• Title/Summary/Keyword: diffuser

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The Ejector Design and Test for 5kW MCFC System (5kW 용융탄산염 연료전지(MCFC) 이젝터 설계 및 시험)

  • Kim, Beom-Joo;Kim, Do-Hyeong;Lee, Jung-Hyun;Lee, Sung-Yoon;Kim, Jin-Yoel;Kang, Seung-Won;Lim, Hee-Chun
    • Transactions of the Korean hydrogen and new energy society
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    • v.20 no.1
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    • pp.31-37
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    • 2009
  • An ejector is a machine utilized for mixing fluid, maintaining a vacuum, and transporting fluid. The Ejector enhances system efficiency, are easily operated, have a mechnically simple structure, and do not require a power supply. Because of these advantages, the ejector has been applied to a variety of industrial fields such as refrigerators, power plants and oil plants. In this work, an ejector was used to safely recycle anode tail gas in a 5 kW Molten Carbonate Fuel Cell system at KEPRI(Korea Electric Power Research Institute). In this system, the ejector is placed at mixing point between the anode tail gas and the cathode tail gas or the fresh air. Commercial ejectors are not designed for the actual operating conditions for our fuel cell system. A new ejector was therefore designed for use beyond conventional operating limits. In this study, the entrainment ratio is measured according to the diametrical ratio of nozzle to throat in the designed ejector. This helps to define important criteria of ejectors for MCFC recycling.

The development of small water-jet propulsion for 150HP grade inboard type (150마력급 선내형 소형 워터제트 추진시스템 개발)

  • Lee, Joong-Seop;Lee, Chi-Woo
    • Journal of Advanced Marine Engineering and Technology
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    • v.38 no.3
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    • pp.246-252
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    • 2014
  • This study is on the development of 150PS inboard type of compact water jet propulsion system. The water jet is composed of intake, impeller, diffuser, reverse bucket and main shaft. Components of water jet have been manufactured through precision processing after sand casting. Development of water jet propelled engine has been finally completed by processes which are design, production and inspection on each component. The water jet performance characteristics show that 0.29 m3/s of maximum flow rate and 37 m/s of flow velocity have been secured in the ground test pool. Field test was performed by 21ft test ship that water jet propulsion equipment developed in this study was installed. As a result, the weight of hull, engine and other parts of the ship has been almost 1.2 ton and 45 km/h of maximum sailing speed has been recorded with 3700 rpm of engine in the domestic coast test.

Effects of Compound Angle, Diffuser Angle, and Hole Pitch on Film-cooling Effectiveness (막냉각 홀의 측면 방향 분사각, 확장각 및 주기가 막냉각 효율에 미치는 영향)

  • Kim, Sun-Min;Lee, Ki-Don;Kim, Kwang-Yong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.9
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    • pp.903-913
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    • 2011
  • A numerical study is carried out to analyze the steady three-dimensional turbulent flow through cylindrical and fan-shaped holes and the film cooling of these holes at low and high blowing ratios. Compressible Reynoldsaveraged Navier-Stokes equations and the energy equation are solved using a finite-volume-based solver, and a shearstress transport model is used as the turbulence closure. The effects of the compound angle, pitch to diameter ratio, and lateral expansion angle of the hole on the film-cooling effectiveness are evaluated by the film-cooling effectiveness. It is observed that the compound angle of the hole enhances the film performance for the cylindrical hole, and a small hole pitch induces interactions between the coolants from the adjacent holes, thus reducing the film-cooling performance.

An Experimental Study on Performance of Second Throat Exhaust Diffusers of Different Configuration (2차목 초음속 디퓨저의 형상 변화에 따른 성능에 관한 실험적 연구)

  • Jeon, Jun Su;Kim, Wan Chan;Yeoun, Hae In;Kim, Min Sang;Ko, Young Sung;Han, Young Min
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.38 no.4
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    • pp.279-288
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    • 2014
  • Second throat supersonic exhaust diffusers (STEDs) were designed to simulate high-altitude conditions according to the normal-shock model. Experimental studies were performed on the STEDs to investigate how performance characteristics varied with the length and diameter of the STED using high-pressure nitrogen gas. The variation in performance due to length indicated that the performance of the STED could be very slightly improved by adjusting the diffuser inlet length ($L_d$), and it could be significantly improved by optimizing the second throat length ratio ($L_{st}/D_{st}$) and the divergence length ($L_s$). The starting and vacuum chamber pressures exhibited the highest level of performance near ($A_d/A_{st}$) of the design point.

