• Transactions of The Korea Fluid Power Systems Society
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• v.1 no.1
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• pp.10-16
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• 2004

The failures such as leakage and burst stemmed from the repetitive motions of bending and stretching of the assembly of hydraulic hose in construction machines, agriculture machines, vehicles, and industrial heavy machines can induce big troubles. Therefore, the hydraulic hose itself eventually requires an estimation of life to operate the hydraulic system safely. In this research, we have qualitatively selected the efficient test items by the analysis of the life and potential failures of hydraulic hose. We have used more than seven of hydraulic hoses simultaneously for the research. We have applied impulse pressure and half omega flexing motions to the accelerated life testing Test results have been expressed by employing weibull plot.

• Journal of the Korean Society of Manufacturing Process Engineers
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• v.17 no.2
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• pp.37-46
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• 2018

Present research is to evaluate and improve the sealing performance of the duct cap assembly for the ice dispensers through structural analysis. The nonlinear contact problems to check the sealing performance were analyzed using ANSYS software. The results of the analyses related to the sealing performance: the displacement distribution, the contact condition between the cap-silicon and the case, and the pressure distribution on the contact surface, were examined and discussed. Based on the results of the existing design of the duct cap assembly, two cases of the design modifications to improve the sealing performance were introduced. By examining the results of the two cases, a final design improvement plan was proposed and analyzed. It is shown that the sealing performance of the proposed final design is much more favorable than the existing design. The method of structural analysis and design improvement of the duct cap assembly presented in this paper will help improve the sealing performance of the ice dispenser duct caps.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.24 no.7 s.178
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• pp.1740-1747
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• 2000

Under repeated rolling, initial plastic deformation introduces residual stresses which render the steady cyclic state purely elastic. This is called the process of shakedown. Many studies have been done about the shakedown in semi-infinite half space using calculated Hertizian pressure. In this paper shakedown processes in a shaft are studied by finite element analyses of a two dimensional(plane strain) model with elastic-linear-kinematic-hardening-plastic material subjected to repeated, frictionless rolling contact. Symmetric and non-symmetric pressure distributions are obtained using a simplified model of the bearing-shaft assembly. The rolling contact is simulated by repeatedly translating both pressure distributions along the surface of the shaft. By the influence of the non-symmetric pressure, larger residual radial tensile stress is generated in the immediate subsurface layer, which may make a crack propagate and, the subsurface undergoes a zigzag plastic deformation during the shakedown process, which may lead to a crack initiation.

• Journal of the Microelectronics and Packaging Society
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• v.19 no.1
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• pp.61-66
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• 2012

Chemical Mechanical Planarization (CMP) is a polishing process used in the microelectronic fabrication industries to achieve a globally planar wafer surface for the manufacturing of integrated circuits. Pad conditioning plays an important role in the CMP process to maintain a material removal rate (MRR) and its uniformity. For metal CMP process, highly acidic slurry containing strong oxidizer is being used. It would affect the conditioner surface which normally made of metal such as Nickel and its alloy. If conditioner surface is corroded, diamonds on the conditioner surface would be fallen out from the surface. Because of this phenomenon, not only life time of conditioners is decreased, but also more scratches are generated. To protect the conditioners from corrosion, thin organic film deposition on the metal surface is suggested without requiring current conditioner manufacturing process. To prepare the anti-corrosion film on metal conditioner surface, vapor SAM (self-assembled monolayer) and FC (Fluorocarbon) -CVD (SRN-504, Sorona, Korea) films were prepared on both nickel and nickel alloy surfaces. Vapor SAM method was used for SAM deposition using both Dodecanethiol (DT) and Perfluoroctyltrichloro silane (FOTS). FC films were prepared in different thickness of 10 nm, 50 nm and 100 nm on conditioner surfaces. Electrochemical analysis such as potentiodynamic polarization and impedance, and contact angle measurements were carried out to evaluate the coating characteristics. Impedance data was analyzed by an electrical equivalent circuit model. The observed contact angle is higher than 90o after thin film deposition, which confirms that the coatings deposited on the surfaces are densely packed. The results of potentiodynamic polarization and the impedance show that modified surfaces have better performance than bare metal surfaces which could be applied to increase the life time and reliability of conditioner during W CMP.

