• 한국가스학회지
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• 제20권2호
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• pp.43-48
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• 2016

본 논문에서는 돌출구조물을 장착한 안전모의 지지하중과 응력분포에 대한 유한요소 해석결과를 제시하고 있다. 9.4mm의 동일한 변위하중을 안전모에 가한 5가지의 서로 다른 해석모델에 대하여 지지하중과 von Mises 최대응력을 해석하였다. 이들 모델에서, 모델 4와 모델 5는 주어진 9.4mm의 변위하중에 대하여 최고의 지지하중과 낮은 최대응력을 보여준다는 측면에서 우수한 것으로 나타났다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2006년도 춘계학술대회 논문집
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• pp.515-516
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• 2006

The goal of total disc replacement is to restore pain-free mobility to a diseased functional spinal unit, by replacing the degenerated disc with a mobile bearing prosthesis. SB Charite III is named commercial product as the Artificial Intervertebral Disc (AID). SB Charite III consists of sliding core and endplate made by Ultra-high Molecular Weight Polyethylene (UHMWPE) and cobalt chrome alloy, respectively. To evaluate the effect of von-Mises stress in AID, and three-dimensional finite element model of AID analysis was preformed for four different loading types of sliding core. Consequently, endplate was compared with a compressive preload at 400N and flexion moment at $3{\sim}9Nm4. Therefore, this research has obtained result that von-Mises stress of sliding core in AID disc by radius curvature.

• 한국추진공학회지
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• 제26권5호
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• pp.44-51
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• 2022

본 연구에서는 굴곡이 있는 형상의 노즐의 제작 방법으로 5축 가공을 제안하였고 제작한 형상의 구조적 검토를 위해 유동 해석과 구조해석을 활용하였다. 유동 해석에 사용한 프로그램은 STAR-CCM+이며 노즐의 내부온도와 압력 분포를 획득하였고 구조해석의 경계조건으로 사용하였다. 구조해석은 상용 프로그램 NASTRAN을 활용하였으며 von-mises 기법으로 응력을 계산하였다. 발생하는 최대 응력 값을 기준으로 안전 마진은 0.78, 베어링 안전 마진 또한 46.8로 안전하였다. 그리고 크리프 수명은 Larson-Miller 변수식 방법을 사용하여 최대 응력 값 187 MPa와 배기가스 완전 혼합된 온도 463 K를 적용하여 예측된 수명 시간은 9.97 x 10¹² 시간으로 계산되었다.

• 한국군사과학기술학회지
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• 제24권5호
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• pp.467-474
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• 2021

A study on optimal shape selection of a mechanical fastening for the repair of crack defect of ROK Air Force F-5 fighter wing was conducted. The crack defect occurred in the spar of the wing, and the technical manual does not specify the repair method. However, ROK Air Force decided to develop a repair technology for this defect in consideration of various logistic conditions. Three repair shapes for the proper repair were devised and the finite element analysis was performed to examine the structural safety of these three connection members. As a result of the structural safety review, two connection members except one were structurally safe with safety margins over zero because the calculated stress values were at or below the yield strength level. Therefore, two connection members were determined to be able to use for repair under the condition that the aircraft operated within the design limit load. The results of this study would be very useful if the same defect occurs in long-term aircraft operated by the ROK Air Force.

• The Journal of Advanced Prosthodontics
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• 제12권5호
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• pp.316-321
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• 2020

PURPOSE. The stress distribution and microgap formation on an implant abutment structure was evaluated to determine the relationship between the direction of the load and the stress value. MATERIALS AND METHODS. Two types of three-dimensional models for the mandibular first molar were designed: bone-level implant and tissue-level implant. Each group consisted of an implant, surrounding bone, abutment, screw, and crown. Static finite element analysis was simulated through 200 N of occlusal load and preload at five different load directions: 0, 15, 30, 45, and 60°. The von Mises stress of the abutment and implant was evaluated. Microgap formation on the implant-abutment interface was also analyzed. RESULTS. The stress values in the implant were as follows: 525, 322, 561, 778, and 1150 MPa in a bone level implant, and 254, 182, 259, 364, and 436 MPa in a tissue level implant at a load direction of 0, 15, 30, 45, and 60°, respectively. For microgap formation between the implant and abutment interface, three to seven-micron gaps were observed in the bone level implant under a load at 45 and 60°. In contrast, a three-micron gap was observed in the tissue level implant under a load at only 60°. CONCLUSION. The mean stress of bone-level implant showed 2.2 times higher than that of tissue-level implant. When considering the loading point of occlusal surface and the direction of load, higher stress was noted when the vector was from the center of rotation in the implant prostheses.