• Composites Research
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• 제30권5호
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• pp.297-302
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• 2017

본 연구에서는 적층복합재료에 발생하는 주요 손상인 박리를 방지하기 위하여, 굽힘-비틀림 하중이 작용하는 T-빔의 유한요소해석을 수행하였다. 복합재료 T-빔의 제작에 사용할 수 있는 3차원 직조 프리폼을 설계하고자 하였으며, 이는 2차원 구조의 직조섬유가 두께방향으로도 직조가 되어 있는 형태로서, 층간 분리에 의한 박리를 방지할 수 있는 구조이다. 적층복합재료의 해석 및 평가를 위하여 개발된 유한요소해석 소프트웨어인 ANSYS Composites PrePost를 이용하여 구조해석을 수행함으로써 적층복합재료의 섬유비율을 최적화하고, 이를 토대로 3차원 프리폼 T-빔의 제작을 위한 가이드라인을 제시하였다. 해석결과, T-빔의 길이방향 섬유의 비율이 수직방향 섬유의 2배일 때 가장 높은 강도를 보였으며, 하중조건의 변화에도 최적화된 빔 구조의 강도가 유지되는 것을 확인할 수 있었다. 도출된 섬유비율을 이용하여 3차원 프리폼을 개발할 경우, 박리가 일어나지 않는 고강도의 T-빔 구조물을 제작할 수 있을 것으로 기대된다.

• 한국기계가공학회지
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• 제16권6호
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• pp.63-68
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• 2017

The purpose of this study is to improve the whitening phenomenon around the PET preform gate for blow molding. CAE analysis of plastic injection molding has been applied to design of preform shape and select the injection molding conditions. A ceramic insulation gate with lower thermal conductivity than metal is applied to improve the whitening phenomenon created around the gate in the injection molding process. According to the results of CAE analysis, the warpage deformation at the square corner was estimated to be about 0.34 mm at the bottom. From the results of the temperature history analysis, it was confirmed that the resin near the gate cooled more rapidly than the cavity. Ceramic insulated gates were fabricated to reduce the cooling rate and experiments were conducted to confirm the effectiveness of the whitening phenomenon improvement. As a result of the ceramic insulation gate experiment, it was confirmed that the whitening phenomenon was significantly reduced around the gate.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2007년도 춘계학술대회 논문집
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• pp.427-430
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• 2007

Gas turbine disk components have been used by Ni-base superalloys which have high temperature strength for enduring stress induced by high speed rotation. This study introduced the overview of development strategy of precision forging of turbine disk and closed-die forging process for manufacturing good quality gas turbine disk. To make superior quality turbine disk, it is important to select optimal forging process conditions like preform shape, die shape and forging temperature etc. In this paper, closed-die forging process has been studied through the rigid-plastic finite element simulation. Proposed forging process can be used for the successful manufacturing of small-size gas turbine disk.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2003년도 추계학술대회논문집
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• pp.255-258
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• 2003

In this study, to develop a flash-less die for forming of shoe-outsole, experiments and forming analysis were carried out. In order to reduce the extra-materials, of feet method and mass distribution method are used in the preform design. To improve the accuracy of contact surface of dies, the contact status of dies are measured by using the pressure film. The vertical pressing die structure and the guide-gutter system have been developed for the discharge of extra-materials and re-pressing. By the investigation, flash of shoe-outsole was considerably reduced.

• 한국정밀공학회지
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• 제22권1호
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• pp.103-108
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• 2005

In this study, to develop a flash-less mold for forming of shoe-outsole, experiments and forming analysis were carried out. In order to reduce the extra-materials, offset method and mass distribution method are used in the preform design. The vertical mold structure pressing the preform was introduced to produce a flash-less shoe-sole. To measure the contact status of parting surface of mold, the pressure film has been used. The guide-gutter system and the continuous pressing mold have been developed for the discharge of extra-materials and re-pressing. By the investigation, flash of shoe-outsole was considerably reduced.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 추계학술발표대회 논문집
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• pp.253-256
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• 2000

In order to commercialize the low cost composite fabrication technology in the area of domestic aerospace structure field, Resin Transfer Molding process has been considered as an alternative process to replace the high cost autoclave technology. The end part for the development of RTM process is the control rod of flight control system of aircraft. A braided preform was triaxially designed to improve the dimensional stability and mechanical property in the direction of external loads. Through the flow analysis using CVFEM, the resin filling time was calculated and the resin injection method was determined. The results of the flow analysis were directly applied to RTM mold design. The control rod was successfully manufactured by RTM process using internal pressure. The length and outer diameter of the manufactured part are 1148mm and 32mm, respectively.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 1994년도 추계학술대회 논문집
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• pp.173-181
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• 1994

Process design is one of the most important fields in metal forming, where the finite element method has appeared a useful method for industrial applications. In this study, a program using the rigid plastic finite element has been developed for preform design in three-dimensional plastic deformation. The surface integration for calculation of the friction between die and workpiece has been implemented with care in numerical treatment. The developed program is applied to a precision coining process for designing an optimal punch.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2008년도 추계학술대회 논문집
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• pp.327-328
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• 2008

• 대한기계학회:학술대회논문집
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• 대한기계학회 2005년도 창립60주년 기념 추계 학술대회
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• pp.122.1-122.1
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• 2005

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2008년도 춘계학술대회 논문집
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• pp.817-818
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• 2008