• E2M - 전기 전자와 첨단 소재
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• 제10권1호
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• pp.8-14
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• 1997

The UV/O$_{3}$ dry cleaning has been well known in removing organic molecules. The UV/O$_{3}$ dry cleaning method was performed to clean the Si wafer surfaces and contact holes contaminated by organic molecules such as residual PR. During the cleaning process, the Si surfaces were analyzed with X-ray photoelectron spectroscopy (XPS), atomic force microscope (AFM) and ellipsometer. When the UV/O$_{3}$ dry cleaning at 200'C was performed for 3 minutes, the residual photoresist was almost removed on Si wafer surfaces, but Si surfaces were oxidized. For UV/O$_{3}$ application of contact hole cleaning, the contact string were formed using the equipment of ISRC (Inter-university Semiconductor Research Center). Before Al deposition, UV/O$_{3}$ (at 200.deg. C) dry cleaning was performed for 3 minutes. After metal annealing, the specific contact resistivity was measured. Because UV/O$_{3}$ dry cleaning removed organic contaminants in contact holes, the specific contact resistivity decreased. Each contact hole size was different, but the specific contact resistivities were all much the same. Thus, it is expected that the UV/O$_{3}$ dry cleaning method will be useful method of removal of the organic contaminants at smaller contact hole cleaning.

• Nuclear Engineering and Technology
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• 제48권3호
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• pp.765-772
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• 2016

In analyzing residual radiation, researchers generally use a two-step Monte Carlo (MC) simulation. The first step (MC1) simulates neutron transport, and the second step (MC2) transports the decay photons emitted from the activated materials. In this process, the stochastic uncertainty estimated by the MC2 appears only as a final result, but it is underestimated because the stochastic error generated in MC1 cannot be directly included in MC2. Hence, estimating the true stochastic uncertainty requires quantifying the propagation degree of the stochastic error in MC1. The brute force technique is a straightforward method to estimate the true uncertainty. However, it is a costly method to obtain reliable results. Another method, called the adjoint-based method, can reduce the computational time needed to evaluate the true uncertainty; however, there are limitations. To address those limitations, we propose a new strategy to estimate uncertainty propagation without any additional calculations in two-step MC simulations. To verify the proposed method, we applied it to activation benchmark problems and compared the results with those of previous methods. The results show that the proposed method increases the applicability and user-friendliness preserving accuracy in quantifying uncertainty propagation. We expect that the proposed strategy will contribute to efficient and accurate two-step MC calculations.

• Journal of Advanced Marine Engineering and Technology
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• 제38권9호
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• pp.1146-1149
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• 2014

단자 표식이 불분명한 3상유도전동기에서 고정자 권선의 극성을 판별하는 데는 외부 여자전류에 의해 유도되는 기전력 특성에 기초하거나 또는 회전자의 잔류자기를 이용하는 방법이 가능하다. 회전자의 잔류자기로 유도되는 권선에서의 기전력은 자속 크기와 수동 구동의 회전자 속도 및 위상 관계에 따라 정해지며 이 같은 극성 판별이 작업현장에서 가능하려면 기전력의 크기가 멀티테스터로 확인될 수 있는 정도이어야 하고 또한, 코일 간 위상 특성이 극성 판별에 적합해야 한다. 잔류자기에 의한 기전력들이 3상 평형 관계에 있다면 전체 합성 전압은 권선들의 극성 연결 상태가 정상일 때 0이 되어야 하는 한편, 극성 연결의 오류 시에는 상대적으로 큰 출력 전압을 나타낸다는 점에서 본 연구에서는 각 경우에 대한 특성을 분석하였다. 또한, 잔류자기에 의한 판별 방식을 실험용 전동기에 적용하여 극성의 정상 및 이상 상태에서의 출력 파형을 비교함으로써 제시된 방식이 극성 판별 방법으로서 현장에서 용이하게 활용될 수 있는지를 확인한다.

• 소음진동
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• 제11권1호
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• pp.68-75
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• 2001

A method for actively controlling dynamic reaction forces in flexible structures subject to persistent excitations is presented. Since reaction forces are not directly measured in flexible structures, reaction forces are estimated by using the Kalman filter. The estimated reaction force is used as an error signal in the adaptive feedforward disturbance cancellation controller. In order to compensate the static effect of the truncated modes in the reaction forces, the residual flexibility matrix is used with the Kalman filter. The paper presents the formulation of the reaction forces in conjunction with the Kalman filter estimator and the adaptive feedforward controller. The results show that the dynamic reaction forces at its supports in a flexible beam test rir are well suppressed.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집A
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• pp.849-853
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• 2000

The retaining rings used to restrain the end turns of the rotor winding against centrifugal force require very careful attention during design and manufacture because they have traditionally been the highest-stressed components of the generator. In other words, the rings maintain their shrink fits during their entire service life. In this study, using finite element method, the part of shrink fits in generator was analyzed to obtain residual stresses in retaining ring and contact Pressures between contact surfaces at zero, rated, and 120 rated speeds, respectively.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회A
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• pp.464-468
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• 2008

In most of the passenger side airbag door in hard type IP today is designed with invisible tear-seam line. In order to design the tear-seam invisible, the tear-seam must be designed with required RWT (residual wall thickness) that is just thick enough to be broken by the PAB pressure on deployment and not by other surrounding impact forces. Hence, keeping the right optimum opening force is very important, and finding the right RWT became the key in designing the tear-seam. The study conducted in this paper describes the search for the optimum RWT around the tear-seam by using finite element method and the optimum RWT is suggested for milling type tear-seam having V-shape cross-section.

