• Journal of the KSME
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• v.29 no.3
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• pp.244-252
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• 1989

평면변형조건에서 성형한계를 빠르고 정확하게 측정할 수 있는 방법을 개발하는 것도 중요하다. 평면변형조건에서의 성형한계를 구하는 데에는 펀치 스트레칭이 주로 이용되지만 그 외에도 여러 가지 방법들이 시도되고 있다. 평면변형조건에서 펀치스트레칭 시험을 행하여 파단이 일 어날 때까지의 펀치 행정거리를 한계 돔 높이(limiting dome height)라 하여 선진 제국에서는 박판금속의 성형성에 대한 품질관리 수단으로서 이용하고 있다. 우리나라의 박판금속의 성형 업계에서도 새로운 공정의 개발에 있어서 성형한계도와 변형측정법을 이용하므로서 시행착오를 줄이고, 한계돔 높이에 의한 품질관리기법을 이용하므로서 불량율저감 및 생산성 향상을 기할 필요가 있다 하겠다. 각종 재료에 대하여 측정한 성형한계에 관한 자료는 그 대표적인 값(예를 들면, 평면변형에서의 성형한계 값)으로서 컴퓨터에 저장하여두면 성형성에 대한 CAE에 의한 분석시에 편리하게 이용될 수 있다.

• Journal of the Korean Society for Precision Engineering
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• v.14 no.10
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• pp.127-134
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• 1997

열가소성 복합재료는 고상 성형법에 의해 저렴한 가격으로 부피가 튼 제품의 제조에 널리 사용될 수 있어 아주 좋은 전망을 가지고 있다. 그러나, 이러한 재료의 성형성에 대해선 아직 잘 알려지지 않았다. 본 연구의 첫번때 주안점은 2축 인장성형시 성형성에 대한 연구에 두었다. 실험에 사용된 재료는 임의의 방향으로 위치한 유리 섬유를 중량비로 20, 35, 40% 함유한 폴리프로필렌이다. 성형시험은 75 .deg. C 에서 150 .deg. C 사이의 온도에서 행했으며, 펀치 속도는 0.01cm/sec 와 1cm/sec 에서 행했다. 2축 인장성형에서 측정된 한계 변형률(Limiting Strain)은 Marciniak 불완전성 (Imperfection) 이론에 근거한 예견치외 비교되었다. 이론치와 실험치가 잘 일치함을 보였으며, 성형한계선도(Forming Limit Diagram) 로써 결과들을 요약하였다. 성형한계 변형률은 성형온도와 성형속도에 의해 크게 영향을 받는다는 것을 보인다. 이러한 결과들은 적절한 성형조건이 선택된다면 열가소성 복합재료의 인장성형은 실제 상업적으로 이용하기에 충분한 성형성을 갖는다는 것을 보인다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2003.10a
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• pp.196-196
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• 2003

• Transactions of the Korean Society of Mechanical Engineers
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• v.9 no.6
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• pp.777-787
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• 1985

The study is concerned with the analysis of flanging as a sheet metal working process. In terms of mechanics, the flanging process can be divided into two groups, i.e, shrink flanging and stretch flanging. In this study, the shrink flanging process is analyzed by using the proposed energy criterion and the forming limit is found for the process. The forming limit for stretch flanging is also found by employing the neckind theory. Experiments are carried out for both processes. Approximate forming limits are obtained from the experiments. An approximate method to calculate the punch force is proposed and the computed results are compared with the experimental results. It is shown that there are good agreements in forming limits and punch forces between theory and experiments.

