• 한국지반환경공학회 논문집
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• 제15권9호
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• pp.47-58
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• 2014

본 연구에서는 해상풍력발전시스템(NREL 5 MW) 하중해석을 위해 필요한 기초구조물과 해저지반간의 상호작용 모델링 방안을 모색하고, 해상풍력시스템 해석프로그램인 GH-Bladed를 활용하여 하중해석을 수행함으로 지반모델링 방법과 설계하중조건에 따른 기초구조물 설계하중을 비교 분석하였다. 또한 상기 하중해석 결과를 기초구조물 해석프로그램 L-Pile에 적용하여 기초구조물 단면에 대한 안정성 검토를 수행하였다. 본 논문에서 정리한 기초구조물 모델링 방법인 고정단, winkler spring, coupled spring 모델과 설계하중조건 DLC 1.3, DLC 6.1a, DLC 6.2a의 해석결과를 바탕으로 모노파일의 단면변화를 관찰하였다. 그 결과 모든 설계하중조건에서 고정단, coupled spring 모델의 경우 모노파일의 단면이 직경 7 m, 두께 80 mm로 산정되었으며, winkler spring 모델을 적용하여 해석을 수행한 결과 모노파일의 단면이 직경 5 m, 두께 60 mm로 산정되었다. 본 연구를 통해 지반-기초구조물간의 상호작용 모델링 방법이 기초구조물의 설계 단면을 결정하는 하중해석 결과에 영향을 미친다는 것을 파악하였으며, 이러한 영향을 고려하여 해상풍력시스템 기초구조물을 설계한다면 기초구조물 설계 시 발생할 수 있는 과다 과소설계 가능성을 최소화할 수 있을 것으로 기대된다.

• 한국지반공학회논문집
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• 제26권7호
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• pp.17-24
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• 2010

기초구조물의 설계에 있어 전세계적으로 하중저항계수설계법(LRFD)이 확산되는 추세이다. 현재 국내의 현장타설 말뚝 설계에 있어 AASHTO(2007)에서 제안한 저항계수를 이용하고 있지만, 이는 미국 내 분포하는 무결암에 대한 저항계수이며 지역적 가변성이 큰 저항계수의 특성상 국내 암반에 적용하기에 부적합하다. 따라서 본 연구에서는 국내에서 수행된 재하시험 자료를 이용하여 국내 지반에 적합한 저항계수를 산정하였다. 측정지지력 확인이 가능한 8개 현장의 재하시험 결과 중 22개의 자료를 이용하여 4가지의 지지력 공식에 대한 저항편향계수를 산정하였으며, 이를 이용하여 신뢰성분석을 수행하였다. 그 결과 현장타설말뚝의 안전율이 3.0일 때 목표 신뢰도지수는 약 2.01~2.30 으로 산정되었다. 또한 최적화를 이용하여 저항계수 및 하중계수를 산정한 결과 저항계수는 약 0.48~0.56, 사하 중계수는 약 1.25, 활하중 계수는 약 1.75로 산정되었다. 하지만 목표 신뢰도지수를 AASHTO에서 제안한 3.0을 이용하여 저항계수를 산정하면 목표 신뢰도지수 2.0을 적용하였을 때 산정한 저항계수의 약 50% 값을 가진다.

• 동력기계공학회지
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• 제7권1호
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• pp.34-41
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• 2003

A method is presented for generating the path which significantly reduces residual vibration of a flexible robot manipulator and applying control theory to track the desired path. The desired path is optimally designed so that the system completes the required move with minimum residual vibration. A closed loop control theory is applied to track the planned path in the case of load variation. Specifically, it is desired that the optimally designed path has a better trajectory tracking capabilities during the residual vibration over the cycloidal path, in various cases of load. Perturbation adaptive control is used as closed loop control scheme. A planar two link manipulator is used to evaluate this method.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1999년도 봄 학술발표회 논문집
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• pp.252-259
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• 1999

One of the most important factors for a proper design of a slender compression member may be the exact determination of the elastic critical load of that member. In the cases of non-prismatic compression member, however, there are times when the exact critical load becomes impossible to determinate if one relies on the neutral equilibrium method or energy principle. Here in this paper, the approximate critical loads of symmetrically or non-symmetrically tapered members are computed by finite element method. The two parameters considered in this numerical analysis are the taper parameter, $\alpha$ and the sectional property parameters, m. The computed results for each sectional property parameter, m are presented in an algebraic equation which agrees with those by F.E.M The algebraic equation can be easily used by structural engineers, who are engaged in structural analysis and design of non-prismatic compression member.