DESIGNING EXPERIENCE OF AUTOMOTIVE TURBOCHARGER IMPELLER FOR FLANK MILLING (Flank Milling 공법적용을 위한 자동차용 터보차져 임펠러의 설계체험)

  • Bang, J.C.;Shuripa, V.A.
    • Journal of computational fluids engineering
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    • v.18 no.4
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    • pp.1-8
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    • 2013
  • The performance of small-size impellers with ruled surfaces was investigated for flank milling over a wide speed range, using computational fluid dynamics analyses and gas bench tests. An impeller with a ruled surface was designed, manufactured, and tested to evaluate the effects of blade loading, the backsweep angle, and the relative velocity distribution on the compressor performance. The simulations and tests were completed using the same compressor cover with identical inlet and outlet channels to accurately compare the performance of the abovementioned impeller with a commercial impeller containing sculptured blades. Both impellers have the same number of blades, number of splitters, and shroud meridional profiles. The backsweep angles of the blades on the ruled impeller were selected to work with the same pinched diffuser as for a sculptured impeller. The inlet-to-exit relative velocity diffusion ratio and the blade loading were provided to maximize the flow rate and to minimize the surge flow rate. The design flow rate, rpm, were selected same for both impellers. Test results showed that for the compressor stage with a ruled impeller, the efficiency was increased by 0.32% with an extended surge margin without a reduction in the pressure ratio as compared to the impeller with the sculptured design. It was concluded that an increased relative velocity diffusion coupled with a large backsweep angle was an effective way to improve the compressor stage efficiency. Additionally, an appropriate blade loading distribution was important for achieving a wide operating range and higher efficiency.

Mixed-Flow Pump Impeller-Diffuser Optimization Method by Using CFX and HEEDS (CFX 와 HEEDS 를 이용한 사류펌프 임펠러-디퓨저 최적화방법)

  • Lee, Yong Kab;Park, In Hyung;Shin, Jae Hyok;Kim, Sung;Lee, Kyoung Yong;Choi, Young Seok
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.39 no.10
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    • pp.831-842
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    • 2015
  • An optimization process was developed to improve mixed-flow pump performance. The optimization process was combined with CFX (a computational fluid dynamics (CFD) code) and HEEDS (an optimization code). CFX is a widely used CFD software for turbo machinery, whereas HEEDS, which uses the SHERPA algorithm, is a newly introduced optimization code. HEEDS can use a large number of optimization variables; thus, it is possible to effectively consider interaction effects. In this paper, an impeller model, which is already optimized with design of experiments (DOE), is used as the base model. The optimization process developed in this paper shows an improved design within an acceptable timeframe.

An Analysis of the Thermal Flow Characteristics in Engine-Room and VTRU in accordance with Application of Thermoelectric Device Cooling System to Prevent Overheating of the Korean Navy Ship VRTU (해군 함정 VRTU의 과열방지를 위한 열전소자 냉각장치의 적용에 따른 기관실 및 VRTU 내부 열 유동특성 분석)

  • Jung, Young In
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.21 no.9
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    • pp.610-616
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    • 2020
  • This study conducted joint research with the Navy logistics command ship technology research institute to resolve the occurrence of naval vessel's high-temperature warning and equipment shutdown caused by VRTU overheating during summer operation and the dispatch of troops to equatorial regions. The cooling effect was checked according to the installation of a thermoelectric device cooling system, and heat flow and heat transfer characteristics inside VRTU was analyzed using Computational Fluid Dynamics. In addition, the temperature distribution inside the engine room was assessed through interpretation, and the optimal installation location to prevent VRTU overheating was identified. As a result, the average volume temperature inside the VRTU decreased by approximately 10 ℃ with the installation of the cooling system, and the fan installed in the cooling system made the heat circulation smooth, enhancing the cooling effect. The inside of the engine room showed a high-temperature distribution at the top of the engine room, and the end of the HVAC duct diffuser showed the lowest temperature distribution.

