• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 1999년도 춘계학술대회논문집
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• pp.82-85
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• 1999

Permanent magnets of Nd-Fe-B group have kept a key post in the permanent magnet market and used in various parts. Tube Process is a process to produce permanent magnets using a deformable tube for denslfication of powder magnets. Advantage claimed for this process is that it can accomplish both densification and anisotropication in one step forming. In this paper. the simulation has been carried out for a full Tube Process in a closed Qe considering the compressibility of material, arbitrary curved shape and deformable body contact between Nd-Fe-B powder magnet and copper tube. The results show that the analysis of Tube Process is applicable with great help in the stage of preform design.

• Fibers and Polymers
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• 제3권3호
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• pp.120-127
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• 2002

Ever since the ideal forming theory has been developed for process design purposes, application has been limited to sheet forming and, for bulk forming, to two-dimensional steady flow. Here, application for the non-steady case was made under the plane-strain condition. In the ideal flow, material elements deform fellowing the minimum plastic work path (or mostly proportional true strain path) so that the ideal plane-strain flow can be effectively described using the two-dimensional orthogonal convective coordinate system. Besides kinematics, schemes to optimize preform shapes for a prescribed final part shape and also to define the evolution of shapes and frictionless boundary tractions were developed. Discussions include numerical calculations made for a real automotive part under forging.

• 한국광학회지
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• 제14권3호
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• pp.219-223
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• 2003

광섬유의 잔류응력(residual stress)을 측정하기 위해 위상보정 편광기(polariscope)를 새롭게 구성하고, 간섭이나 회절에 대한 영향을 최소화시키면서 빠르고 정확하게 측정하는 방법을 제시하였다. 이 방법을 이용하여 일반 광섬유의 잔류 응력 분포를 측정할 수 있었다. 또한 광섬유의 잔류응력이 모재의 잔류응력분포와 달리 인출 시 발생하는 광섬유 내 온도의 냉각곡선에 밀접한 관계를 갖고 있음을 알 수 있었다.

• Composites Research
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• 제32권1호
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• pp.65-70
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• 2019

항공기 복합재료 날개 구조는 대부분 접착 혹은 패스너로 체결되어 있는데, 이러한 적층 구조 복합재료는 층간 강도가 취약하여 층간 분리가 일어나기 쉽다. 이러한 적층 복합재료의 단점을 보완하기 위해 두께 방향의 섬유를 보강한 3차원 직조형 복합재료를 통하여 강도, 손상 내구성, 충격 및 피로 하중을 향상시킬 수 있다. 또한, 자동화된 직조 공정에 의하여 단일 구조 near-net-shape의 프리폼 제조가 가능하기 때문에 공정 단축, 체결 부품 감소로 복합재료 전체 가격을 절감할 수 있다. 따라서 본 연구에서는 3차원 직조형 복합재료의 항공기 구조물 적용 가능성을 확인하기 위하여 3차원 프리폼의 기본적인 구조인 orthogonal(ORT), layer-to-layer(LTL), through-the-thickness(TTT) 패턴을 직조하고 이를 복합재료로 성형하여 압축 시험, 인장 시험, Open-hole 인장 시험을 하였다. 이 중 orthogonal 직조 복합재료가 인장 및 압축 탄성계수와 강도 모두 가장 높았으며 노치 민감도에서도 orthogonal 복합재료가 일방향 적층복합재료나 패브릭 적층 복합재료에 비하여 가장 우수한 특성을 보였다.

• 한국재료학회지
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• 제3권6호
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• pp.606-613
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• 1993

자동차용 부품재 및 일반산업용 재료로 사용되고 있는 AC4A Al합금에 $SiC_{w}$ preform을 용탕단조법으로 강화시킨 복합재료의 시효 경화능은 SiC/aub w/30%> 10%> 20%의 순이며, 이는 $100^{\circ}C$-$400^{\circ}C$까지의 등시시효에서도 같은 결과를 나타낸다. 복합재의 T6처리재가 AC4A I/M재 보다도 시효경화능이 크고 절대값이 높았으며 $SiC_{w}$체적분율 증가에 따라 초기경화 현상을 나타내었다. 가압력에 의한 강화효과는 미시효때와 같이 가압력 75MPa일때 가장 좋았으며, $SiC_{w}$는 30%> 10%>20%순이었다. 가압력이 낮을경우 가입과 동시에 휘스커는 파단되지 않고 원래의 형상을 유지하거나 기지금속과 wetting으로 일부 변형된 다음 가압이 진행되면서 이부부의 응력 집중으로 wetting부가 파단하게 되어 가압력을 이기지 못하고 파단하게 되어 휘스커 모양도 다각형이거나 구형에 가깝게 되며 가압이 진행됨에따라 재차 파단되므로써 길이도 짧게 된다. 한편 가압력 75 MPa일 경우 휘스커의 형상은 일부 변형된 것과 잘게 파손된 것이 고르게 공존하고 있어 강화효과가 가장 우수한 것으로 사료된다.

