• Title/Summary/Keyword: 흡입압력

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An Experimental Study on the combustion Characteristics in the Helmholtz-Type Pulsating Combustor (헬름홀쯔형 맥동연소기의 연소 및 작동특성에 관한 실험적 연구)

  • 길상인;신현동
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.15 no.5
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    • pp.1727-1736
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    • 1991
  • 본 연구에서는 자체 제작된 헬름홀쯔형 맥동 연소기를 이용하여 작동원리와 연소특성을 조사함으로써 맥동연소현상을 물리적으로 이해하는 것이다. 주기적 화염 의 직접가시화, 연소장의 시간평균 온도 및 농도분포, 변동압력의 크기와 공기흡입량 을 조사함으로써 맥동에 영향을 미치는 요인이 무엇인지 그리고 이것이 어떠한 변화를 야기시키는가를 살펴보고자 한다. 이렇게 얻어진 결과의 종합을 통해 장치의 형상이 결정된 일반적인 맥동연소기가 자발적인 상태에서 작동될 때 작동결정인자가 무엇인가 를 알수가 있을 것으로 사료된다.

Design of Thermal Vapor Compressor by Numerical Analysis and Experimental Verification (전산해석을 통한 열증기압축기 설계와 실험적 검증)

  • Park, Il-Seouk;Park, Sang-Min;Ha, Ji-Soo
    • The KSFM Journal of Fluid Machinery
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    • v.8 no.6 s.33
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    • pp.33-39
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    • 2005
  • A thermal vapor compressor in which the subsonic/supersonic flow appears simultaneously, has been accurately designed through the CFD analysis for the various shape parameters such as the primary nozzle shape, converging duct shape, mixing tube diameter, and so on. The performance of the developed thermal vapor compressor has been experimentally verified to be installed in a Multi Effect Desalination(MED) plant as an important element. In this paper, the effects of each parameter are discussed on the basis of CFD results and the experimental results for various boundary conditions(motive pressure, suction pressure, and discharge pressure) are presented in compared with CFD results. The two results show a good agreement with each other within 2 % accuracy with regard to the entrainment ratio.

Development of Vacuum Sprinkler Extinguishing System (부압식 스프링클러설비)

  • Oh, Ju-Hwan
    • Proceedings of the Korea Institute of Fire Science and Engineering Conference
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    • 2011.11a
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    • pp.61-66
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    • 2011
  • 부압식 스프링클러 설비는 우리나라에서 일반적으로 사용되고 있는 준비작동식이나 건식 또는 습식 스프링클러 설비의 2차측 배관내의 압력을 부압(진공)상태로 유지시켜 오작동(스프링클러 헤드의 파손 또는 배관의 누수) 시에 발생되는 소화수의 누수를 진공압(-0.05~-0.08MPa)으로 흡입하는 구조로 설계되어 수손피해에 대한 위험도를 제거 하여 기존의 스프링클러 시스템의 문제점을 해결 할 수 있는 획기적인 기술로 볼 수 있다. 또한 부압식 스프링클러 설비는 습식, 준비작동식에 해당하는 시설에 모두 적용이 가능하며 매년 국내, 외에서 건설되는 모든 대상물에도 설치가 가능하며 기존 설비된 건물에도 손쉽게 적용이 가능하여 앞으로 IT관련 산업, 반도체 제조공장, 호텔, 학교, 병원, 관공서, 지하철 역사, 정밀가공 제조설비 등 특히 내진설계에 적용되고 있는바 그 적용성이 무궁무진한바 본 부압식 스프링클러 시스템의 연구를 통한 확대에 대한 가능성은 무한할 것으로 예상된다.

