• Journal of Korean Society of Steel Construction
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• v.16 no.1 s.68
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• pp.145-153
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• 2004

Conventional lead-rubber bearings may be unstable in case of strong ground motions. To address this problem, this paper proposed a new concept of isolation device wherein shape memory alloy wires were incorporated in an elastomeric bearing. A three-span continuous steel bridge was used for seismic analyses to compare the performance of lead-rubber and proposed bearings. The proposed bearings showed almost the same performance as the lead-rubber bearings. In particular, the proposed bearings limited relative displacement effectively with strong ground motions and recovered its original undeformed shape.

• Journal of Sensor Science and Technology
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• v.7 no.6
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• pp.437-445
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• 1998

The actuator using shape memory alloy spring with bias spring can act as a bidirectional actuator due to the restoring force of the bias spring. In the design of shape memory actuator with bias spring, the required design specifications are the generated force and the necessary stroke. To fulfill these requirements, shape memory alloy spring and bias spring should be designed carefully considering the specified application. In this paper, the novel design method for shape memory alloy actuator with bias spring, which does not require any assumptions from experience, has been proposed and verified by the test of fabricated shape memory alloy actuator. The experimental results show good agreements with calculated values, which guarantees the practical validity of our proposed design method.

• Bulletin of the Korean Space Science Society
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• 2003.10a
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• pp.74-74
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• 2003

로켓엔진의 연소실에서는 고온의 연소가스로부터 다량의 열이 발생하기 때문에 이로부터 연소실을 보호하기 위한 방법이 필수적으로 요구된다. 한국 최초의 액체 로켓인 KSR-III 로켓의 주엔진인 KL-3 엔진에서는, 연소실을 보호하기 위한 방법으로 실리카/페놀(Silica/Phenolic) 내열재를 이용하는 용융냉각 방식을 채택하였다 용융냉각 방식은 내열재와 고온의 연소가스와의 물리ㆍ화학적 상호작용에 의해 삭마가 발생하게 되는데, 이러한 삭마는 연소실에서도 가장 고온부인 노즐목에 집중적으로 발생하는 경향이 있다. 그러나 노즐목에서 삭마의 진행은 노즐목의 크기를 증가시키고 연소압 및 추력을 감소시키는 부작용을 초래하게 된다. 본 연구에서는 이러한 열적 삭마에 의한 노즐목 크기의 증가량을 알아내기 위해 KL-3 엔진 노즐목의 형상을 측정하고자 시도하였으며, 노즐목의 삭마에 영향을 미치는 주요 인자를 확인하고 진행과정을 고찰하였다. 노즐목의 형상 측정을 위해서는 기존에 사용하던 3차원 변위 측정기를 이용한 방식의 접근이 곤란함에 따라 영상처리 기법을 도입한 측정 방식을 고안하여 사용하였으며, 이 장비는 만족스런 성능을 보여주었다. 시험결과를 통해서 삭마에 영향을 주는 주요 인자로 분무형태, 연소시간, 연소 온도를 제시하였고 이 중에서 분무형태는 삭마 형상에, 연소 시간 및 연소온도는 삭마량에 주로 영향을 끼친다는 것을 알 수 있었다. 또한 시간에 따른 삭마의 진행이 3개의 구간으로 나누어 설명할 수 있음을 밝혔는데, 노즐목이 원형을 그대로 유지하며 삭마진행이 미미한 구간, 원형에서 벗어나 요철형상이 발달하면서 삭마진행이 가속되는 구간, 요철형상이 이미 정착되어서 요철의 깊이만 증가하되 삭마량은 미미한 구간이다. 결과적으로 60초 연소 후 노즐목 면적 증가율은 +5.82% 정도이며, 이에 따른 연소압 및 추력의 감소 또한 1% 미만으로 미비하였다. 따라서 본 KL-3 엔진에 사용된 내열재의 내열 성능은 임무를 수행하기에 적절하다고 판단하였다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.14 no.10
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• pp.4685-4693
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• 2013

Present work deals with a shape optimal design to minimize the weight of the mask-frame used in the process of OLED vapor deposition by the fine metal mask. A design concept for an optimal shape of the frame to increase the stiffness and to reduce the weight is derived using the topology optimization, shape design variables of the frame by adopting slots being defined. An optimal shape is determined by solving the shape optimization problem to minimize the weight of the frame under constraints of the maximum displacement. Weight of the optimal design is 117.6 kg, which is reduced by 138.4 kg(54.1%) of that of the first design, 256 kg.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.15 no.4
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• pp.599-607
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• 2002

During the shape optimization, relocations of nodes happen successively. However, excessive movement of nodes often results in the mesh distortion and eventually deteriorates the accuracy of the optimum solution. To overcome this problem, an efficient method lot the shape optimization has been developed. The method starts from the design domain which is large enough to hold the possible shape of the structure. The design domain has pre-defined uniform fine meshes. In each cycle, the method allots real properties to the elements inside the structure and nearly zero to ones outside. The performance of the method is evaluated through two examples with displacement and frequency constraints.

