• 한국지반환경공학회 논문집
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• 제12권9호
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• pp.71-78
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• 2011

최근 준설점토 고화처리과정에서 환경에의 부하를 고려하여 시멘트와 같은 지반 고화재를 최소화 하고자 하는 노력이 시도되고 있다. 그러나 적정한 지반 고화재의 비율이나 각 비율에 따른 물리/역학적 특성과 재료적 특성에 대한 충분한 연구가 수행되지 않아 설계에 반영되는 단계에 까지는 이르지 못하고 있는 것이 현실이다. 이에 본 연구는 준설점토의 유효한 활용과 친환경적 접근이라는 두 가지 문제를 동시에 극복하기 위하여 고화재를 최소화할 수 있는 방안과 고화재 비율에 따른 혼합토의 물리/역학적 특성 및 재료특성을 장단기적 관점에서 규명하고자 하였다. 이를 위해 본 연구에서는 먼저 지반 고화재로써 시멘트를 활용하여 혼합 지반의 역학적 성능을 충분히 발휘하는 범위에서 고화재의 투입량을 최소화할 수 있는 최적의 설계방안에 대해 알아봄과 동시에 각 고화재 투입량에 따른 혼합토의 물리/역학적 특성과 재료적 특성을 평가하여 정리하였다. 강도 측면에서는 빈배합 혼합점토는 본 연구에서 상정한 최대 양생기간인 270일 동안 지속적인 강도증가를 보이고 있었으나 혼합비가 상대적으로 높은 증가 추세가 현격하게 떨어지고 있었다. 압밀측면에서는 시멘트 혼합에 의한 의사과압밀현상이 낮은 배합비에서도 충분히 발휘된다는 점을 알 수 있었다. 본 연구를 통해 준설점토를 조기에 안정화시키고 동시에 친환경적으로 재활용할 수 있는 방안이 구체적으로 모색되었으며, 본 연구에서 수행되는 다양한 시험 및 해석적 연구 자료는 향후 관련 공법을 실제 현장에 적용할 경우에 설계를 위한 기초 설계자료로써 제공될 수 있으리라 기대된다.

• 한국감성과학회:학술대회논문집
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• 한국감성과학회 1999년도 추계학술대회 논문집
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• pp.179-184
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• 1999

To fill the emotivity in the interior design, the functional factor from the provided space, the aesthetic factor including modeling factor, and even the practical factor from the convenience and the value must be considered. To carry out an achieved design by the emotivity, it must follow the recognition of the original function which comes from the emotivity design method, and it should be applied to the design process fitting into the purpose of the space. The value of the sufficient interior by the emotivity is depended on what kind of image it gives, and how much of the satisfaction it can give to the customers. And fur more, it should not be partially lean to any of the decoration and the function of the object. That is, how faithfully it was to the use and the purpose of the interior and the emotion related to all parts which are the functional side and the decorative side mainly considered in the external form is designed by the essential part of the design.

• International Journal of Automotive Technology
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• 제8권3호
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• pp.269-274
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• 2007

A prior fundamental study was executed using a constant volume chamber (CVC) to improve the burning characteristics of lean pre-mixture by the injection of active radicals generated in the sub-chamber of the CVC. The Radical ignition (RI) technique shows remarkable progress in the burning velocity and combustible lean limit compared with the results of the spark ignition (SI) technique. The optimum design value of the sub-chamber geometry is near $0.11cm^{-1}$ for the ratio of the total area of the holes to the sub-chamber volume $(A_h/V_s)$. In this study, based on the former experimental results, the additional works have been performed to examine the effects of the geometry change in the number $(N_h)$, the total section area $(A_h)$, and diameter $(D_h)$ of the passage holes on the combustion characteristics in the CVC. Also ambient conditions such as the initial temperature and the initial pressure of the mixture were selected as experimental parameters and the effects of residual gas at the chamber on the combustion characteristics were investigated. As a result, the correlation between the passage hole number and overall passage hole area was grasped. The effects of the initial temperature were significant, but on the other hand, those of the initial pressure were weak. A more detailed analysis on the residual gas is required in the future.

• 한국자동차공학회논문집
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• 제22권2호
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• pp.156-165
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• 2014

This paper is the first investigation on the effect of flow control methods on the part load performance in a spark ignition engine. For comparison of the methods, two control devices, port throttling and masking, were applied to a conventional engine without any design change of the intake port. Steady flow evaluation shows that steady flow rates per unit opening area and swirl ratio are very low compared with the port throttling and saturated from mid-stage valve lift, however, swirl increases slightly as the lift is higher in case of 1/4 masking control. In the part load performance, the effect of simple port throttling on lean misfire limit expansion is limited and insufficient; on the other hand a masking improves the limit considerably without any port modification for increasing swirl. Also the results show that the intake flow control improves the combustion with following two mechanisms: stratification induced by the combination of the flow pattern and the fuel injection timing attribute to ignition ability and the intensified flow ensure fast burn. In addition fuel consumption reduces under the flow controls and the reduction rate is different according to the operation conditions and control methods. At the Stoichiometric and/or low speed and low load the throttling method is more advantageous; however vice versa at lean and high load condition. Finally, the throttling is more efficient for HC reduction than masking, on the other side the NOx emissions increase under the masking and decrease under the port throttling compared with conventional port scheme.

