• 제목/요약/키워드: Adiabatic Line

검색결과 34건 처리시간 0.023초

단열회로를 이용한 8-b${\times}$8-b 파이프라인 승산기와 개선된 전원클럭 발생기의 연구 (A Study of an 8-b${\times}$8-b Adiabatic Pipelined Multiplier with Simplified Supply Clock Generator)

  • 문용
    • 대한전자공학회논문지SD
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    • 제38권4호
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    • pp.285-291
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    • 2001
  • 단열회로를 이용한 8-b×8-b 파이프라인 승산기와 4가지 위상을 가지는 전원클럭을 공급하기 위한 개선 된 구조의 전원클럭 발생기를 설계하였다. 전원클럭 신호선의 전하는 복원되어 에너지 소모를 줄인다. 단열회로는 ECRL 형태를 기본으로 하였으며 0.6㎛ CMOS 공정을 사용하여 설계하였다. 개선된 전원클럭 발생기는 기존회로보다 4∼11% 정도 효율이 높았다. 모의실험결과 제안하는 단열회로 승산기는 CMOS 승산기보다 2.6∼3.5배 정도의 에너지를 감소시켰다.

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증발 지연 구간을 포함한 비단열 모세관에서의 냉매 유동 특성 예측을 위한 시뮬레이션 (A Simulation for predicting the Refrigerant Flow Characteristics Including Metastable Region in Non-Adiabatic Capillary Tubes)

  • 손기동;박상구;정지환;김윤수
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 하계학술발표대회 논문집
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    • pp.263-270
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    • 2008
  • The capillary tube/suction line heat exchanger (SLHX) is widely used in small refrigeration systems. The refrigerant flowing in the SLHX experiences frictional and accelerational head losses, flashing, and heat transfer simultaneously. The simulation of refrigerant flow through SLHX is important since this will help engineers analyze and optimize the SLHX incorporated in a refrigeration system. The present SLHX model is based on conservation equations of mass, momentum and energy. Also a meta-stable model is included. All these equations are solved simultaneously. In this paper, HFC-134a refrigerant flow through a non-adiabatic capillary tube is simulated. The simulation results are discussed but not validated against experimental measurements yet.

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NASA Rotor 37 익형의 스윕각 최적화 (Optimization of Blade Sweep of NASA Rotor 37)

  • 장춘만;리핑;김광용
    • 대한기계학회논문집B
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    • 제30권7호
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    • pp.622-629
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    • 2006
  • The shape optimization of blade sweep in a transonic axial compressor rotor of NASA Rotor 37 has been performed using response surface method and the three-dimensional Wavier-Stokes analysis. Two shape variables of the rotor blade, which are used to define the rotor sweep, are introduced to increase the adiabatic efficiency of the compressor. Throughout the optimization, optimal shape having a backward sweep is obtained. Adiabatic efficiency, which is the objective function of the present optimization, is successfully increased. Separation line due to the interference between a shock and surface boundary layer on the blade suction surface is moved downstream for the optimized blade compared to the reference one. The increase in adiabatic efficiency for the optimized blade is caused by suppression of the separation due to a shock on the blade suction surface.

비단열 모세관 접합방법이 증기압축식 냉동사이클 성능에 미치는 영향 해석 (Analysis of Vapor Compression Refrigeration Cycle Performance Depending on Different Joining Method of Non-adiabatic Capillary Tube)

  • 이대용;박상구;김현정;정지환
    • Journal of Advanced Marine Engineering and Technology
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    • 제33권8호
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    • pp.1144-1151
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    • 2009
  • 냉동기는 비단열모세관을 채택하여 사용함으로써 사이클의 효율을 향상시킬 수 있다. 비단열모세관은 모세관과 흡입관을 접합함으로써 둘 사이에 열전달이 일어날 수 있도록 한 장치로서 SLHX 라고 부른다. 두 관을 접합하는 방법은 다양하며 이는 사이클의 성능에 영향을 미칠 수 있다. 본 연구에서는 가장 널리 사용되는 두 가지 접합방법이 냉동사이클에 미치는 영향을 해석하였다. 실험결과 용접형 SLHX의 열저항이 테이프형 SLHX의 열저항 보다 크게 작은 것으로 나타났다. 이를 이용한 사이클해석 결과 용접형 SLHX는 COP 와 냉동능력을 5.09%와 14.77% 향상시키고 테이프형 SLHX는 각각 5.05%와 14.75% 향상시켜 둘 사이의 차이는 매우 작은 것으로 나타났다.

Application of Surrogate Modeling to Design of A Compressor Blade to Optimize Stacking and Thickness

  • Samad, Abdus;Kim, Kwang-Yong
    • International Journal of Fluid Machinery and Systems
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    • 제2권1호
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    • pp.1-12
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    • 2009
  • Surrogate modeling is applied to a compressor blade shape optimization to modify its stacking line and thickness to enhance adiabatic efficiency and total pressure ratio. Six design variables are defined by parametric curves and three objectives; efficiency, total pressure and a combined objective of efficiency and total pressure are considered to enhance the performance of compressor blade. Latin hypercube sampling of design of experiments is used to generate 55 designs within design space constituted by the lower and upper limits of variables. Optimum designs are found by formulating a PRESS (predicted error sum of squares) based averaging (PBA) surrogate model with the help of a gradient based optimization algorithm. The optimum designs using the current variables show that, to optimize the performance of turbomachinery blade, the adiabatic efficiency objective is improved substantially while total pressure ratio objective is increased a very small amount. The multi-objective optimization shows that the efficiency can be increased with the less compensation of total pressure reduction or both objectives can be increased simultaneously.