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Robust Design for Shape Parameters of High Pressure Thermal Vapor Compressor by Numerical Analysis (전산해석을 통한 고압열증기압축기 형상변수에 관한 강건 설계)

  • Park, Il-Seouk
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.32 no.12
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    • pp.931-937
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    • 2008
  • A high motive pressure thermal vapor compressor(TVC) for a commercial multi-effect desalination(MED) plant is designed to have a high entraining performance and its robustness is also considered in the respect of operating stability at the abrupt change of the operating pressures like the motive and suction steam pressure which can be easily fluctuated by the external disturbance. The TVC having a good entraining performance of more than entrainment ratio 6.0 is designed through the iterative CFD analysis for the various primary nozzle diameter, mixing tube diameter and mixing tube length. And then for a couple of TVC having a similar entrainment ratio, the changes of the entrainment ratio are checked along the motive and suction pressure change. The system stability is diagnosed through the analyzing the changing pattern of the entrainment ratio.

온라인 기계 진동 관리 시스템을 이용한 가스 압축기 선회 실속의 원격 진단

  • 장은구
    • Journal of KSNVE
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    • v.14 no.1
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    • pp.18-23
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    • 2004
  • 균열 현상은 모든 필터에서 발생하였다. 1997년 9월 원심 압축기 B에서 발생한 지나친 진동현상으로 여러 필터 중 한 필터가 부서져 임펠러 흡입부로 빨려 들어갔다. 1997년 10월 기동중에 선회실속 문제가 임펠러에서 발생하였고, 이 원인은 임펠러 eye가 부분적으로 막혔기 때문이었다. 압축기 입구와 출구의 전체 유량과 압력 상태는 정상이었기 때문에 어떠한 서지현상도 anti-surge 시스템에 의해서 감지되지 않았다. 고장상태를 진단함으로써 압축기의 재가동을 방지하여 필터들이 부서졌다는 것을 확인하게 되었다. 이번 기계 점검과정을 통하여 원격진단의 중요성을 확인하였으며, 이에 회사는 원격서비스(remote service) 계약을 체결하여 현재 원격 진단 서비스 점검이 계약 기간에 따라 정기적으로 이루어지고 있다. 이와 같이 기계에 대한 정기적인 점검을 실시하는 목적은 기계의 결함이나 고장문제를 조기에 발견함으로써 중대한 고장으로의 진행을 사전에 예방하거나 또는 최소화하는데 있다.

A Biomechanical Modeling of Human Pharyngeal Muscular Dysfunction by Using FEM(Finite Element Method) (유한요소법을 이용한 인두의 기능이상에 대한 생체역학적 모델)

  • Kim Sung Jae;Bae Ha Suk;Choi Byeong Cheol;Kim Sung Min
    • Journal of Biomedical Engineering Research
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    • v.24 no.6 s.81
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    • pp.515-522
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    • 2003
  • Pharynx is a system transporting foods by peristaltic motion(contraction and expansion movement! into the esophagus and functioning as airway passages. In this study, structural changes of pharyngeal dysfunction are analyzed by biomechanical model using CT and FEM(finite clement method). Loading condition was assumed that equal pressure was loaded sequentially to inside of pharyngeal tissue. In order to analyze the pharyngeal muscular dysfunction by biomechanical model. the pharyngeal dysfunctions was classified into 3 cases. Taking into account the clinical complication by neuromuscular symptoms such as pharyngeal dysfunction after stroke. we assumed that a change of material property is caused by muscular tissue stiffness. A deformation of cross sectional area of the pharynx is analyzed increasing the stiffness $25\%,\;50\%,\;75\%$ in each case on the basis of stress-strain relationship. Based on three-dimensional reconstruction of pharyngeal structure using limited factor - techniques and the optimization procedure by means of inverse dynamic approach. the biomechanical model of the human pharynx is implemented. The results may be used as clinical index illustrating the degree of pharyngeal muscular dysfunction. This study may be used as useful diagnostic model in discovering early deglutitory impediment caused by physiological or pathological pharyngeal dysfunction.