• Journal of Sensor Science and Technology
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• v.7 no.4
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• pp.285-292
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• 1998

Shape Memory Alloy(SMA) has been used in many engineering fields because of its good characteristics of actuator. For example, SMA wire can be embedded easily in the polymer composite laminate and then be used as actuator for structural control. Since the strain have a significant influence on the electrical resistance of SMA wire, It is a possible to use the SMA wire as a sensor of such physical quantities. In this study, the possibility for the application of Ni-Ti SMA wire as a sensor embedded within a composite laminate is investigated.

• Journal of Korean Tunnelling and Underground Space Association
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• v.21 no.1
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• pp.93-113
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• 2019

The behavior of the 3 hinged precast arch structure was investigated by comparing field measurements with numerical analyses performed for precast lining arch structures, which are widely used for the open-cut tunnel. According to the field measurements, the maximum vertical displacement occurred at the crown with upward displacements during the backfilling up to the crown of the arch and downward displacements at the backfill height above the crown. The final crown displacement was 19 mm upward from the original position. The horizontal displacement at the sidewall, which had a maximum horizontal displacement, occurred inward of the arch when compacting the backfill up to the crown and returned to the original position after completing the backfill construction. According to the analysis of displacement measurements, economical design is expected to be possible for precast arch structures compared to rigid concrete structures due to ground-structure interactions. Duncan model gave good results for the estimation of displacements and deformed shape of the tunnel according to the numerical analyses comparing with field measurements. The earth pressure coefficients calculated from the numerical analyses were 0.4 and 0.7 for the left and the right side of the tunnel respectively, which are agreed well with the eccentric load acting on the tunnel due to topographical condition and actual field measurements.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.35 no.7
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• pp.655-660
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• 2007

A canard-leading edge flap deflection scheduling laws have been established to enhance the maneuverability of the canard type fighter class aircraft. These scheduling laws are the relation of canard-leading edge flap deflections and flight conditions to maximize the lift-drag ratio. For these purposes, the corrected supersonic panel method has been used to predict the lift-drag characteristics due to canard-leading edge flap deflections. In addition, the high speed wind tunnel test has been conducted with 1/20 scale model to validate the predicted scheduling laws. Good agreements have been obtained compared with the results of high speed wind tunnel test. Based on the results obtained from the experimental and numerical studies, the corrected supersonic panel method has shown to be useful to establish the canard-leading edge flap deflection scheduling law for the aerodynamic design of canard type fighter class aircraft.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.26 no.4
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• pp.309-318
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• 2013

Abutment-to-pile connection in an integral abutment bridge is vulnerable to lateral displacement induced by thermal movement of the superstructure. However, previous researches have merely focused on the connection. In order to improve the performance of the connection, new abutment-to-pile connection designs were proposed based on quasi-static nonlinear finite element model. The reinforcement detail specified in PennDOT DM4 and HSS tube were barely effective in controlling crack growing but spiral rebar effectively performed to delay crack growth as well as absorbing energy capacity. However, it was found that delaying cracking and strengthening the connection also caused the high lateral load in superstructures. Consequently, shape of HP pile were modified to introduce plastic hinge of the HP pile for reducing the lateral load in superstructures. Connections with modified HP pile significantly prevented crack propagations under the lateral displacement.

• Journal of the Korean Geotechnical Society
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• v.20 no.8
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• pp.193-203
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• 2004

Arching effects in backfill materials generate a nonlinear active earth pressure distribution on a rigid retaining wall with rough face, and arching effects on the shape of the nonlinear earth pressure distribution depends on the mode of wall movement. Therefore, the practical shape of failure surface and arching effect in the backfill changed with the mode of wall movement must be considered to calculate accurate magnitude and distribution of active earth pressure on the rigid wall. In this study, a new formulation for calculating the active earth pressure on a rough rigid retaining wall rotating about the base is proposed by considering the shape of nonlinear failure surface and arching effects in the backfill. In order to avoid mathematical complexities in the calculation of active earth pressure, the imaginary failure surface composed of four linear surfaces is used instead of the nonlinear failure surface as failure surface of backfills. The comparisons between predictions from the proposed equations and existing model test results show that the proposed equations produce satisfactory predictions.