• Title/Summary/Keyword: 무요소 해석법

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An Improved Method for Initial Shape Analysis of Cable-Stayed Bridges (사장교의 개선된 초기형상 해석법)

  • Kim, Moon Young;Kyung, Yong Soo;Lee, Jun Sok
    • Journal of Korean Society of Steel Construction
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    • v.15 no.2
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    • pp.175-185
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    • 2003
  • The extended tangent stiffness matrices and force-deformation relations of the elastic catenary element were initially derived through the addition of the unstrained length of cables to unknown nodal displacements. A beam-column element was then introduced to model the deck and pylon of cable-stayed bridges. The conventional geometric nonlinear analysis, initial force method, and TCUD method were summarized, with an effective method combining two methods presented to determine the initial shapes of cable-stayed bridges with dead loads. In this combined method, TCUD method was applied to eliminate vertical and horizontal displacements at cable-supported points of decks and on top of pylons, respectively. The initial force method was also adopted to eliminate horizontal and vertical displacements of decks and pylons, Finally, the accuracy and validity of the proposed combined method were demonstrated through numerical examples.

A Study of 50W High Speed BLDC Motor for Air Blower Drive (에어 블로워 구동용 50W급 고속 BLDC 모터에 관한 연구)

  • Baek, Chan-Wook;Seo, Jung-Moo;Yoo, Ji-Yoon;Jung, In-Soung
    • Proceedings of the KIEE Conference
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    • 2006.10d
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    • pp.110-112
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    • 2006
  • 본 연구는 소형, 고효율 3kW급 고분자 전해질 연료공급 모듈용 에어블로워 개발에 있어 필수요소인 BLDC형 블로워 모터에 관한 것이다. 에어블로워의 목표출력(50W)에 최적화된 BLDC모터를 설계하기위하여 등가자기회로법과 유한요소법을 이용하였고, 모터를 제작하여 해석결과와 비교 검증하였다.

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Fatigue Life Evaluation in Frequency Domain of aircraft Equipment Exposed to Random Vibration (무작위 진동에 노출된 항공기 탑재 장비의 주파수영역 피로수명 평가)

  • Jung, Hyun Su;Kim, Ki Seung;Kim, Jun Su;Lee, Seong Woo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.8
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    • pp.627-638
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    • 2017
  • Expecting fatigue life of mounted radar in aircraft is very important when designing, because the mounted radar in aircraft is exposed to long-term external random vibration. Among the methods of predicting the fatigue life, Fatigue analysis method in frequency domain has continuously been proposed in this field. In this paper, four fatigue analysis methods in frequency domain, which are widely used, have been selected and compared with the results for Specimen fatigue test. As a result, Dirlik and Benascicutti-Tovo methods have been matched better with fatigue analysis in time domain than the method in frequency method through the comparison between the fatigue analysis method in time domain and the method in frequency domain by conducting the specimen fatigue test with strain gage. Based on the results of the specimen fatigue test, We have conducted fatigue analysis of mounted radar in aircraft with Dirlik and Benasciutti-Tovo methods in the finite element model, and confirmed that the required life was satisfying.

Finite-EIement Analysis with Localized Functional for Alternating Magnetic Field Problems (국부범함수를 사용한 교류자장 문제의 유한요소 해석)

  • 김원범;정현교;고창섭;한송엽
    • Journal of the Korean Magnetics Society
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    • v.1 no.2
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    • pp.79-84
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    • 1991
  • A variational approach employing localized functional is presented to solve alternating magnetic field problems with open boundary. The functional used in the approach consists of the domain integral of finite element region only and the boundary integral of the interfacial boundary between the finite and infinite element regions. The boundary integral is obtained by transforming the infinite domain integral for the infinite element region into the interfacial boundary integral. The proposed algorithm is then applied to a simple two-dimensional problem where the analytic solutions are available. It is shown that the algorithm makes it possible to yield good agreements between the numerical and analytic solutions. and that it requires less computer storage memory and computation time than the conventional finite element method due to the reduction of the computing region.

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실험계획법을 이용한 선형 모터의 최적 설계

  • 설진수;임경화
    • Proceedings of the Korean Society Of Semiconductor Equipment Technology
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    • 2005.09a
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    • pp.188-192
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    • 2005
  • 나노 구동용 선형 모터는 이송체의 구동에 따른 진동과 열 특성으로 인하여 발생되는 기구간의 진동과 기계적인 마찰력 변화로 나노위치제어에 어려움이 있다. 그러므로 이송체에 대한 진동과 열에 대한 분석이 필요하다. 본 논문에서는 개발된 선형 모터의 이송체를 무부하 상태에서 유한 요소 해석을 통해 진동 특성을 분석하고 실험계획법을 적용하여 이송체에 대하여 최적화된 설계 방향을 제시하고자 한다. 또한 이송체의 진동 특성을 고려한 경량화를 통해 선형 모터의 안정된 구동을 모색하고자 한다.