Research Activities of Transpiration Cooling for High-Performance Flight Engines (고성능 비행체 엔진을 위한 분출냉각의 연구동향)

  • Hwang, Ki-Young;Kim, You-Il
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.10
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    • pp.966-978
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    • 2011
  • Transpiration cooling is the most effective cooling technique for the high-performance liquid rockets and air-breathing engines operating in aggressive environments with higher pressures and temperatures. When applying transpiration cooling, combustor liners and turbine blades/vanes are cooled by the coolant(air or fuel) passing through their porous walls and also the exit coolant acting as an insulating film. Practical implementation of the cooling technique has been hampered by the limitations of available porous materials. But advances in metal-joining techniques have led to the development of multi-laminate porous structures such as Lamilloy$^{(R)}$ fabricated from several diffusion-bonded, etched metal thin sheets. And also with the availability of lightweight, ceramic matrix composites(CMC), transpiration cooling now seems to be a promising technique for high-performance engine cooling. This paper reviews recent research activities of transpiration cooling and its applications to gas turbines, liquid rockets, and the engines for hypersonic vehicles.

Numerical Study on Cavitation Performance Evaluation in a Centrifugal Pump Impeller (원심펌프 임펠러의 캐비테이션 성능평가에 관한 수치적 연구)

  • Mo, Jang-Oh;Kim, You-Taek;Lee, Young-Ho
    • Journal of Advanced Marine Engineering and Technology
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    • v.36 no.2
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    • pp.286-293
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    • 2012
  • In this investigation, flow analysis with single phase has been performed for a centrifugal impeller with a design efficiency of 90%, head of 20m and rotational speed of 3500 rpm at a design flow rate of 16m3. The impeller was designed based on an empirical formula suggested by A.J. Stepanoff. In a case of the single phase analysis, the hydraulic efficiency and head is 88.8% and 19.4m, respectively, which showed a good agreement with the values designed. The flow analysis with two phases was carried out under the various NPSH, at whose 8.79m the cavitation on the suction side of the blade was observed. The required NPSH of the designed impeller is approximately 6.5m and above this value, the designed centrifugal pump impeller needs to be operated under inlet pressure condition.

The Study on the Development of Ozone Water Diffusion Device by Ozonated Olive Oil Mix Ratio that will Increase (올리브 오일의 오존화 혼합비율을 높여주는 오존수 확산장치개발에 관한 연구)

  • Kim, Duck-Sool
    • Journal of the Korean Applied Science and Technology
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    • v.31 no.4
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    • pp.688-693
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    • 2014
  • This study is to increase the utilization of the ozonated water generator to make it easier to take advantage of the ozone water in the world today, there will be to develop a system that operates in one motion. Furthermore, olive oil and ozone is reacted with the wish to apply to the manufacturing technology. In the case of many existing products ozone generator driven mostly non-ozone system. In the case of ozone, but handwriting is implied general way pressure ozone gas leakage risks of suction force to the pump, it is the case of the challenge by using the injector, and limit the generation of ozone and ozone inhalation according to whether the water inlet leakage of existing products risk due to minimized. Despite the disadvantages of the injector system was found the effectiveness of the ozonated water production unit injector system used in this study to maintain the microbiological disinfection performance.

A Study on Propulsion Performance of Underwater Ram-Jet with Optimized Nozzle Configuration (최적 노즐형상을 갖는 수중램제트의 추진성능에 관한 연구)

  • Kang, H.K.;Kim, Y.T.;Lee, Y.H.
    • Journal of the Society of Naval Architects of Korea
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    • v.34 no.4
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    • pp.42-52
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    • 1997
  • The basic principle of underwater ram-jet as a unique marine propulsion concept showing vary high cruise speed range(e. g. 80-100 knots) is the thrust production by the transfer of the potential energy of compressed gas to the operating liquid through kinetic mixing process. This paper is aimed to investigate the propulsive efficiency of the nozzle flow in underwater ram-jet at the speed of 80 knots for the buried type vessel. The basic assumption of the theoretical analysis is that mixture of water and air can be treated as incompressible gas. For an optimized nozzle configuration obtained from the performance analysis, preliminary data for performance evaluation are obtained and effects of nozzle inner wall friction, ambient temperature, ambient pressure, water density, gas velocity, bubble radius, flow velocity, diffuser area ratio, mass flow ratio and water velocity gradient are investigated.

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