• Title/Summary/Keyword: 가압 시스템

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The Study of De-orbit Time Prediction Using Temperature Change of Geostationary Satellite Propellant System (정지궤도위성 추진시스템의 온도변화를 이용한 위성폐기시점 추정연구)

  • Park Eung Sik;Park Bong Kyu;Han Cho Young;Kim Yong Min
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.5-10
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    • 2005
  • The geostationary satellite propulsion system has thermistors which can measure liquid propellant temperature at tanks, pipes and etc. In the satellite propulsion system with several tanks, the propellant in the tanks is moved by temperature change and this temperature pattern is constant. In this paper, the temperature change pattern of KOREASAT 1 propulsion system is compared and the prediction study of pressurant inflow using temperature change of geostationary satellite propulsion system is described.

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Feeding System Design/Analysis Using Test Data Correlation Method (Test data 보정기법을 활용한 추진기관 공급계 설계/해석)

  • Cho, Nam-Kyung;Jeong, Yong-Gahp;Han, Sang-Yeop;Kim, Young-Mog
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.127-131
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    • 2006
  • An optimization algorithm is applied to a calibration task. In this paper, test data correlation, a reverse analysis method, is presented. With this method, flow rate and heat transfer rate, which are difficult to be measured are estimated using measured pressure and temperature data for helium pressurization system of launch vehicle.

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Parametric Design Analysis of a Pressurized Hybrid System Combining Gas Turbine and Solid Oxide Fuel Cell (가스터빈과 고체산화물 연료전지를 결합한 가압형 하이브리드 시스템의 설계변수 해석)

  • Jeong, Young-Hyun;Kim, Tong-Seop;Kim, Jae-Hwan
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.26 no.11
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    • pp.1605-1612
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    • 2002
  • Thermodynamic performance analysis has been carried out for a hybrid electric power generation system combining a gas turbine and a solid oxide fuel cell and operating at over-atmospheric pressure. Performance characteristics with respect to main design parameters such as maximum temperature and pressure ratio are examined in detail. Effects of other important design parameters are investigated including fuel cell internal parameters such as fuel utilization factor, steam/carbon ratio and current density, and system parameters such as recuperator efficiency and compressor inlet temperature.

Development of Alarm System Using Fault Tree Analysis for Pumping Station and Reservoir of Waterworks (Fault Tree 분석에 의한 상수도 가압장과 배수지의 경보시스템 구축)

  • Ahn, Yong-Po;Song, Moo-Geun;Lee, Dong-Ik
    • Journal of Korean Society of Water and Wastewater
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    • v.25 no.6
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    • pp.847-859
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    • 2011
  • This paper presents an alarm system for the integrated monitoring and control station of waterworks in Daegu City. An alarm system informs the operator or other responsible individuals about the abnormality in the process so that an appropriate action can be taken. In practice, operators receive far more false and nuisance alarms than valid and useful alarms. Too many false and nuisance alarms can distract the operator from operating the plant, and thus critical alarms may be ignored. This problem can lead to the point that the operator no longer trusts the alarms or even shuts down the whole monitoring system. This paper proposes an efficient method to reduce false and nuisance alarms by prioritizing every fault using the Fault Tree Analysis (FTA) technique. The effectiveness of the proposed method is evaluated with a set of computer simulation under various faulty conditions.

The Study of Pressurant Inflow Prediction Using Temperature Change of Geostationary Satellite Propellant System (정지궤도 인공위성 추진시스템의 온도변화를 통한 배관내 가압제 유입 예측기법 연구)

  • Park Eung Sik;Jun Hyoung Yoll;Park Bong Kyu;Han Cho Young;Choi Seong Bong;Kim Yong Min
    • 한국전산유체공학회:학술대회논문집
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    • 2005.04a
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    • pp.96-99
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    • 2005
  • The geostationary satellite propulsion system has thermistors which can measure liquid propellant temperature at tanks, pipes and etc. In the satellite propulsion system with several tanks, the propellant in the tanks is moved by temperature change and this temperature pattern is constant. In this paper, the temperature change pattern of KOREASAT 1 propulsion system is compared and the prediction study of pressurant inflow using temperature change of geostationary satellite propulsion system is described.