• Journal of the Korean Society of Industry Convergence
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• v.24 no.5
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• pp.597-608
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• 2021

The control head components used in small military vessels are designed to be domestically produced, prototypes, structural analysis, and casting methods are designed and cast. The control head assembly consists of a lever, an aluminum outside cover, Middle, front gear cover, back gear cover, and a zinc worm gear. In order to reverse the design of each component, 3D scanning device was used, 3D modeling was performed by CATIA, and prototype productions were carried out by 3D printer. In order to reduce the cost of components, gating system is used by gravity casting method. The SRG ratio of 1:0.9:0.6 was set by applying non-pressurized gating system to aluminum parts, 1:2.2:2.0 and pressurized gating system to zinc parts, and the shapes of sprue, runner and gate were designed. The results of porosity were also confirmed by casting analysis in order to determine whether the appropriate gating system can be designed. The results showed that all parts started solidification after filling completely. ANSYS was used for structural analysis, and the results confirmed that all five components had a safety factor of 15 more. All castings are free of defects in appearance, and CT results show only very small porosity. ZnDC1 zinc alloy worm gear has a tensile strength of 285 MPa and an elongation of 8%. The tensile strength of the four components of A356 aluminum alloy is about 137-162 MPa and the elongation is 4.8-6.5%.

• Proceedings of the Korea Information Processing Society Conference
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• 2006.05a
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• pp.783-786
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• 2006

컴퓨터기반 협동학습(CSCL)은 컴퓨터를 기반으로 학습자들이 공동체를 형성하고 상호협력관계를 통하여 학습하는 환경으로 학습자가 자신의 능력에 맞게 학습할 수 있고 다른 이들과 생각과 정보를 표현, 교환, 조언, 수정하는 등의 상호작용을 할 수 있다. 이러한 CSCL환경에서 학습자들이 어떤 학습 주제에 대해 주어진 프로젝트를 수행하기 위해 서로간의 생각과 정보를 효과적으로 교환하기 위해서는 그 주제에 속하는 개념들에 대한 용어들이 표준화되어지고, 개념들간의 관련성 및 제약성에 대한 정보들이 미리 정의되어 알려져 있어야만 한다. 그런데, 그러한 정보들을 학습자들이 일일이 파악하기란 매우 힘든 일이다. 이러한 문제는 온톨로지 기술을 이용하여 기계로 하여금 그러한 정보들을 이해하여 처리할 수 있도록 함으로써 해결할 수 있다. 따라서, 본 연구에서는 CAD 분야에서 학습자들이 어떠한 제품을 설계하기 위한 프로젝트를 수행시 서로간의 정보와 의견을 효과적으로 교환함으로써 프로젝트를 보다 효율적으로 수행할 수 있도록 하기 위해 공동의 학습공간을 지원하고 제품 설계에 대한 온톨로지를 구성하여 이를 이용하는 것을 제안한다.

• Journal of the Institute of Electronics Engineers of Korea TC
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• v.46 no.2
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• pp.126-133
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• 2009

In this paper, The planar waveguide slotted antenna is presented for a satellite communication of vehicles. In stead of the microstrip patch array antenna having a dielectric loss and a feeding loss, the proposed antenna has the 3-layered waveguide feeding network structure for assembling easily. Also this antenna can receive mechanically both RHCP and LHCP transmitted from a satellite using a polarizer made from a thin single layer film. The Gain of the proposed 4X8 array antenna is 27.5dB and the gain of 8X16 array antenna is 32dB.

