 인한 관내 유동에서의 항력 감소 (Drag Reduction Induced by Increased Kinematic Viscosity of Nanofluids Containing Carbon Nanotubes in A Horizontal Tube)

  • 유지원;정세권;최만수
    • 한국입자에어로졸학회지
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    • 제9권4호
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    • pp.271-277
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    • 2013
  • This article reports the drag reduction phenomenon of aqueous suspensions containing carbon nanotubes (CNTs) flowing through horizontal tubes. Stable nanofluids were prepared by using a surfactant. It is found that the drag forces of CNT nanofluids were reduced at specific flow conditions compared to the base fluid. It is found that the friction factor of CNT nanofluids was reduced up to approximately 30 % by using CNT nanofluids. Increased kinematic viscosities of CNT nanofluids are suggested to the key factors that cause the drag reduction phenomenon. In addition, transition from laminar to turbulent flow is observed to be delayed when CNT nanofluids flow in a horizontal tube, meaning that drag reduction occurs at higher flow rates, that is, at higher Reynolds numbers.

반응표면법을 이용한 평행류 열교환기의 설계인자 최적화 (Optimal Design of a Parallel-Flow Heat Exchanger by Using a Response Surface Method)

  • 오석진;이관수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.1028-1033
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    • 2004
  • The heat and flow characteristics in a single-phase parallel-flow heat exchanger was examined numerically to obtain its optimal shape. A response surface method was introduced to predict its performance approximately with respect to design parameters over design domain. Design parameters are inflow and outflow angle of the working fluid and horizontal and vertical location of inlet and outlet. The evaluation of the relative priority of the design parameters was performed to choose three important parameters in order to use a response surface method. A JF factor was used as an evaluation characteristic value to consider the heat transfer and the pressure drop simultaneously. The JF factor of the optimum model, compared to that of the base model, was increased by about 5.3%.

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자동차용 유압관로의 주파수 응답 특성 (Frequency Response Characteristics of Automotive Hydraulic Pipelines)

  • 김도태
    • 한국자동차공학회논문집
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    • 제15권6호
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    • pp.177-182
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    • 2007
  • In this paper, automotive hydraulic pipeline systems are modeled in which a straight blocked pipe, two pipes with sudden expansion or contraction are connected in series and terminated with a chamber. The frequency response characteristics of these composite pipeline systems are investigated experimentally. The theoretical analysis for various pipe configurations is base on transfer matrix method with frequency dependent viscous friction distributed parameter pipeline model. The gain and phase of transfer functions are included for comparison with experimental results. There is close agreement between the results of experimental and theoretical determination of pressure response in automotive hydraulic pipeline systems.

초경팁 납접형 둥근톱의 공구 마멸 (Tool Wear of the Tungsten Carbide Tipped Circular Saw)

  • 이재우
    • 한국정밀공학회지
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    • 제19권2호
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    • pp.228-236
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    • 2002
  • In this study, the carbon steels, SM20C were machined with the tungsten carbide tipped circular saw to clarify the cutting-off characteristics in terms of tool wear. The results show that an improved performance in view of both the tool wear and the cutting efficiency was obtained by using oil base cutting fluid at the cutting speed of 100m/min with the feed of 0.06mm/tooth. The rake angle of 10$^{\circ}$ , clearance angle of 8$^{\circ}$ , nose radius of R0.1mm, and end cutting edge champer of 0.1mm$\times$25$^{\circ}$ are believed as the best tool geometries. The tool wear decreases due to using the saw of the disk of STS5 and the tool material of P30.

틸트로터 무인기의 날개-나셀 공력해석 (Aerodynamic Analysis on Wing-Nacelle of Tiltrotor UAV)

  • 최성욱;김철완;김재무
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2004년도 춘계 학술대회논문집
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    • pp.27-34
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    • 2004
  • In the Smart UAV Development Program, one of the 21c Frontier R&D Program, the tiltrotor has been studied as the concept of vehicle. The tiltrortor aircraft take-off and land in rotary wing mode like conventional helicopter, and cruise in fixed wing mode like conventional propeller airplane. For the conversion of the flight mode from helicopter to airplane, the nacelle located at wing tip has to be tilted from about 90 degrees of helicopter mode to about 0 degree of airplane mode. In this study, the aerodynamic characteristics of the wing with tilted nacelle is investigated using computation fluid dynamics technique. In order to feature out aerodynamic interferences between wing and nacelle, the flow calculations are conducted for the wing and the nacelle separately and for the combined geometry of wing and nacelle, respectively. Through this computations, not only the aerodynamic data-base for the wing-nacelle is constructed but also its contribution to the configuration design of the wing-nacelle is anticipated.

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