최적화 방법에 따른 축류압축기의 효율평가 (Evaluation of Efficiency by Applying Different Optimization Method for Axial Compressor)

  • 장춘만;;김광용
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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    • pp.543-544
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    • 2006
  • Shape optimization of a transonic axial compressor rotor operating at the design flow condition has been performed using three-dimensional Navier-Stokes analysis and three different surrogate models: i.e.., Response Surface Method(RSM), Kriging Method, and Radial Basis Function(RBF). Three design variables of blade sweep, lean and skew are introduced to optimize the three-dimensional stacking line of the rotor blade. The object function of the shape optimization is selected as an adiabatic efficiency. Throughout the shape optimization of the rotor blade, the adiabatic efficiency is increased for the three different surrogate models. Detailed flow characteristics at the optimal blade shape obtained by different optimization method are drawn and discussed.

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비단열 모세관의 형상 변경에 따른 소형 냉동 사이클 성능 해석 (Simulation of the small Refrigeration Cycle as shape change of the Non-Adiabatic Capillary Tube)

  • 남기원;이대용;박상구;정지환;김윤수
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2009년도 하계학술발표대회 논문집
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    • pp.550-555
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    • 2009
  • The present simulation focuses on the effect of the shape of capillary tube-suction line heat exchangers(SLHX), The results in the three cases of the SLHX types show that both of the location and length of heat exchange section influence the coefficient of performance(COP) and cooling capacity. Simulation shows the COP may be improved by 4.6% and the cooling capacity may be improved by 13.6% in the Lateral type.

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알루미늄 용탕 보온용기의 단열재 적층구조 변경을 통한 보온성 향상 (Thermal Insulation Improvement by Laminated Adiabatic Structure Change in Holding Furnace with Molten Aluminum Alloy)

  • 황준선;강충길
    • 한국주조공학회지
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    • 제31권6호
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    • pp.336-341
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    • 2011
  • Recently, aluminium usage in the automobile industry has been increased cause of its lightweight. The aluminium has a melting-solidification process in producing line and another melting process was needed in manufacturing process. Two times of melting process for making ingot and casting not only makes the loss of time and money but contaminates the air with Sox, Nox. For this reason, the holding furnace with laminated adiabatic material was developed. This holding furnace can deliver the molten aluminium directly to the industry needing molten aluminium. Recent holding furnace has above $15^{\circ}C/h$ of cooling rate and that causes solidification of molten aluminium. The ANSYS software was used to analysis the heat transfer. The adiabatic materials were laminated with optimized arrangement and holding furnace shape was changed with optimized modelling by ANSYS analysis for reducing the cooling rate of molten aluminium in holding furnace.

초저전력 프로세서용 16-bit 단열 ALU의 설계 및 구현 (A Design and Implementation of 16-bit Adiabatic ALU for Micro-Power Processor)

  • 이한승;나인호;문용;이찬호
    • 대한전자공학회논문지SD
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    • 제41권3호
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    • pp.101-108
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    • 2004
  • 단열회로를 이용하여 16-bit ALU와 단열회로에 4가지 위상을 가지는 전원클럭을 공급하기 위한 전원클럭 발생기를 설계하였다. 4개의 전원클럭 신호선의 전하는 AC 형태의 전원클럭을 통해서 복원되어 에너지 소모를 줄인다. 구현에 사용한 단열회로는 ECRL(efficient charge recovery logic) 형태를 기본으로 하였으며 0.35㎛ CMOS 공정을 사용하여 설계하였고 3.3V 전원을 사용하였다. 회로설계 후 layout을 진행하였으며, layout 후 LPE(layout parasitic extraction)를 수행하여 이를 모의실험에 사용하였다. 모의실험결과 전원클럭 발생기를 포함한 단열회로를 이용한 ALU는 동일한 구조를 갖는 기존의 CMOS ALU보다 1.15~1.77배 정도의 에너지소모를 감소 시켰다.

A Study on the Optimum Mix Proportion of the Mass Concrete Designed as Massive and Deep Structure

  • Kwon Yeong-Ho;Lee Hwa-Jin
    • 콘크리트학회논문집
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    • 제17권2호
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    • pp.293-302
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    • 2005
  • This study describes data from determination of the optimum mix proportion and site application of the mass concrete placed in bottom slab and side wall having a large depth and section as main structures of LNG in-ground tank. This concrete requires low heat hydration, excellent balance between workability and consistency because concreting work of LNG in-ground tank is usually classified by under-pumping, adaptation of longer vertical and horizontal pumping line than ordinary pumping condition. For this purpose, low heat Portland cement and lime stone powder as cementitious materials are selected and design factors including unit cement and water content, water-binder ratio, fine aggregate ratio and adiabatic temperature rising are tested in the laboratory and batch plant. As experimental results, the optimum unit cement and water content are selected under $270kg/m^3$ and $l55{\~}l60 kg/m^3$ separately to control adiabatic temperature rising below $30^{\circ}C$ and to improve properties of the fresh and hardened concrete. Also, considering test results of the confined water ratio($\beta$p) and deformable coefficient(Ep), $30\%$ of lime stone powder by cement weight is selected as the optimum replacement ratio. After mix proportions of 5cases are tested and compared the adiabatic temperature rising($Q^{\infty}$, r), tensile and compressive strength, modulus of elasticity, teases satisfied with the required performances are chosen as the optimum mix design proportions of the side wall and bottom slab concrete. $Q^{\infty}$ and r are proved smaller than those of another project. Before application in the site, properties of the fresh concrete and actual mixing time by its ampere load are checked in the batch plant. Based on the results of this study, the optimum mix proportions of the massive concrete are applied successfully to the bottom slab and side wall in LNG in-ground tank.