• Composites Research
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• 제26권1호
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• pp.7-13
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• 2013

본 연구에서는 특수강과 복합재료를 사용한 이중구조 실린더의 설계를 위한 해석에 대해서 기술하였다. 특수강과 복합재의 이중구조는 제품의 특성에 적합한 물성을 유지하면서도 무게를 절감해 줄 수 있으며, 이로 인해 고탄성 저중량을 필요로 하는 각종 지상무기 산업분야와 항공분야, 스포츠 관련 분야 등에 점차 확대 적용되고 있다. 따라서 본 연구에서는 하나의 설계에 복합재의 적층각, 종류 등을 바꾸어 가며 이중구조의 설계에 가장 적합한 복합재 적용 방법을 찾기 위해 해석을 실시하였다. 또한 해석의 결과 값들의 비교를 통해 본 연구 설계목표에 가장 알맞은 복합재 적용 방법을 제시하였다.

• KSTLE International Journal
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• 제8권2호
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• pp.29-34
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• 2007

Recently, requirements relating to performance, environment and noise in the oil hydraulic system of the heavy construction equipment have been reinforced continuously. In order to solve these technical trends, studies on the system compactness, operation under high pressure and great rotating speed, electronic control, substitute oil, and noise reduction have been progressed briskly. Among these recent studies, the system operation under high pressure is quite difficult to carry into effect due to mechanical limitations; that is, for realizing the system operation in the hydraulic pump under high pressure, the improvements or innovations on the design techniques, the manufacturing techniques, and the lubrication performance of the working oil are required. Accordingly, in this study, the stress distribution and optimum design factors under the maximum pressure were discussed by using stress analysis on the cylinder block of the hydraulic axial piston pump, which is one of the most important relative sliding regions.

• Nuclear Engineering and Technology
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• 제52권2호
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• pp.397-416
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• 2020

Investigations of the commercial aircraft impact effect on nuclear island infrastructures have been drawing extensive attention, and this paper aims to perform the safety assessment of Generation III nuclear power plant (NPP) buildings subjected to typical commercial aircrafts crash. At present Part II, based on the verified finite element (FE) models of aircrafts Airbus A320 and A380, as well as the NPP containment and auxiliary buildings in Part I of this paper, the whole collision process is reproduced numerically by adopting the coupled missile-target interaction approach with the finite element code LS-DYNA. The impact induced damage of NPP plant under four impact locations of containment (cylinder, air intake, conical roof and PCS water tank) and two impact locations of auxiliary buildings (exterior wall and roof of spent fuel pool room) are evaluated. Furthermore, by considering the inner structures in the containment and raft foundation of NPP, the structural vibration analyses are conducted under two impact locations (middle height of cylinder, main control room in the auxiliary buildings). It indicates that, within the discussed scenarios, NPP structures can withstand the impact of both two aircrafts, while the functionality of internal equipment on higher floors will be affected to some extent under impact induced vibrations, and A380 aircraft will cause more serious structural damage and vibrations than A320 aircraft. The present work can provide helpful references to assess the safety of the structures and inner equipment of NPP plant under commercial aircraft impact.

• 대한치과보철학회지
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• 제35권4호
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• pp.627-646
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• 1997

In order to find the degree of osseointegration at bone-implant interface of clinically successful implants, models including the 3.75mm wide, 10mm long screw type $Br{\aa}nemark$ implant as a standard and cylinder, 15mm long, 5.0mm wide, two splinted implants, and implants installed in various cancellous bone density were designed. Also, the amount of load and material of prostheses were changed. The stress and minimum contact fraction were analyzed on each model using three-dimensional finite element method(I-DEAS and ABAQUS version 5.5). The results of this study were as follows. 1. 10mm long, 3.75mm diameter-screw type implant had $36.5{\sim}43.7%$ of minimum contact fraction. 2. Cylinder type implant showed inferior stress distribution and higher minimum contact fraction than screw type. 3. As implant length was increased, minimum contact fraction was increased a little, however, maximum principal stress was decreased. 4. Implants with a large diameter had lower stress value with slightly higher minimum contact fraction than standard screw type. 5. Two splinted implants showed no change of minimum contact fraction. 6. The higher bone density, the lower stress value. 7. The material of occlusal surface had no effect on the stress of the bone-implant interface.

• 한국전산구조공학회논문집
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• 제15권3호
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• pp.389-398
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• 2002

동전모양의 균열이 이상복합 실린더 계면에 존재하는 혼합모드 조건(I, II)에 대해 유한요소법을 사용하여 에너지해방율을 구하였다. 두재료의 탄성비와 노치율을 변화시켜 상업용 FEM 프로그램인 ABAQUS로부터 얻은 결과를 가상 균열법과 J 적분법에 적용하였으며 에너지해방율을 구하여 무차원함수로 표현하였다. 모드 II의 무차원 에너지해방율($\sqrt{G_{II}E^*}/\sqrt[p]{\pi a}$)은 균열길이와 탄성비가 증가되면서 그 값이 증가됨을 알수 있었다. 반면, 모드 I의 무차원 에너지해방율($\sqrt{G_{I}E^*}/\sqrt[p]{\pi a}$)은 탄성비가 증가하면서 그 값이 감소하며, 두재료의 탄성비가 3 이상인 경우에 균열길이가 증가되면서 무차원 에너지해방율이 감소하다가 다시 증가하게 나타났다. 또한 수치해석된 결과치를 무한판 실린더의 응력확대계수에 대한 정해와 비교하여 본 해석의 신뢰성을 확보하였다.