• Journal of the KSME
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• v.33 no.1
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• pp.47-65
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• 1993

판재의 스탬핑 성형성평가를 위해 소재제조업체와 자동차업체에서 널리 사용되고 있는 2,3개의 대표적인 모사실험과 컴퓨터 모드의 실험에 대하여 소개하였고 각각의 특징들에 대하여 논하 였다. 스탬핑금형의 개발과 연속생산공정에 있어서 성형한계선은 원형그리드해석기법과 함께 핀재의 성형난이도 평가 및 불량원인 규명과 조치에 유용하게 사용가능하다. 또한 돔장출실험과 평면변형장출실험에서 각각 얻어지는 한계돔높이와 한계펀치높이는 입하코일에 대한 스탬핑성 공여부의 사전확인 및 연속생산 공정에 대한 통계적 품질관리수단으로 활용하면 스탬핑공정에 서의 불량률감소 및 생산성향상에 기여할 수 있을 것으로 생각된다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.12
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• pp.1201-1208
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• 2009

Dome stretching tests and tension tests were performed to evaluate the formability of a copper alloy used for manufacturing the regenerative cooling chamber. The test specimens were prepared to investigate the effect of heat treatment and direction of specimens on the formability. The test results show that forming limit values are increased by the heat treatment of the material but the variation of the forming limit values by manufacturing direction is negligible compared to the heat treatment effect, and forming limit values are also different according to the test methods. These results indicate that the high temperature heat treatment of the material before bulging is a very important process to deform the inner cylindrical structure of the regenerative cooling chamber into a nozzle shape by the bulging process without necking or fracture and the test methods also have a great effect on a evaluation of the formability. The forming limit diagram obtained in this study would be utilized to the design of regenerative cooling chamber nozzles.

• Journal of Industrial Technology
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• v.19
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• pp.67-74
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• 1999

The mechanical properties including forming limit and deep-drawability of commercially-used sheet metals were experimentally estimated in this study. Uniaxial tensile test to obtain basic mechanical properties was carried out, followed by limiting dome height (LDH) test and forming limit diagram (FLD) test to quantitatively evaluate the sheet-formability. Deep drawing and reverse drawing tests were also performed to find out the critical values of the blank holding force and the gap between the die and the blank holder which enabled the deep drawing and reverse drawing of a successful cop without any wrinkle or fracture. The thickness of the cup wall along the rolling-, transeverse- and $45^{\circ}$-directions was measured and compared with one another. And the punch force-stroke curve and the critical punch force expected from the theory coincided with the experimental result very well for mild steel while not for aluminium alloy.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.25 no.7
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• pp.1107-1118
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• 2001

The forming limit diagram introduced by Keeler and Goodwin has been used generally to analyze the formability of sheet metal. However, path dependent forming limit curves based on the state of strain can be explained only by a single criterion which is based on the state. In this study, experimental forming limits in strain space of some metal sheets are transformed into forming limit curves in stress space. Effects of yield criterion are investigated in transforming the forming limit curves. Some important design aspects which are based on the close prediction of movements in forming limit curves during sheet forming are concluded.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.11a
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• pp.194-197
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• 2007

The dome stretching and tension test have been made to obtain a forming limit curve(FLC) for the copper alloy which is used for manufacturing the regenerative cooling chamber. For experimental survey of the forming limit curve, we have used in-plane tension specimen to obtain tension-compression strain state and also out of plane specimen to obtain tension-tension strain state through dome stretching test. All specimens are divided into longitudinal and radial direction specimens by the manufacturing method. The test results shows that in tension-tension region, copper alloy possesses a maximum major strain of 62.3% and maximum minor strain of 58.6%. In the tension-compression region, maximum major strain is 60.5% and maximum minor strain is 25.8%.

• Journal of Korean Society of Steel Construction
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• v.15 no.1
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• pp.17-24
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• 2003

This study aimed to develop experiment-based limiting heights for interior, nonload-bearing, cold-formed steelwall panels sheathed with gypsum board and subjected to uniformly distributed lateral loadings. Th e limiting heightswere evaluated by their strength (for flexure, shear, and web crippling) and deflection. Limiting heights for deflectionlimits of L/360, L/240, and L/120 (where L is the height of the wall) were developed over the range of typical designpressures.