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An Improved Initial Force Method for Determining the Initial Configuration of Suspension Bridges (현수교 시스템의 초기형상 결정을 위한 개선된 초기부재력법)

  • Kim, Min;Kim, Ho-Kyung;Kim, Moon-Young
    • Journal of Korean Society of Steel Construction
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    • v.23 no.2
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    • pp.237-247
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    • 2011
  • This paper presents an improved initial force method for determining the initial shape of suspension bridges. After determining the initial shape factors through the force equilibrium conditions of each hanging point, the initial force method was applied with the computed values, each node's coordinates, and unstrained lengths of the cable element as inputs. The unstrained length of each cable element was regarded as a fixed value in each iteration step, unlike in the typical initial force method. This method can be applied to 2D and 3D suspension bridge models. The validity of the present method was demonstrated by comparing the results of the numerical examples.

Development of Meshless Method for Free Vibration Analysis of Arbitrarily Shaped Free Plates Using Local Polar Coordinates (지역 극좌표계를 이용한 임의 형상 자유단 평판의 자유진동해석을 위한 무요소법 개발)

  • Kang, Sang-Wook;Atluri, S. N.
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.18 no.6
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    • pp.674-680
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    • 2008
  • A new meshless method for obtaining natural frequencies of arbitrarily shaped plates with the free boundary condition is introduced in the paper. In order to improve the characteristics of convergence and accuracy of the method, a special local polar coordinates system is devised and located for each of nodes distributed along the boundary of the plate of interest. In addition, a new way of decreasing the size of the system matrix that gives natural frequencies of the plate is employed to reduce the amount of numerical calculations, which is needed for computing the determinant of the system matrix. Finally the excellence of the characteristics of convergence and accuracy of the method is shown in several case studies, which indicate that natural frequencies by the proposed method are very accurate and converged swiftly to exact values as the number of boundary nodes increases.

Critical Speed Analysis of the Turbopump considering the Casing Structural Flexibility (케이징 구조 유연성을 고려한 터보펌프 임계 속도 해석)

  • 전성민;김진한;곽현덕;윤석환
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.6
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    • pp.92-97
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    • 2006
  • A critical speed analysis is performed for a 30 ton thrust turbopump considering the casing structural flexibility. A full three-dimensional finite element method including rotor and casing is used to predict rotordynamic behavior. Rotor alone model and rotor-casing coupled model with fixed-fixed and free-free boundary conditions are calculated to investigate the effects of the casing structural flexibility. The stiffness of ball bearings are applied as unloaded and loaded values to consider rotor operating conditions in vacuum and real engine respectively. From the results of the numerical analyses, it is found that the effect of the casing structural flexibility reduces the critical speeds of the turbopump. Especially, the loaded rotor condition with higher bearing stiffness is affected dramatically rather than the unloaded rotor condition with lower bearing stiffness.

Global Sensitivity Analysis of Joints for Plug-in Digital Framework (플러그인 디지털 프레임웍을 위한 연결부 전역민감도 해석)

  • Lee, Dooho;Won, Young-Woo;Kwon, Jong-Hyun
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.40 no.5
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    • pp.483-488
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    • 2016
  • Plug-In Digital Framework is a system response analysis tool that is employed when system components are composed of black-box modules. Generally, the dynamic characteristics of joints between the system components significantly affect system responses, and they lead to displacement- and frequency-dependent stiffness and loss factor. Thus, the sensitivity of each joint parameters should be estimated from a global perspective. In this study, we introduce a global sensitivity analysis procedure under the Plug-In Digital Framework. To efficiently calculate the system responses, we introduce the frequency response function (FRF)-based substructuring method. Using the random balance designs (RBD), we generate the system responses and estimate the global first-order sensitivities for each joint stiffness. We apply the proposed global sensitivity analysis method to an interior noise problem of a passenger car, and we evaluate the efficiency of the global sensitivity analysis method.

항공기용 ACM(Air Cycle Machine) 설계 및 공력성능시험

  • 현용익;김진한;김춘택;차봉준;이대성;김승우;천익정
    • 유체기계공업학회:학술대회논문집
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    • 1997.02a
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    • pp.58-73
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    • 1997
  • 본 연구는 항공기용 환경제어계통의 시스템관련 제반 기술 및 그 핵심요소인 ACM(Air Cycle Machine)시제기의 개발을 통하여 국내의 여런 항공기개발 사업과 관련하여 급속히 요구되고 있는 항공기의 sub-system을 국산화할 수 있는 기술축적을 목적으로 수행되었다. 본 연구에서는 항공기용 환경제어장치(Environmental Control System : ECS)를 개발대상으로 하여 그 핵심부품인 Air Cycle Machine의 시제품을 순수 국내 기술로 설계/제작하였고, 자체 개발한 성능시험기를 이용하여 성능시험을 수행하였으며 또한 ACM 성능을 검증하기 위하여 기존제품의 자료와 비교하였다. 향후 이 시스템의 상품화를 위해서는 구동축의 무윤활 베어링에 대한 연구가 병행되어 주유동의 오일오염을 국소화시키는 시스템보완이 요구된다. 항공기용 환경제어장치(ECS)의 시스템해석부터 ACM의 공력/구조설계, 제작, 시험등 일련의 개발과정을 통하여 시스템에 대한 해석능력이 향상되었고, 그 핵심요소인 ACM의 순수 국산화개발이 가능하다는 판단을 내릴 수 있었다. 또한, ACM을 구성하고 있는 원심압축기와 반경류형 터빈의 제작 및 시험법은 유사 시스템 및 일반 터보기계류의 국산화개발에 유용하게 이용될 것으로 기대된다.

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