• 한국건설관리학회논문집
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• 제5권4호
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• pp.71-78
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• 2004

최근 우리나라의 건설 환경은 도심지 내 대형 건설공사가 증가하는 추세이며, 건설공사 관리 요소 중 기존 골조공사의 관리 중요성에 더하여 마감공사관리의 중요성이 부각되고 있다. 마감공사의 체계적인 관리를 위해서는 마감공사의 공정 중 자재 양중 측면, 공사기간 측면에서 많은 부분을 차지하고 있는 세대 내 가구공사의 관리체계 정립이 필수적이라 할 수 있다. 본 연구에서는 초고층 주거건축을 위한 마감공사 중 양중 측면에서 주 고려 대상이 되고 있는 가구공사의 관리체계를 정립하기 위하여, 적시생산(Just-In-Time)방식과 린건설(Lean Construction)의 개념을 도입하였다. 이를 바탕으로 가구공사의 프로세스를 분석하고 그에 따른 개선방안을 제시하였다. 이러한 분석과 개선방안의 제시는 마감공사의 원활한 흐름을 유도할 수 있으며, 또한 공사기간을 단축하고 공사비용을 절약함으로써 프로젝트의 성공에 기여할 수 있다.

• 한국가스학회지
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• 제17권5호
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• pp.8-14
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• 2013

천연가스에 수소를 첨가하는 수소-천연가스 혼합연료 (HCNG) 엔진 기술은 수소의 빠른 화염속도와 넓은 가연범위를 이용하여 출력 및 배기성능을 최적화하는 기술로서 희박연소 한계를 증가시킴으로써 열효율의 개선은 물론 유해배출물의 저감을 얻을 수 있다. 그러나 과급장치를 사용하는 희박연소 엔진의 경우 전부하 운전조건에서 희박연소 한계의 증가는 충분한 공기량을 공급할 수 있도록 과급용량의 증가가 선결되어야 구현될 수 있다. 본 연구에서는 HCNG 엔진 개발의 일환으로 과급시스템의 변경에 의한 엔진의 출력특성을 파악하고, 과급용량 증대의 적용가능성을 검토하고자 하였다. 터보차저가 과급압력의 증대 보다는 유량이 증가된 영역에서 효율이 높게 설계된 경우 농후한 혼합기 조건에서는 과급압력이 감소되더라도 제원상의 출력을 만족하며 효율적인 운전이 가능하였다.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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• pp.307-313
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• 2002

In the paper, the prototype development of a 75kW class microturbine for the distributed generation market is partly presented which has continued with the government funding. In the introduction, an overview of the development of microturbines in the world is presented. A series of development procedures are shown with design, manufacture and self-sustaining tests. During the first year, aerodynamic and structural design/analysis, mechanical design are performed for the compressor, the turbine and the combustor. A premixed lean burn combustor technology is used fur the low emission requirements. Foil air bearings and high-speed motors are employed for higher reliability. The self-sustaining conditions have been successfully achieved with the prototype manufactured engine as a preceding operation.

• 대한기계학회논문집B
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• 제32권4호
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• pp.317-326
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• 2008

The main purpose of the present study is to perform shape optimizations of transonic compressor blade in order to enhance its performance. In this study, the Latin hypercube sampling of design of experiments and the weighted average surrogate model with the help of a gradient based optimization algorithm are used within design space by the lower and upper limits of each design variable and for finding optimum designs, respectively. 3-D Reynolds-averaged Navier-Stokes solver is used to evaluate the objective functions of adiabatic efficiency and pressure ratio. Six variables from lean and airfoil thickness profile are selected as design variables. The results show that the adiabatic efficiency is enhanced by 1.43% by efficiency optimization while the pressure ratio is increased very small, and pressure ratio is increased by 0.24% by pressure ratio optimization.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회B
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• pp.2440-2443
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• 2008

This paper presents a three dimensional shape optimization procedure for a low-speed axial flow fan blade with a weighted average surrogate model. Reynolds-averaged Navier-Stokes equations with shear stress transport turbulence model are discretized by finite volume approximations. Six variables from airfoil profile and lean are selected as design variables. 3D RANS solver is used to evaluate the objective functions of total pressure efficiency. Surrogate approximation models for optimization have been employed to find the optimal design of fan blade. A search algorithm is used to find the optimal design in the design space from the constructed surrogate models for the objective function. The total pressure efficiency is increased by 0.31% with the weighted average surrogate model.

• 연구논문집
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• 통권22호
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• pp.5-19
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• 1992

An aerodynamic design technique of a centrifugal impeller is developed. The design procedure consists of a preliminary design, a three-dimensional blade surface generation, a flow analysis of impeller passage and a compatibility analysis for the designed impeller. To get a higher efficiency, the backswept impeller which has a lean angle and a parabolic blade surface is designed. In the present analysis of flow in an impeller, an inviscid quasi-three-dimensional method and a viscous three-dimensional method are used. Compatibility of the designed impeller is decided with the results of the analyses. The quasi-three-dimensional method is easy to use, but limited to a few conditions in real application for the prediction of the actual flow in the impeller. Since the viscous three-dimensional method proved to predict the real flow in the impeller relatively well, it can be used as a means for the decision of compatibility of the designed impeller.