• 한국항공우주학회지
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• 제42권5호
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• pp.390-397
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• 2014

BO-105 헬리콥터는 무힌지 로터 허브시스템이 적용되었으며, 블레이드의 루트 영역이 무힌지 허브 시스템의 플렉셔에 해당한다. 따라서 본 블레이드를 이용한 훨타워 시험 수행을 대비하여 굽힘 강성이 낮은 플렉셔 부분에 대한 굽힘 강성 보강을 수행하였다. 플렉셔 굽힘 강성 보강 수행을 위해 플렉셔 부분의 단면 형상을 모델링하여 굽힘 강성을 계산하였으며, 이를 바탕으로 강성 보강을 위한 복합재의 두께를 선정하였다. 보강된 플렉셔의 실제 굽힘 강성을 확인하기 위하여 강성보강 전 형상에 대한 강성 측정 시험과 강성보강 이후 형상에 대한 강성 측정 시험을 수행하여 결과를 비교하였다.

• 한국정밀공학회지
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• 제26권8호
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• pp.79-88
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• 2009

This paper presents the analytical stiffness analysis method for a low-DOF planar parallel manipulator. An n-DOF (n<3) planar parallel manipulator to which 1- or 2-DOF serial mechanism is connected in series may be used as a positioning device in planar tasks requring high payload and high speed. Differently from a 3-DOF planar parallel manipulator, an n-DOF planar parallel counterpart may be subject to constraint forces as well as actuation forces. Using the theory of reciprocal screws, the planar stiffness is modeled such that the moving platform is supported by three springs related to the reciprocal screws of actuations (n) and constraints (3-n). Then, the spring constants can be precisely determined by modeling the compliances of joints and links in serial chains. Finally, the stiffness of two kinds of 2-DOF planar parallel manipulators with simple and complex springs is analyzed. In order to show the effectiveness of the suggested method, the results of analytical stiffness analysis are compared to those of numerical stiffness analysis by using ADAMS.

• 동력기계공학회지
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• 제21권6호
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• pp.40-45
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• 2017

The objective of this study is the finite element-transfer stiffness coefficient method, which is the combination of the modeling technique of finite element method and the transfer technique of transfer stiffness coefficient method, is applied in the static analyses of two dimensional curved beam structures. To confirm the effectiveness of the applied method, two computational models are selected and analyzed by using finite element method, finite element-transfer stiffness coefficient method and exact solution. The computational results of the static analyses for two computational models using finite element-transfer stiffness coefficient method are equal to those using finite element method. When the element partition number of curved beam structure is increased, the computational results of the static analyses using both methods approach the exact solution. We confirmed that the finite element-transfer stiffness coefficient method is superior to finite element method when the number of the curved beam elements is increased from the viewpoints of the computational speed and the utility of computer memory.

• 한국소음진동공학회논문집
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• 제18권1호
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• pp.110-122
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• 2008

Pneumatic vibration isolator typically consisting of dual-chamber pneumatic springs and a rigid table are widely employed for proper operation of precision instruments such as optical devices or nano-scale equipments owing to their low stiffness- and high damping-characteristics. As environmental vibration regulations for precision instruments become more stringent, it is required to improve further the isolation performance. In order to facilitate their design optimization or active control, a more accurate mathematical model or complex stiffness is needed. Experimental results we obtained rigorously for a dual-chamber pneumatic spring exhibit significantly amplitude dependent behavior, which cannot be described by linear models in earlier researches. In this paper, an improvement for the complex stiffness model is presented by taking two major considerations. One is to consider the amplitude dependent complex stiffness of diaphragm necessarily employed for prevention of air leakage. The other is to employ a nonlinear model for the air flow in capillary tube connecting the two pneumatic chambers. The proposed amplitude-dependent complex stiffness model which reflects dependency on both frequency and excitation amplitude is shown to be very valid by comparison with the experimental measurements. Such an accurate nonlinear model for the dual-chamber pneumatic springs would contribute to more effective design or control of vibration isolation systems.

• 한국전산구조공학회논문집
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• 제21권1호
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• pp.1-11
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• 2008

전단빌딩에 발생한 손상 추정에 있어서 대상 구조물의 물성치를 가정하고 이상화한 모델을 이용한 역해석이 필요하다. 강성행렬을 이용하는 고전적인 손상추정 방법에 비해 유연도 행렬을 이용한 손상추정은 구조물의 저차모드를 이용하기 때문에 비교적 정확한 값을 계산할 수 있기 때문에 더 효과적으로 알려져 있다. 이 논문에서는 손상추정을 위한 알고리즘으로 유전자 알고리즘(Genetic Algorithm, GA)을 도입하였고, 구조 응답에서 취득할 수 있는 유연도 행렬을 이용하여 역해석을 통한 손상추정 기법을 소개하고 있다. 제안된 손상추정 기법은 전단빌딩의 강성에 대한 정확한 정보가 없는 상황에서 전단빌딩의 손상으로 인한 실제 강성변화량을 추정하도록 하였다. 더불어 open source code인 OPENSEES를 이용하여 전단빌딩 수치해석을 통해 제안된 손상추정 기법의 효율성을 검증하였다.