• 한국항공우주학회지
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• 제46권12호
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• pp.994-1003
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• 2018

유한요소 해석을 이용하여 분할 너트를 이용하는 파이로테크닉 분리 너트의 체결부 특성을 파악하였다. 분할 너트를 이용하는 경우, 체결 과정에서 분할 너트가 반경 방향으로 벌어지는 것을 막기 위해 구속해주는 구속원통이 필수적이다. 이때, 제작 과정에서 공차로 인해 분할 너트의 외경과 구속원통 내경 사이에 발생하는 틈새의 영향을 파악하기 위하여 적절한 유한요소 볼트 체결 모델링 기법을 연구하였으며, 틈새가 0.00, 0.03, 0.06, 0.10 mm인 모델을 만들어 해석 결과를 검토하였다. 해석 결과를 통해 너트의 분할 여부 및 틈새 크기에 따라 달라지는 체결부의 특성을 확인하였으며 이로부터 신뢰성 있는 파이로테크닉 분리 너트 설계를 위해 고려해야 할 사항을 파악하였다.

• Nuclear Engineering and Technology
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• 제20권3호
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• pp.197-202
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• 1988

장기 용출율을 예측하기 위하여 유한 격판 근사 방법이 개발되었다. 이 방법은 폐기물 고화체에서의 방사성 동위원소 확산 특성이 고화체 형태에 관련되지 않고 체적/면적비 (V/S)와 확산계수에만 의존한다는 가정에 근거하고 있다. 결과적으로 용출율은 동일 체적/면적비를 갖는 유한 격판을 기술하는 방정식의 해로 표시할 수 있다. 유한 격판 근사 방법을 사용한 계산 결과는 유한 원통과 유한 구형에 관한 확산 해석에 관한 해와 비교되었다. 여기서 도출된 단순 모델은 다른 모델과의 비교 결과 잘 일치하고 있고 방사성 핵종의 용출 현상에 관한 장기 예측에 전반적인 응용이 가능한 것을 보여준다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2006년도 춘계학술대회 논문집
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• pp.387-388
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• 2006

This article provides a dynamic analysis model for huge marine engine that examined analytically variation effects of frequency response by fitting of transverse stays such as hydraulic type. First, vibration analysis using the three dimensional finite element models for the huge marine engine has performed in order to find out the dynamic characteristics. Second, three dimensional finite elements model for the huge marine engine was modifued so that generate forcing nodes in crosshead part and top bracing nodes in cylinder frame part. Third, a system matrix and output matrix was derived for the general siso(single input single out) state space model. Finally, developed state space model for the three dimensional finite elements model for the huge marine engine without the additional modifying process.

• 대한기계학회논문집A
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• 제27권7호
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• pp.1138-1145
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• 2003

In this paper, a study on the dynamic behavior and lubrication characteristics of a reciprocating compression mechanism used in small refrigeration compressor is performed. In the problem formulation of the compressor dynamics, the viscous frictional force between piston and cylinder wall is considered in order to determine the coupled dynamic behaviors of piston and crankshaft. The solutions of the equations of motion of the reciprocating mechanism along with the time dependent Reynolds equations for the lubricating film between piston and cylinder wall and oil films of the journal bearings are obtained simultaneously. The hydrodynamic forces of journal bearings are calculated using finite bearing model and Gumbel boundary condition. And, a Newton-Raphson procedure was employed in solving the nonlinear equations of piston and crankshaft. The results explored the effects of design parameters on the stability and lubrication characteristics of the compression mechanism.

• Bulletin of the Korean Chemical Society
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• 제29권6호
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• pp.1131-1136
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• 2008

The electrical repulsive energy between two model cylinders was calculated by solving nonlinear Poission- Boltzmann (P-B) equation under Derjaguin approximation. Effects of the surface potential, Debye screening length, and configuration of cylinders on the repulsive interaction energy were examined. Due to the anisotropy of the shape of cylinder, the interaction repulsive energy showed dependence to the configuration of particles; cylinders aligned in end-to-end configuration showed largest repulsive energy and crossed particles had lowest interaction energy. The configuration effect is originated from the curvature effect of the interacting surfaces. The curved surfaces showed less repulsive energy than flat surfaces at the same interacting surface area. The configuration dependency of interaction energy agreed with the previous analytical solution obtained under the linearized P-B equation. The approach and results present in this report would be applicable in predicting colloidal behavior of cylindrical particles.