• 소성∙가공
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• 제18권2호
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• pp.150-155
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• 2009

A shaft for laser printers has to be produced with high dimensional accuracy of a few micrometers. Most companies produce the shaft, therefore, by machining. These days, forging process is tried to be employed in manufacturing the shaft for productivity. In this study, the dimensional inaccuracy of straightness is studied and the underfill is not focused because the shaft shape is simple and the load capacity of press is sufficient. The straightness and concentricity of the shaft is important for the operation of a laser printer. Many design parameters such as preform shapes, tooling dimensions, forging load, and billet geometries may affect on the dimensional accuracy. In the forging process of shafts, a billet which is cut from wires is used. The billet, therefore, may be a little bit curved but not always straight. The elastic recovery is considered to cause the dimensional inaccuracy. Therefore, the effect of the forging load on the elastic recovery and straightness is investigated through the finite element analyses using DEFORM-3D and ABAQUS.

• 대한기계학회논문집
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• 제18권11호
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• pp.2954-2966
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• 1994

The characteristics and good corrosion resistance at room and elevated temperatures led to increasing application of Ti-alloys such as aircraft, jet engine, turbine wheels. In forging of Ti-alloy at high temperature, die chilling and die speed should be carefully controlled because the flow stress of Ti-alloy is sensitive to temperature, strain and strain-rate. In this study, the forging of turbine disk was numerically simulated by the finite element method for hot-die forging process and isothermal forging process, respectively. The effects of the temperature changes, the die speed and the friction factor were examined. Also, local variation of process parameters, such as temperature, strain and strain-rate were traced during the simulation. It was shown that the isothermal forging with low friction condition produced defect-free disk under low forging load. Consequently, the simulational information will help industrial workers develope the forging of Ti-alloys including 'preform design' and 'processing condition design'. It is also expected that the simulation method can be used in CAE of near net-shape forging.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2011년 춘계학술대회논문집
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• pp.92-95
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• 2011

In manufacturing optical fibers, the process starts with the glass fiber drawing from the heated and softened silica preform in the furnace, and the freshly drawn glass fiber is still at high temperature when it leaves the glass fiber drawing furnace. It is necessary to cool down the glass fiber to the ambient temperature before it then enters the fiber coating applicator, since the hot glass fiber is known to cause several technical difficulties in achieving high quality fiber coating. As the fiber drawing speed keeps increasing, a current manufacturing of optical fibers requires a dedicated cooling unit with helium gas injection. A series of three-dimensional flow and heat transfer computations are carried out to investigate the effectiveness of fiber cooling in the fiber cooling unit. The glass fiber cooling unit is simplified into the long cylindrical enclosure at which the hot glass fiber passes through at high speed, and the helium is being supplied through several injection slots of rectangular shape along the cooling unit. This study presents and discusses the effects of helium injection rates on the glass fiber cooling rates.

• 한국정밀공학회지
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• 제27권5호
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• pp.63-68
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• 2010

The use of aluminum alloy parts in the automotive industry has been increasing recently due to its low weight compared with steel to improve fuel efficiency. Companies in the auto parts' manufacturing sector are expected to meet the government's strict environmental regulations. In this study, manufacturing process of aluminum alloy bolt has been designed from forming to heat treatment. Bolt forming process is composed of cold forging for body and rolling for thread. In this study only cold forging process is considered by employing the finite element method. In the cold forging process, preform shape was designed and damage value was considered for die design. Two steps of forging process has been developed by the simulation and a prototype was manugactured accordingly. As a final process, solution heat treatment and aging process was employed. A final prototype was found to meet the required specifications of tensile strength and dimension.

• 소성∙가공
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• 제17권8호
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• pp.600-606
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• 2008

In closed-die hot forging, a billet is formed in dies such that the flow of metal from the die cavity is restricted. Some parts can be forged in a single set of dies, whilst others, due to shape complexity and material flow limitations, must be shaped in multi sets of dies. The purpose of a performing operation is to distribute the volume of the parts such that material flow in the finisher dies will be sound. This study focused on the design of preforms, flash thickness and land width by theoretical calculation and finite element analysis, to manufacture the super hot forging product, 70MC type piston crown used in marine engine. The optimal design of preforms by the finite element analysis and the design experiment achieves adequate metal distribution without any defects and guarantees the minimum forming load and fully filling of the cavity of the die for producing the large piston crown. The maximum loads obtained by finite element analysis are compared with the results of experiments. The loads of the analysis have good agreements with those of the experiment. Results obtained using DEFORM-2D enable the designer and manufacturer of super hot forging dies to be more efficient in this field.