• 한국정밀공학회지
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• 제29권10호
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• pp.1070-1077
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• 2012

Virtual machine tools have been magnified recently as manufacturers could estimate performances of machine tools before design and manufacturing of them. However, it requires much time and efforts to make FEM models and predict precision of machine tools well because machine tools are composed of many joints such as bolt joints, LM joints, rotational bearing joints and mounts. Especially, we have studied computational modeling methods of bolt joints to predict precision of machine tools well in this paper. Stiffness and damping coefficients of bolt joints are investigated and generalized with respect to fasten forces through experiments and FEM analysis. Matrix 27 element of ANSYS is used and bolt joints are simplified as square areas with 8 nodes to apply stiffness and damping simultaneously. Additionally, coordinate transformation of matrix 27 for bolt joints is induced to apply to skewed bolt joints of machine tools and evaluate it using FEM analysis.

• 한국지반공학회논문집
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• 제21권5호
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• pp.15-24
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• 2005

본 논문에서는 교량 말뚝기초의 모델링기법에 관한분류 및 단부 지점조건의 영향을 분석하였다. 연성스프링 방법은 모델링 형태가 간편하면서도 복잡한 군말뚝 거동을 효과적으로 나타낼 수 있으므로 실제 설계에 유용한 방법이다. 다양한 말뚝 배열, 말뚝 간격, 선단지지조건, 그리고 하중크기에 따라 3차원 해석기법(YSGroup)을 통해 영향인자 분석을 수행하였으며, 그 결과 횡방향 변위, 최대 말뚝 휨응력, 그리고 군말뚝의 횡방향 스프링강성을 산정, 이를 비교$\cdot$분석하였다. 영향인자 분석을 통해 3차원 해석기법(YSGroup)을 통해 횡방향 스프링강성을 산정한 경우는 다른 단독말뚝 해석을 통해 산정한 경우에 비하여 복잡한 군말뚝 거동을 보다 적절히 예측함을 알 수 있었다.

• Structural Engineering and Mechanics
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• 제26권3호
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• pp.343-361
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• 2007

This article presents a numerical tool for dimensioning two-threaded fasteners connecting prismatic parts subjected to fatigue tension loads that are coplanar with the screw axis. A simplified numerical model is developed from unidirectional finite elements, modeling the connected parts and screws with bent elements and the elastic contact layer between the parts with springs. An algorithm updating the contact stiffness matrix, calculating forces and displacements at each node of the structure and thus normal stresses in the screws in both static and fatigue is further developed using C language. An experimental study is also conducted in parallel with the numerical approach to validate the developed model assumptions, the numerical model and the 3D finite element results. Since stiffness values for the compressive zones in the parts are analytically difficult to determine, a statistical software method is used, from which a tuning factor is derived for identifying these stiffness values. The method is also applied to set out the influence of each parameter on the fatigue behaviour of each screw. Finally, the developed model will be used to establish a new, sophisticated, fast and accurate tool for dimensioning bolted mechanical structures.

• Earthquakes and Structures
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• 제9권5호
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• pp.957-981
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• 2015

Earthquakes occur as a cluster in many regions around the world where complex fault systems exist. The repeated shaking usually induces accumulative damage to affected structures. Damage accumulation in structural systems increases their level of degradation in stiffness and also reduces their strength. Many existing analytical tools of modeling RC structures lack the salient damage features that account for stiffness and strength degradation resulting from repeated earthquake loading. Therefore, these tools are inadequate to study the response of structures in regions prone to multiple earthquakes hazard. The objective of this paper is twofold: (a) develop a tool that contains appropriate damage features for the numerical analysis of RC structures subjected to more than one earthquake; and (b) conduct a parametric study that investigates the effects of multiple earthquakes on the response of RC moment resisting frame systems. For this purpose, macroscopic constitutive models of concrete and steel materials that contain the aforementioned damage features and are capable of accurately capturing materials degrading behavior, are selected and implemented into fiber-based finite element software. Furthermore, finite element models that utilize the implemented concrete and steel stress-strain hysteresis are developed. The models are then subjected to selected sets of earthquake sequences. The results presented in this study clearly indicate that the response of degrading structural systems is appreciably influenced by strong-motion sequences in a manner that cannot be predicted from simple analysis. It also confirms that the effects of multiple earthquakes on earthquake safety can be very considerable.

• Structural Engineering and Mechanics
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• 제27권2호
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• pp.199-222
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• 2007

Composite laminated structures supported on elastic foundations are being increasingly used in a great variety of engineering applications. Composites exhibit larger dispersion in their material properties compared to the conventional materials due to large number of parameters associated with their manufacturing and fabrication processes. And also the dispersion in elastic foundation stiffness parameter is inherent due to inaccurate modeling and determination of elastic foundation properties in practice. For a better modeling of the material properties and foundation, these are treated as random variables. This paper deals with effects of randomness in material properties and foundation stiffness parameters on the free vibration response of laminated composite plate resting on an elastic foundation. A $C^0$ finite element method has been used for arriving at an eigen value problem. Higher order shear deformation theory has been used to model the displacement field. A mean centered first order perturbation technique has been employed to handle randomness in system properties for obtaining the stochastic characteristic of frequency response. It is observed that small amount of variations in random material properties and foundation stiffness parameters significantly affect the free vibration response of the laminated composite plate. The results have been compared with those available in the literature and an independent Monte Carlo simulation.