• Korean Chemical Engineering Research
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• 제50권6호
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• pp.960-968
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• 2012

본 연구에서는 에틸렌 옥사이드가 부가된 3 종류의 아민 옥사이드 양쪽성 계면활성제에 대하여 임계 마이셀 농도, 표면장력, 계면장력, 접촉각, 점도, 기포 안정성 등을 측정하였다. 또한 계면활성제 수용액에 대한 제타전위 측정과 QCM (quartz crystal microbalance) 실험을 통하여 양쪽성 계면활성제가 양이온 계면활성제에서 비이온 계면활성제로 작용이 전환되는 등전점을 결정하였다. 제타전위 측정을 통하여 결정한 양쪽성 계면활성제의 등전점은 QCM 실험을 통하여 결정한 등전점 결과가 거의 일치하였으며, 표면 마찰 시험기를 사용하여 측정한 유연력 측정 결과와도 일치하는 경향을 나타내었다. 본 연구에서 사용한 3종류 계면활성제 모두, pH가 중성인 조건에서 섬유 유연 효과가 큰 것을 확인하였는데, 이러한 결과는 등전점 보다 낮은 산성 혹은 중성 조건에서 양이온 계면활성제로 작용함으로써 세탁 후 린스 과정에서 유연제로서 효과적으로 작용할 수 있음을 의미한다.

• Korean Chemical Engineering Research
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• 제50권3호
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• pp.455-463
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• 2012

본 연구에서는 에틸렌 옥사이드와 프로필렌 옥사이드가 부가된 DEP-OSA82-AO 양쪽성 계면활성제에 대하여 계면활성제의 기본적인 물성(임계 마이셀 농도, 표면장력, 계면장력, 접촉각, 점도, 기포 안정성 등)을 측정하였다. 또한 계면활성제 수용액에 대한 제타전위 측정과 QCM (quartz crystal microbalance) 실험을 통하여 양쪽성 계면활성제가 양이온 계면활성제에서 비이온 계면활성제로 작용이 전환되는 등전점을 결정하였다. 제타전위 측정을 통하여 결정한 양쪽성 계면활성제의 등전점은 QCM 실험을 통하여 결정한 등전점 결과가 거의 일치하였으며, 표면 마찰 시험기를 사용하여 측정한 유연력 측정 결과와도 일치하는 경향을 나타내었다. 특히 DEP32-OSA82-AO와 DEP34-OSA82-AO 계면활성제의 경우, 산성 조건 혹은 중성 조건일 경우가 알칼리성 조건에 비하여 섬유 유연 효과가 큰 것을 확인하였는데, 이러한 결과는 등전점 보다 낮은 pH 산성 혹은 중성 조건에서 DEP32-OSA82-AO와 DEP34-OSA82-AO 계면활성제가 모두 양이온 계면활성제로 작용함으로써 세탁 후 린스 과정에서 유연제로서 효과적으로 작용할 수 있음을 의미한다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.671-679
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• 2008

The effect of Pre-cooled Turbojet Engine installation and nozzle exhaust jet on Hypersonic Turbojet EXperimental aircraft(HYTEX aircraft) were investigated by three-dimensional numerical analyses to obtain aerodynamic characteristics of the aircraft during its in-flight condition. First, simulations of wind tunnel experiment using small scale model of the aircraft with and without the rectangular duct reproducing engine was performed at M=5.1 condition in order to validate the calculation code. Here, good agreements with experimental data were obtained regarding centerline wall pressures on the aircraft and aerodynamic coefficients of forces and moments acting on the aircraft. Next, full scale integrated analysis of the aircraft and the engine were conducted for flight Mach numbers of M=5.0, 4.0, 3.5, 3.0, and 2.0. Increasing the angle of attack $\alpha$ of the aircraft in M=5.0 flight increased the mass flow rate of the air captured at the intake due to pre-compression effect of the nose shockwave, also increasing the thrust obtained at the engine plug nozzle. Sufficient thrust for acceleration were obtained at $\alpha=3$ and 5 degrees. Increase of flight Mach number at $\alpha=0$ degrees resulted in decrease of mass flow rate captured at the engine intake, and thus decrease in thrust at the nozzle. The thrust was sufficient for acceleration at M=3.5 and lower cases. Lift force on the aircraft was increased by the integration of engine on the aircraft for all varying angles of attack or flight Mach numbers. However, the slope of lift increase when increasing flight Mach number showed decrease as flight Mach number reach to M=5.0, due to the separation shockwave at the upper surface of the aircraft. Pitch moment of the aircraft was not affected by the installation of the engines for all angles of attack at M=5.0 condition. In low Mach number cases at $\alpha=0$ degrees, installation of the engines increased the pitch moment compared to no engine configuration. Installation of the engines increased the frictional drag on the aircraft, and its percentage to the total drag ranged between 30-50% for varying angle of attack in M=5.0 flight.