• 한국지진공학회:학술대회논문집
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• 한국지진공학회 2001년도 추계 학술발표회 논문집 Proceedings of EESK Conference-Fall 2001
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• pp.268-275
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• 2001

Modal analysis does well predict the elastic dynamic response of the torsionally unbalanced structure. But modal analysis overestimates the rotation of the structure in inelastic range, so one side members require ductility too much and the others require ductility too small in comparison with torsionally balanced structure. In this paper, in order to reduce difference of ductility demand between both side members of the torsionally unbalanced structure, design eccentricity of seismic load is evaluated and the method determining the strength center of structure is proposed using modal analysis. For several cases, the ductility demand of stucture is compared to investigate the propriety of the proposed approach.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2007년도 추계학술대회 논문집
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• pp.349-352
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• 2007

A GFRP based composite blade was developed for a 2MW wind energy conversion system of type class IIA. The blade sectional geometry was designed to have a general shell-spar and shear web structure. The load cases specified in the IEC61400-1 international specification were considered. For withstanding all relevant extreme loads, the structural analysis for the complete blade was performed using a commercial FEM code. The static load carrying capacity, blade tip deflection and natural frequencies were evaluated to satisfy the strength and stability requirements in accordance with the IEC61400-1 and GL Regulations. The prototype blade was passed the structural proof test for GL certification.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집A
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• pp.752-757
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• 2001

To reduce stress concentration around the intersection between a spherical pressure vessel and a cylindrical nozzle under various load conditions using less material, the optimization for the distribution of reinforcement has researched. The ranked bidirectional evolutionary structural optimization(R-BESO) method is developed recently, which adds elements based on a rank, and the performance indicator which can estimate a fully stressed model. The R-BESO method can obtain the optimum design using less iteration number than iteration number of the BESO. In this paper, the optimized intersection shape is sought using R-BESO method for a flush and a protruding nozzle. The considered load cases are a radial compression, torque and shear force.

• Advances in Computational Design
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• 제1권2호
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• pp.155-173
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• 2016

This paper presents a method of design for the energy harvesting of a piezoelectric cantilever beam. Vibration modes have strain nodes where the strain distribution changes in the direction of the beam length. Covering the strain nodes of the vibration modes with continuous electrodes effects a cancellation of the voltages outputs. The use of segmented electrodes avoids cancellations of the voltage for multi-mode vibration. The resistive load affects the voltage and generated power. The optimum resistive load is considered for segmented and continuous electrodes, and then the power output is verified. One of the effective parameters on energy harvesting performance is the existence of concentrated mass. This topic is studied in this paper. Resonance and off-resonance cases are considered for the harvester. In this paper, both theoretical and experimental methods are used for satisfactory results.

• 항공우주시스템공학회지
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• 제2권2호
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• pp.1-7
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• 2008

Recently the wind energy has been alternatively used as a renewable energy resource instead of the mostly used fossil fuel due to its lack and environmental issues. This work is to propose a structural design and analysis procedure for development of the low noise 100W class small wind turbine system which will be applicable to relatively low speed region like Korea and for the domestic use. Structural analysis including load cases, stress, deformation, buckling, vibration and fatigue life was performed using the Finite Element Method, the load spectrum analysis and the Miner rule. In order to evaluate the designed structure, the structural test was carried out and its test results were compared with the estimated results. In addition, the blade should be safe from the impact damage due to FOD(Foreign Object Damage) including the bird strike. In order to analize the bird strike penomena on the blade, MSC. Dytran was used, and the applied method Arbitrary Lagrangian-Eulerian was evalud by comparison with the previous study results.

• International Journal of Aerospace System Engineering
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• 제2권1호
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• pp.38-42
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• 2015

This work is to propose a structural design and analysis procedure for development of the low noise 1kW class small wind turbine system which will be applicable to relatively low speed region like Korea and for the domestic use. The proposed structural configuration has a sandwich composite structure with the E-glass/Epoxy face sheets and the Urethane foam core for lightness, structural stability, low manufacturing cost and easy manufacturing process. Structural analysis including load cases, stress, deformation, buckling, vibration and fatigue life was performed using the Finite Element Method, the load spectrum analysis and Miner rule. In order to evaluate the designed structure, the structural test was carried out and its test results were compared with the estimated results. Moreover Investigation on structural safety of tower was verified through structural analysis by FEM.