• 한국인터넷방송통신학회논문지
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• 제22권2호
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• pp.9-14
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• 2022

본 논문은 부분집합 합 문제의 해를 수행 복잡도 O(nlogn)으로 얻는 알고리즘을 제안하였다. SSP는 집합 S의 원소가 초증가수열과 랜덤수열로 구성된 경우로 구분된다. 초증가수열 SSP의 해를 구하는 알고리즘은 수행 복잡도 O(nlogn)의 가산 알고리즘 (Additive Algorithm)이 제안되었다. 그러나 랜덤수열 SSP의 해를 구하는 알고리즘은 2ⁿ-1의 가능한 모든 경우수를 확인하는 Brute-Force 방법으로 수행 복잡도는 O(n2ⁿ)만이 알려져 있다. 결국, SSP는 NP-완전 (NP-Complete) 문제로 알려져 있다. 본 논문은 초증가수열과 랜덤수열 SSP에 대해 수행 복잡도 O(nlogn)으로 해를 구하는 감산 알고리즘 을 제안하였다. 기존 개념은 목표 값 t보다 작은 값으로 구성된 부분집합 S에 대해 부분집합의 합에서 목표값을 뺀 값을 잉여량 (Residual, r)으로 하여 잉여량 보다 작은 값들 중 최대 값을 S에서 제거하는 방법을 적용하였다. 제안된 알고리즘을 다양한 초증가수열과 랜덤수열 SSP에 적용한 결과 S의 원소 개수보다 적은 수행 횟수로 해를 빠르게 얻는데 성공하였다. 결국, 제안된 알고리즘은 SSP의 해를 얻는 일반적인 알고리즘으로 적용할 수 있을 것이다.

• Journal of Welding and Joining
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• 제15권5호
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• pp.64-73
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• 1997

Deformations of structures due to welding appear much complicated and deformated modes are also complex. As parameters governing deformations are various and effect of parameters on deformations is not well known, precise prediction of deformation due to welding has been a difficult problem. Until now, many research papers as to welding deformation have been published, but the research results can explain only one aspect of welding deformation have been published, but the research results can explain only one aspect of welding deformation and are hard to be used in reasonable prediction of welding deformations in complicated structures. In this study, based on the accumulated results concerning to welding deformations, a practical method to predict complicated welding deformations of large structure is proposed. A simplified model to estimate residual plastic strains is suggested and main parameters affecting residual plastic strains are shown to be heat input and joint restaints. Inherent strain theory and experimental data are combined with the finite element method and welding deformations of large structures are calculated by elastic analysis. Comparison of calculated results with experimental data shows the accuracy and validity of the proposed method.

• Nuclear Engineering and Technology
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• 제53권5호
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• pp.1686-1704
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• 2021

This study addresses the numerical simulation of the shield building of an AP1000 nuclear power plant (NPP) subjected to a large commercial aircraft impact. First, a simplified finite element model (F.E. model) of the large commercial Boeing 737 MAX 8 aircraft is established. The F.E. model of the AP1000 shield building is constructed, which is a reasonably simplified reinforced concrete structure. The effectiveness of both F.E. models is verified by the classical Riera method and the impact test of a 1/7.5 scaled GE-J79 engine model. Then, based on the verified F.E. models, the entire impact process of the aircraft on the shield building is simulated by the missile-target interaction method (coupled method) and by the ANSYS/LS-DYNA software, which is at different initial impact velocities and impact heights. Finally, the laws and characteristics of the aircraft impact force, residual velocity, kinetic energy, concrete damage, axial reinforcement stress, and perforated size are analyzed in detail. The results show that all of them increase with the addition to the initial impact velocity. The first four are not very sensitive to the impact height. The engine impact mainly contributes to the peak impact force, and the peak impact force is six times higher than that in the first stage. With increasing initial impact velocity, the maximum aircraft impact force rises linearly. The range of the tension and pressure of the reinforcement axial stress changes with the impact height. The perforated size increases with increasing impact height. The radial perforation area is almost insensitive to the initial impact velocity and impact height. The research of this study can provide help for engineers in designing AP1000 shield buildings.

• 대한기계학회논문집A
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• 제24권7호
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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.