• 제목/요약/키워드: inlet pressure

검색결과 1,654건 처리시간 0.029초

열회수장치에 의한 열회수성능 분석 (Analysis of Heat Exchanging Performance of Heat Recovering Device Attached to Exhaust Gas Duct)

  • 서원명;윤용철;강종국
    • 생물환경조절학회지
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    • 제9권4호
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    • pp.212-222
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    • 2000
  • 본 연구는 온실 난방시스템의 연소 체임버에 부착된 연소가스 배출연통에 열회수기를 장착하여 배출가스로부터 열을 회수하는 열회수장치의 성능에 대해 실험·분석하였다. 열회수시스템은 LPG 연소 체임버와 두 개의 열회수기로 구성되어있다. 열회수기-A는 배기가스 연통에 직접 연결되어 있으며 열회수기-B는 열회수기-A에 직렬로 연결되어 있다. 회수되는 열량은 가스의 질량흐름율과 두 측점간의 엔탈피 차이로서 산정하였으며 5가지의 송풍전압별로 각 열회수기의 성능을 검토하였다. 각 열회수기의 공기튜브 다발에 공급된 공기와 튜브 다발에 가로질로 통과하는 연소가스간의 열교환, 열회수기 유·출입부간의 압력감소, 열회수기의 총열회수성능 등으로 온실의 연통을 통해 낭비되는 열을 회수하여 연료 절감 효과를 얻을 수 있는 최적의 열회수장치 설계용 기초자료 확보에 본 연구의 목적이 있다.

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수동형 감요수조의 하부덕트 유동에 관한 기초연구 (A Fundamental Study on Lower Duct Flow of passive anti-rolling tanks System)

  • 이철재;임정선;정한식;정효민
    • 해양환경안전학회:학술대회논문집
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    • 해양환경안전학회 2006년도 추계학술발표회
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    • pp.265-269
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    • 2006
  • 파랑에 의한 선박의 횡동요를 방지하는 감요장치는 크게 수동식과 능동식 으로 분류할 수 있으며 수동형 감요수조는 선박에서 가장 널리 사용되고 있다. 이 연구에서는 감요장치의 하부덕트유동에 관한 기초연구로서 덕트의 제어 댐퍼와 유입부의 유통에 대해 입자영상 유속측정장치를 이용하여 속도벡터분포에 관한 정량적인 데이터를 확보하였다. 그 결과 실험관 벽면에서 측정 된 압력의 분포는 디스크가 전개 상태인 0 도에서 45도까지는 입구 압력은 일정한 상태로 거의 변화하지 않았으나 약 60도 이상에서부터 압력 상승과 점차 급격한 변동현상이 나타났다.

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Simultaneous Biofiltration of H2S, NH3 and Toluene using an Inorganic/Polymeric Composite Carrier

  • Park, Byoung-Gi;Shin, Won-Sik;Chung, Jong-Shik
    • Environmental Engineering Research
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    • 제13권1호
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    • pp.19-27
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    • 2008
  • Simultaneous removal of ternary gases of $NH_3$, $H_2S$ and toluene in a contaminated air stream was investigated over 180 days in a biofilter. A commercially available inorganic/polymeric composite chip with a large void volume (bed porosity > 0.80) was used as a microbial support. Multiple microorganisms including Nitrosomonas and Nitrobactor for nitrogen removal, Thiobacillus thioparus (ATCC 23645) for $H_2S$ removal and Pseudomonas aeruginosa (ATCC 15692), Pseudomonas putida (ATCC 17484) and Pseudomonas putida (ATCC 23973) for toluene removal were used simultaneously. The empty bed residence time (EBRT) ranged from 60 - 120 seconds and the inlet feed concentration was $0.0325\;g/m^3-0.0651\;g/m^3$ for $NH_3$, $0.0636\;g/m^3-0.141\;g/m^3$ for $H_2S$, and $0.0918\;g/m^3-0.383\;g/m^3$ for toluene, respectively. The observed removal efficiency was 2% - 98% for $NH_3$, 2% - 100% for $H^2S$, and 2% - 80% for toluene, respectively. Maximum elimination capacity was about $2.7\;g/m^3$/hr for $NH_3$, > $6.4\;g/m^3$/hr for $H_2S$ and $4.0\;g/m^3$/hr for toluene, respectively. The inorganic/polymeric composite carrier required 40 - 80 days of wetting time for biofilm formation due to the hydrophobic nature of the carrier. Once the surface of the carrier was completely wetted, the microbial activity became stable. During the long-term operation, pressure drop was negligible because the void volume of the carrier was two times higher than the conventional packing materials.