• Aerospace Engineering and Technology
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• v.5 no.2
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• pp.174-180
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• 2006

The present paper describes transient thermal and mechanical analyses of a lox/kerosene type turbopump in a LRE(Liquid Rocket Engine). Turbopumps are used to pressurize propellants to achieve higher specific impulse of LRE. The turbopump under development has been designed and verified by structural analyses using finite element methods. Some parts of the turbopump operate under cryogenic environments, while the others work under ambient and high temperature environments. Therefore, numerical analysis at a turbopump system level is essential. In this study, casing assemblies of lox pump and fuel pump were analyzed to determine strength test and air-tightness test conditions. Also, some operational stress and strains of fuel pump casings were measured and analyzed. Based on these results, stress concentration of fuel pump casings during the operation could be successfully predicted.

• Korean Journal of Optics and Photonics
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• v.33 no.2
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• pp.74-83
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• 2022

The entire process, from the raw material to the final system qualification test, has been developed to fabricate a large-diameter, lightweight reflective-telescope system for a satellite observation. The telescope with 3 anastigmatic mirrors has an aperture of 700 mm and a total mass of 66 kg. We baked a silicon carbide substrate body from a carbon preform using a reaction sintering method, and tested the structural and chemical properties, surface conditions, and crystal structure of the body. We developed the polishing and coating methods considering the mechanical and chemical properties of the silicon carbide (SiC) body, and we utilized a chemical-vapor-deposition method to deposit a dense SiC thin film more than 170 ㎛ thick on the mirror's surface, to preserve a highly reflective surface with excellent optical performance. After we made the SiC mirrors, we measured the wave-front error for various optical fields by assembling and aligning three mirrors and support structures. We conducted major space-environment tests for the components and final assembly by temperature-cycling tests and vibration-shock tests, in accordance with the qualifications for the space and launch environment. We confirmed that the final telescope achieves all of the target performance criteria.

• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 2017.04a
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• pp.51-51
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• 2017

정식기는 주로 노외에서 사용되므로 사용자에 따라 극심한 작업환경 하에 놓일 수 있다. 사용 중 정식기 호퍼에 토양이나 자갈, 돌 등에 의해 반복적인 하중이 가해지거나 순간적인 충격하중이 가해져 취약부가 파손될 가능성이 있으므로, 토양과 직접 맞닿는 삽날부의 경우 내구성을 고려한 설계/제작이 필수적이다. 본 연구에서는 보행형 반자동 정식기 개발에서 고추묘와 같은 초장이 긴 작물의 묘를 효과적으로 이식할 수 있도록 개선된 삽날에 대해 기존 삽날과 강도 및 강성을 비교하고, 그 결과가 삽날의 내구성에 미칠 영향에 대하여 고찰하였다. 실험에는 양날 개폐 방식의 기존 및 개선삽날 2종이 사용되었으며, 각각 3회씩 정적 강도를 평가하였다. 실제 정식기 사용시 하중이 가해지는 방향은 삽날에 수직한 방향의 압축하중으로 이를 모사하여 일정변위 속도로 삽날에 하중을 가하였으며, 시험 진행시 DAQ 시스템을 통해 실시간으로 하중 및 변위 데이터를 저장하여 시험 종료 후 해당 데이터를 이용하여 $P-{\delta}$ 선도를 도출하였다. 시험 결과 기존삽날의 평균 최대하중이 개선삽날에 비해 높은 것으로 나타났으며, 최대 하중이 나타나는 지점의 변위의 경우, 기존삽날이 개선삽날에 비해 짧게 나타났다. 정적 강도측면에서 개선삽날이 기존삽날에 비해 최대 강도가 낮은 것으로 판단할 수 있으나, 실제 호퍼의 내구성에 영향을 줄 수 있는 주요 인자는 반복적으로 가해지는 비교적 낮은 수준의 충격하중으로 볼 수 있다. 이러한 관점에서 볼 때 일정 수준 이상의 강도를 가지면서, 기존삽날에 비해 낮은 강성을 가지는 개선삽날이 변형을 통한 충격에너지 흡수로 오히려 삽날 조립체(호퍼)의 내구성 측면에서 유리할 수 있다. 따라서 향후에는 기존 및 개선삽날을 적용한 호퍼에 대해 피로시험을 수행하여 관련 내용을 실험적으로 검증하고자 한다.