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Effect of Gas Bypass at Turbine Inlet on Design of a Pressurized Solid Oxide Fuel Cell / Gas Turbine Hybrid System (가압형 고체산화물 연료전지 / 가스터빈 하이브리드 시스템 설계에서 터빈입구 바이패스의 효과)

  • Park, S.K.;Sohn, J.L.;Kim, T.S.
    • The KSFM Journal of Fluid Machinery
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    • v.11 no.1
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    • pp.33-39
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    • 2008
  • Hybrid power generation systems combining a solid oxide fuel cell and a gas turbine is promising due to their high efficiency. In the pressurized hybrid system, the operating condition of the gas turbine may play a critical role in designing the hybrid system. In particular, prevention of surge of the compressor can be a critical issue. The existence of fuel cell between the compressor and the turbine may cause an additional pressure loss and thus compressor operating points tend to approach the surge if the original turbine inlet temperature is pursued. In this study, bypassing some of the turbine inlet gas directly to the turbine exit side is simulated. Its effects on suppressing the surge problem and change in performance characteristics are discussed.

An Analysis of the Water Supply System with Pressurizing Tank (가압탱크를 이용한 급수시스템의 해석 및 최적화 연구)

  • Lee, T.W.;Kim, T.H.;Choi, D.H.;Kim, S.D.;Kim, J.P.
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.6 no.2
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    • pp.93-102
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    • 1994
  • It is the goal of this study to provide the essential data for design and operation of optimum water supply system. Experimental and theoretical analyses have been conducted for various parameters, for example, volume and air percent of pressurizing tank, pump speed and pressure range inside tank, etc. Pressure inside tank with time, flow rate, energy consumption rate and pump operation time have been obtained for design and operating parameters to optimize the components and to establish the operating method of system, and therefore to contribute to the development of technology from a point of view of the improvement of quality, the enhancement of system efficiency and the reduction of construction cost.

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Field Experiments on Features of Airflow through Open Door in Pressure Differential System (급기가압 제연시스템의 피난문 개방시 방연풍속 형성특성에 대한 현장실험)

  • Kim, Jung-Yup;Rie, Dong-Ho;Kim, Ha-Young
    • Proceedings of the SAREK Conference
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    • 2008.06a
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    • pp.463-467
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    • 2008
  • The fact that the major cases of life casualties are from smoke in the fire accidents and the expected steep increase of skyscrapers, huge spaces, multiplexes and huge scaled underground spaces demand establishment of efficient smoke countermeasure. The field experiments on pressure differential systems for smoke management in two high buildings of 20 stories and 21 stories are carried out to evaluate the features of airflow through open door between accommodation and lobby. The procedures and results of experiments are presented.

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A Practical Design of Pressurized Solid Oxide Fuel Cell/Gas Turbine Hybrid Systems (가압형 고체산화물 연료전지/가스터빈 하이브리드 시스템의 현실적 설계)

  • Oh, Kyong-Sok;Park, Sung-Ku;Kim, Tong-Seop
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.31 no.2 s.257
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    • pp.125-131
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    • 2007
  • This paper presents guideline for a practical design of the hybrid system combining a pressurized solid oxide fuel cell and a gas turbine. Design of the hybrid system based on a virtually designed gas turbine was simulated using models for off-design operation of the gas turbine. Two system configurations, with different method for supplying reforming steam, are considered and their design characteristics are compared. A higher design cell temperature provides better system performance. However, there exists a maximum allowable design cell temperature because the operating point of the compressor approaches the surge point with increasing fuel cell temperature. Increased pressure loss at the fuel cell moves the compressor operating point toward the surge point and reduces system performance.

Experiments on Performance of Fan used in Pressure Differential System for Smoke Management (급기가압 제연시스템의 송풍기에 대한 실규모 성능평가 실험)

  • Kim, Jung-Yup
    • Proceedings of the SAREK Conference
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    • 2008.11a
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    • pp.458-462
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    • 2008
  • The fact that the major cases of life casualties are from smoke in the fire accidents and the expected steep increase of skyscrapers, huge spaces, multiplexes and huge scaled underground spaces demand establishment of efficient smoke countermeasure. The core technology for development of smoke management system is analysis tool of fan used in pressure differential system. The experiments on performance of sirroco-typed fan are carried out to evaluate the features of fan and present the experimental data for numerical analysis.

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