Improvement of Gas Dissolution Rate using Air Atomizing Nozzle (이류체 노즐을 이용한 가스의 용존율 향상)

  • Kim, Dong-Seog;Park, Young-Seek
    • Journal of Environmental Science International
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    • v.27 no.3
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    • pp.219-225
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    • 2018
  • This study was conducted to investigate the possibility of utilizing various types of nozzles and gas-liquid mixers to increase the dissolution rate of plasma gas containing ozone generated in a dielectric barrier plasma reactor. After selecting the air atomizing nozzle with the highest gas dissolution rate among the 13 types of test equipment, we investigated the influence of the operating factors on the air atomizing nozzle to determine the optimal plasma gas dissolution method. The gas dissolution rate was measured by a simple and indirect method, specifically, the measurement of KLa instead of direct measurement of ozone concentration, which requires a longer analysis time. The results showed that the KLa value of the simple mix of air and water was $0.372min^{-1}$, Which is 1.44 times higher than that ($0.258min^{-1}$) of gas emitted from a normal diffuser. Among the nozzles of the same type, the KLa value was highest for the nozzle having the smallest orifice diameter. Among the 13 types of devices tested, the nozzle with highest KLa value was the M22M nozzle, which is a gas-liquid spray nozzle. The relationship between water circulation flow rate and KLa value in the experimental range was linear. The air supply flow rate and KLa value showed a parabolic-type correlation, while the optimum air supply flow rate for the water circulation flow rate of 1.8 L / min is 1.38 times.

Changes in Reproductive Characteristics of Chameleon Goby Tridentiger trigonocephalus by Carbon Dioxide Exposure (이산화탄소 노출에 따른 두줄망둑(Tridentiger trigonocephalus)의 번식 특성 변화)

  • Hwang, In Joon;Choi, Sang Jun;Baek, Hea Ja
    • Korean Journal of Fisheries and Aquatic Sciences
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    • v.51 no.1
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    • pp.54-63
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    • 2018
  • We investigated the effect of $CO_2$ exposure on the reproductive process of chameleon goby Tridentiger trigonocephalus. Rearing aquaria were exposed for 90 days to $CO_2$ gas through diffuser connected with pH controller maintaining at pH 7.2 ($156.31{\pm}7.90ppm$) in low treatment, and at pH 6.5 ($274.17{\pm}6.51ppm$) in high treatment. $CO_2$ treatment had no significant effects on survival rates although the value was decreased compared to the controls. In female fish, $CO_2$ treatment had no significant effects on gonadosomatic index (GSI), hepatosomatic index (HSI) and condition factor (CF). However, high $CO_2$ treatment decreased HSI and CF in males significantly compared to the controls (P<0.05). The spawning occurrence was 6 times in the low level $CO_2$ treatment, and 4 times in the high level $CO_2$ treatment although only once in the controls. For the histological observations, there was no significant difference in $CO_2$ treatments. However, in male fish, $CO_2$ treatment delayed the formation of sperm from spermatid compared to controls. These results suggest $CO_2$ may disrupt reproductive process by delaying gametogenesis in chameleon goby and it was more sensitive in males.

A Study on the Effect of Optical Characteristic in 2 inch LCD-BLU by Negative and Positive Optical Pattern :I. Optical Analysis and Design (휴대폰용 2 인치 LCD-BLU의 광특성에 미치는 음각 및 양각 광학패턴의 영향 연구 :I. 광학 해석 및 설계)

  • Hwang C.J.;Ko Y.B.;Kim J.S.;Yoon K.H.
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2006.05a
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    • pp.75-76
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    • 2006
  • LCD-BLU (Liquid Crystal Display - Back Light Unit) is one of kernel parts of LCD unit and it consists of several optical sheets(such as prism, diffuser and protector sheets), LCP (Light Guide Plate), light source (CCFL or LED) and mold frame. The LGP of LCD-BLU is usually manufactured by forming numerous dots with $50{\sim}200{\mu}m$ in diameter on it by erosion method. But the surface of the erosion dots of LGP is very rough due to the characteristics of the erosion process during the mold fabrication, so that its light loss is high along with the dispersion of light into the surface. Accordingly, there is a limit in raising the luminance of LCD-BLU. In order to overcome the limit of current dot patterned LGP, optical pattern design with $50{\mu}m$ micro-lens was applied in the present study. Especially, the negative and positive micro-lens pattern fabricated by modified LiGA with thermal reflow process was applied to the optical design of LGP. The attention was paid to the effects of different pattern conditions to the brightness distribution of BLU with micro-lens patterned LGP. Finally, negative micro-lens patterned LGP showed superior results to the one made by positive in average luminance.

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