• 한국안광학회지
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• 제10권4호
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• pp.273-281
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• 2005

착용한 안경의 무게가 코의 형상에 따라 코 면을 수직으로 누르는 힘과 코의 경사면으로 분해되는 분력을 코 면의 경사도를 결정짓는 경사각 ${\Psi}$을 포함한 공식으로 유도하였다. 경사각 ${\Psi}$는 정면 및 측면에서 측정한 코의 경사각 ${\theta}$ 및 ${\Phi}$의 함수로서 구해지며 $sin{\Psi}$, $cos{\Psi}$, $cot{\Psi}$의 수지 해석 프로그램을 사용하여 안경의 코 받침이 코 면에서 미끄러지거나/미끄러지지 않는 ${\theta}$, ${\Phi}$값의 범위 및 코 면과 코 받침 사이의 마찰계수 변화에 따른 ${\theta}$, ${\Phi}$의 범위를 예측하였다. ${\theta}$ 값이 일정할 때 ${\Phi}$ 값이 증가할수록 안경이 코 받침에 의해 코 면을 누르는 압력은 증가하고 미끄럼 분력은 감소하며, ${\Phi}$값을 고정시키면 ${\theta}$값 변화에 따라 마찬가지 효과가 발생한다.

• Tribology and Lubricants
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• 제36권3호
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• pp.168-192
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• 2020

In recently designed diesel engines, the running conditions for piston-pin bearings have become severe because of the higher combustion pressure and increased temperature. Moreover, the metal removal from the bushing material has strongly reduced the ability of the antifriction material to accept asperity contacts. Therefore, it is necessary to find ways of reducing wear scar on the connecting-rod small-end bushing and piston-pin boss bearing related to the higher combustion pressure on the power cell of an engine. In this work, the position and level of material removal from the surfaces of the bushing and bearing under such severe operating conditions - for example, maximum power and torque conditions of a passenger car diesel engine - are estimated for several combinations of surface roughness. First, piston-pin rotating motion is investigated by calculating the friction coefficient at piston-pin bearings, the oil film thickness, and the frictional torques induced by hydrodynamic shear stress. Subsequently, the wear scarring on the surfaces of a connecting-rod small-end bushing and two piston-pin boss bearings related to piston-pin rotational motion is numerically calculated under the maximum power and torque operating conditions. This work is helpful to determine the reasonable surface roughness of the bushing and bearing for reducing wear volume occurring at the interface between a bearing and a shaft.

• Composites Research
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• 제29권5호
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• pp.236-242
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• 2016

본 연구에서는 유리섬유/폴리프로필렌 기반의 열가소성 복합재의 열성형 시험 평가를 위해, 성형온도에서의 인장 및 면내 전단 물성 시험을 실시하였고, 이를 비직교 구성방정식을 이용하여 정량화 하였다. 이를 통해 실험값과 잘 일치하는 고온에서의 인장 및 전단 물성값을 수식화하여 얻을 수 있었다. 열성형 시험을 위해 반구돔 시험을 실시하였고, 이형제 사용 유무 및 홀더의 무게를 달리해가며 성형품의 최종형상을 비교하였다. 그 결과 이형제를 사용하면 성형품의 대칭성이 확보되고 주름 개선 효과에 유리하다는 것을 확인하였고, 적당한 힘의 홀딩력 제어가 필수적이라는 것을 알 수 있었다. 더 나아가 비직교 구성방정식이 고려된 열성형 수치해석을 실시하여 실험 결과와 유사한 양상을 확인할 수 있었고, 홀딩력이 낮을 수록 주름이 많아지고, 마찰력이 클수록 더 많은 펀치력을 필요로 함을 확인하였다.