Kalina 사이클의 효율 향상 방안 및 성능 비교 (Improvement of Efficiency of Kalina Cycle and Performance Comparison)

  • 윤정인;손창효;최광환;손창민;설성훈;이호생;김현주
    • 한국태양에너지학회 논문집
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    • 제35권5호
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    • pp.11-19
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    • 2015
  • In this paper, EP-Kalina cycle applying liquid-vapor ejector and motive pump is newly proposed. In this EP-Kalina cycle, the liquid-vapor ejector is used to increase pressure difference between inlet and outlet of the turbine. Also the motive pump enhances the performance of liquid-vapor ejector, resulting in increase of system efficiency of OTEC cycles. The comparison cycles in this study are basic, Kalina, EKalina and EP-Kalina ones. The pump work, net power, APRe, APRc, TPP and system efficiency of each cycle are compared. In case of net power, EP-Kalina cycle is lowest among the cycles due to the application of the motive pump. But, the net power difference of cycles seems to be minor since the pump work of cycles is merely about 1kW, compared to turbine gross power of 20kW. The system efficiency of EP-Kalina cycle shows 3.22%, relatively 44% higher than that of basic OTEC cycle. Therefore, the system efficiency is increased by applying the liquid-vapor ejector and the motive pump. Additional performance analysis is necessary to optimize the proposed EP-Kalina cycle.

피스톤 오일 냉각 유로의 성능 검증을 위한 리그 시험기 개발 (Rig Tester Development for the Performance Validation of a Piston Oil Cooling Gallery)

  • 전상명;이정근;주대헌;류관호;하대홍
    • Tribology and Lubricants
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    • 제25권6호
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    • pp.387-398
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    • 2009
  • The operation condition of recently designed pistons for high power and high speed diesel engine become more severe due to the increment of combustion pressure and temperature. So, in order to overcome high temperature, the application of the mono-metal cast aluminum alloy piston featuring an enclosed cast-in open cooling gallery has increased. In this research, it is developed a PCJ (piston cooling jet) rig tester, described the test procedure and validated the performance of sample piston cooling gallery design. Then the test rig will be used for developing the design technology of piston cooling gallery. The test rig is composed with oil reservoir and pumping system, oil jet system, piston fixing and moving system, collecting oil measuring system, and data measuring and recording system. It will be measured collecting efficiencies under conditions of a few piston positions, oil jet pressures and oil viscosities for a piston cooling gallery. Furthermore, the PCJ rig tester will be used for the optimum design of the oil cooling gallery which being applied to increase the cooling efficiency of pistons in diesel engines satisfying the EURO V emission regulation and the more.

하절기 기화냉각장치 설치에 따른 가스터빈 성능변화 (Performance Change of Gas Turbine with a Evaporation Cooling System in Summer Season)

  • 정현조;유호선;문승재
    • 플랜트 저널
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    • 제13권1호
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    • pp.37-43
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    • 2017
  • 본 연구는 하절기 가스터빈 압축기 입구에 설치된 기화냉각장치로 인하여 저하된 공기온도가 가스터빈 성능에 어떠한 변화를 미치는지에 대하여 해석하였다. 연구 대상은 인천화력본부 가스터빈 3호기이며, 기종은 Siemens SGT6-4000F(V 84.3A)이다. 기화냉각장치 설치 전후를 비교하기 위하여 특설계측기를 설치하였으며, 2015년 8월 3일에서 14일까지 11시부터 15시 사이에 대기온도 $29{\pm}1^{\circ}C$ 조건에서 설치 전후 각각 5회씩 총 10회에 걸쳐 정밀성능시험을 시행하고 각각의 평균값을 적용하였다. 시험 결과, 가스터빈 압축기 입구 공기온도 $4.12^{\circ}C$ 저하로 공기 밀도가 증가되어 압축기 압력비는 0.27 증가, 압축기 효율은 0.29 %p 상승, 가스터빈 엔탈피강하 효율은 0.31 %p 증가하였고, 가스터빈 효율은 0.44%p, 출력은 4,489 kW가 증대되는 효과를 얻을 수 있었으며, 습도 및 유동저항 증가에 따른 영향은 미미하였다.

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파사드 일체형 자연순환 태양열온수기 유동해석 (Flow Analysis of Facade Integrated Solar Water Heater with Natural Circulation)