• 한국정밀공학회지
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• 제30권3호
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• pp.254-259
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• 2013

Ball screw system is widely used as a precision mechanical linear actuator that translates rotational motion to linear motion for its high efficiency, great stiffness and long life. Recently, according to the requirements of high accuracy and stiffness, the pre-load on the ball screw which means of remove the backlash in the ball screw is usually used. Because of the preload which means the frictional resistance between the screw and nut, becomes a dominating heat source and it generates thermal deformation of ball screw which is the reason for low accuracy of the positioning decision. There are several methods to solve the problem that includes temperature control, thermal stable design and error compensation. In the past years, researchers focused on the error compensation technique for its ability to correct ball screw error effectively rather than the capabilities of careful machine design and manufacturing. Significant amounts of researches have been done to real-time error compensation. But in this paper, we developed a series of cooling methods to get thermal equilibrium in the ball screw system. So we find the optimum cooling type for improving positioning error which caused by thermal deformation in the ball screw system.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2009년도 하계학술발표대회 논문집
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• pp.1096-1101
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• 2009

The plate heat exchanger(PHE) in heat pump has two flow streams of the refrigerant and water. The flow direction of the refrigerant, unlike that of water, can be changed by a 4-way valve depending on operating condition. Therefore the flow arrangement is a parallel flow for heating and a counter flow for cooling, respectively. In this study, the effects of the flow direction of the water on the heat transfer rate are investigated experimentally. The experiments are carried out for brazed plate heat exchangers under a parallel and counter flow conditions in evaporation and condensation. The experimental parameters in this study include the mass flux of the refrigerant 410A from 3 to $14\;kg/m^2s$ and the flow patterns for the pressure of PHE fixed at 0.97 and 2.46 MPa. The results show that both the heat transfer rate and frictional pressure drop across the PHE increase with the mass flux. The heat transfer rate of the refrigerant 410A for evaporation show great sensitivity to flow direction of the water. The heat transfer rate for evaporation with a counter flow are 5-30% higher than that with a parallel flow.

• 한국의류학회지
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• 제19권3호
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• pp.471-482
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• 1995

Using the acetate velvet and viscose velvet whose pile lengths were sheared as 1.45, 1.55, 1 65, 1.75, 1.85, 1.90mm under the condition equating the weaving process of ground fabric, the conclusions were as follows through the results of the sensory assessments estimated by women students in our university and the physical properties, H. V and T. H. V obtained by KES-F system. 1. In the sensory assessments estimated by the method of paired comparison and ranking of samples, the longer pile length was, the more the hand values of smoothness, softness, thickness, heaviness increased on the whole. 2. The H V. and T. H. V. measured by KES-F system were as follows; Kohi increased to pile length 1.85mm and then decreased a little at 1.90mm. hummer increased as pile length was longer. Fukurami increased to pile length 1.75mm and then decreased gradually as pile length was longer. Total hand value increased gradually from 1. 45mm to 1.85mm, had the top value at 1.85mm, and then decreased a little at 1.90mm. 3. In the results of summarizing $\ulcorner$the physical properties correlated closely with the H. V obtained by sensory assessments$\lrcorner$ and tithe Physical properties correlated closely with the H. V. and T. H. V obtained by KES-F systems, it showed that all the sensory properties correlated closely with compressive energy, flexural rigidity, thickness, weight and pile ratio in the former and that the physical properties correlated closely with each H V and T. H. V were different in the latter. 4. It showed that factor 1 was related to compressive energy, thickness, weight, pile ratio, factor 2 was related to recovery energy, compressive resilience, compressive index, and factor 3 was related to compressive recovery ratio in the result of factor analysis. 5. In the multiple repression analysis, the expressions of all sensory properties had compressive ratio, frictional coefficient in the regression expressions of $\ulcorner$H. V. obtained by sensory assessments$\lrcorner$, while the expressions of each H. V. and different physical properties in the regression expressions of $\ulcorner$H. V. obtained by KES-F system$\lrcorner$.

• Progress in Superconductivity
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• 제10권1호
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• pp.55-59
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• 2008

A Superconductor Flywheel Energy Storage System(SFES) mainly consists of a pair of non-contacting High Temperature Superconductor(HTS) bearings that provide very low frictional losses, a composite flywheel with high energy storage density. The HTS bearings, which offer dynamic stability without active control, are the key technology that distinguishes the SFES from other flywheel energy storage devices, and great effort is being put into developing this technology. The Superconductor Journal Bearing(SJB) mainly consists of HTS bulks and a stator, which holds the HTS bulks and also acts as a cold head. Static properties of HTS bearings provide data to solve problems which may occur easily in a running system. Since stiffness to counter vibration is the main parameter in designing an HTS bearing system, we investigate SJB magnetic force through static properties between the Permanent Magnet(PM) and HTS. We measure stiffness in static condition and the results are used to determine the optimal number of HTS bulks for a 100kWh SFES.