  • 백남춘;이왕제;임희원;신우철
    • KIEAE Journal
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    • 제16권6호
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    • pp.167-172
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    • 2016
  • Purpose: The solar water heater with natural circulation has been used for several decades in the world as it is automatically operated without a pump and controller and is easy to maintain and repair. After the subsidy was offered from 2012, the solar water heater with natural circulation is becoming increasingly popular in Korea. Recently, the development of a wall-integrated solar water heater, which improves the applicability of buildings and prevents the overheating in the summer, is being developed. On the other hand, the design and performance evaluation data of solar water heaters are very inadequate, and analysis of heat and flow is required to develop a new type of solar water heater. Method: Therefore, in this study, we proposed a new simplified system analysis model that reflects heat and pressure loss from the test results of KS B ISO 9806-1 (Solar collector test method), assuming that the collector is a simple pipe system, the validity of which was verified through experiments. Result: As a result, first, the RMSE of the system circulation flow rate and the average temperature of the inlet and outlet of the collector according to the experimental results and the simulation are 0.05563 and 0.88530, respectively, which are very consistent. Secondly, the mass flow rate is increased linearly with the increase of the solar radiation, and the mass flow rate is 0.0104 ~ 0.0180kg/s in the range of $200{\sim}380W/m^2$ of solar irradiance. Compared with the test flow rate 0.0764kg / s of the test collector, it showed a level of less than 20%.

Rotordynamic Characteristics of Floating Ring Seals in Rocket Turbopumps

  • Tokunaga, Yuichiro;Inoue, Hideyuki;Hiromatsu, Jun;Iguchi, Tetsuya;Kuroki, Yasuhiro;Uchiumi, Masaharu
    • International Journal of Fluid Machinery and Systems
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    • 제9권3호
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    • pp.194-204
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    • 2016
  • Floating ring seals offer an opportunity to reduce leakage flows significantly in rotating machinery. Accordingly, they have been applied successfully to rotating machinery within the last several decades. For rocket turbopump applications, fundamental behavior and design philosophy have been revealed. However, further work is needed to explore the rotordynamic characteristics associated with rotor vibrations. In this study, rotordynamic forces for floating ring seals under rotor's whirling motions are calculated to elucidate rotordynamic characteristics. Comparisons between numerical simulation results and experiments demonstrated in our previous report are carried out. The three-dimensional Reynolds equation is solved by the finite-difference method to calculate hydrodynamic pressure distributions and the leakage flow rate. The entrance loss at the upstream inlet of the seal ring is calculated to estimate the Lomakin effect. The friction force at the secondary seal surface is also considered. Numerical simulation results showed that the rotordynamic forces of this type of floating ring seal are determined mainly by the friction force at the secondary seal surface. The seal ring is positioned almost concentrically relative to the rotor by the Lomakin effect. Numerical simulations agree quite well with the experimental results.

수직형 소형풍력터빈의 비정상 익력 평가 (Analysis of Unsteady Blade Forces in a Vertical-axis Small Wind Turbine)

  • 이상문;김철규;전석윤;알사지드;장춘만
    • 한국수소및신에너지학회논문집
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    • 제29권2호
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    • pp.197-204
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    • 2018
  • In the present study, unsteady flow analysis has been conducted to investigate the blade forces and wake flow around a hybrid street-lamp having a vertical-axis small wind turbine and a photovoltaic panel. Uniform velocities of 3, 5 and 7 m/s are applied as inlet boundary condition. Relatively large vortex shedding is formed at the wake region of the photovoltaic panel, which affects the increase of blade torque and wake flow downstream of the wind turbine. It is found that blade force has a good relation to the variation of the angle of attack with the rotation of turbine blades. Variations in the torque on the turbine blade over time create a cyclic fluctuation, which can be a source of turbine vibration and noise. Unsteady fluctuation of blade forces is also analyzed to understand the nature of the vibration of a small wind turbine over time. The detailed flow field inside the turbine blades is analyzed and discussed.

Flow Evaluation and Hemolysis Analysis of BVAD Centrifugal Blood Pump by Computational Fluids Dynamics

  • Bumrungpetch, Jeerasit;Tan, Andy Chit;Liu, Shu-Hong;Luo, Xian-Wu;Wu, Qing-Yu;Yuan, Jian-Ping;Zhang, Ming-Kui
    • International Journal of Fluid Machinery and Systems
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    • 제7권1호
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    • pp.34-41
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    • 2014
  • Computational fluid dynamics (CFD) and particle image velocimetry (PIV) are commonly used techniques to evaluate the flow characteristics in the development stage of blood pumps. CFD technique allows rapid change to pump parameters to optimize the pump performance without having to construct a costly prototype model. These techniques are used in the construction of a bi-ventricular assist device (BVAD) which combines the functions of LVAD and RVAD in a compact unit. The BVAD construction consists of two separate chambers with similar impellers, volutes, inlet and output sections. To achieve the required flow characteristics of an average flow rate of 5 l/min and different pressure heads (left - 100mmHg and right - 20mmHg), the impellers were set at different rotating speeds. From the CFD results, a six-blade impeller design was adopted for the development of the BVAD. It was also observed that the fluid can flow smoothly through the pump with minimum shear stress and area of stagnation which are related to haemolysis and thrombosis. Based on the compatible Reynolds number the flow through the model was calculated for the left and the right pumps. As it was not possible to have both the left and right chambers in the experimental model, the left and right pumps were tested separately.