• 제목/요약/키워드: Load Transient Response

검색결과 226건 처리시간 0.026초

Elastic Wave Propagation in Monoclinic System Due to Transient Line Load

  • Kim, Yong-Yun
    • The Journal of the Acoustical Society of Korea
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    • 제17권2E호
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    • pp.53-58
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    • 1998
  • In this paper, we study the response of several anisotropic systems to buried transient line loads. The problem is mathematically formulated based on the equations of motion in the constitutive relations. The load is in form of a normal stress acting with arbitrary axis on the plane of monoclinic symmetry. Plane wave equation is coupled with vertical shear wave, longitudinal wave and horizontal shear wave. We first considered the equation of motion in reference coordinate system, where the line load is coincident with symmetry axis of the orthotrioic material. Then the equation of motion is transformed with respect to general coordiante system with azimuthal angle by using transformation tensor. The load is first described as a body force in the equations of the motion for the infinite media and then it is mathematically characterized. Subsequently the results for semi-infinite spaces is also obtained by using superposition of the infinite medium solution together with a scattered solution from the free surface. Consequently explicit solutions for the displacements are obtained by using Cargniard-DeHoop contour. Numerical results which are drawn from concrete examples of orthotropic material belonging to monoclinic symmetry are demonstrated.

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Bounds on plastic strains for elastic plastic structures in plastic shakedown conditions

  • Giambanco, Francesco;Palizzolo, Luigi;Caffarelli, Alessandra
    • Structural Engineering and Mechanics
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    • 제25권1호
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    • pp.107-126
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    • 2007
  • The problem related to the computation of bounds on plastic deformations for structures in plastic shakedown condition (alternating plasticity) is studied. In particular, reference is made to structures discretized by finite elements constituted by elastic perfectly plastic material and subjected to a special combination of fixed and cyclic loads. The load history is known during the steady-state phase, but it is unknown during the previous transient phase; so, as a consequence, it is not possible to know the complete elastic plastic structural response. The interest is therefore focused on the computation of bounds on suitable measures of the plastic strain which characterizes just the first transient phase of the structural response, whatever the real load history is applied. A suitable structural model is introduced, useful to describe the elastic plastic behaviour of the structure in the relevant shakedown conditions. A special bounding theorem based on a perturbation method is proposed and proved. Such theorem allows us to compute bounds on any chosen measure of the relevant plastic deformation occurring at the end of the transient phase for the structure in plastic shakedown; it represents a generalization of analogous bounding theorems related to the elastic shakedown. Some numerical applications devoted to a plane steel structure are effected and discussed.

자이로콥터의 동적 유한요소모델링 및 구조진동해석 (Dynamic Finite Element Modeling and Structural Vibration Analysis of a Gyrocopter)

  • 정세운;양용준;김현정;제상언;조태환;김동현
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2005년도 춘계학술대회논문집
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    • pp.813-820
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    • 2005
  • In this study, finite element modeling and structural vibration analyses of a gyrocopter have been conducted considering dynamic hub-loads due to rotating blades. For this research, 3D CATIA models for most mechanical parts are exactly prepared and assembled into the final aircraft configuration. Then the dynamic finite element model including several non-structural parts are constructed based on the exact 3D CAD data. Computational structural dynamics technique based on finite element method is applied using both MSC/NASTRAN and developed in-house code which can largely reduce the pre and postprocessing time of general transient dynamic analyses. Modal based transient and frequency response analyses are used to efficiently investigate vibration characteristics. The results include natural frequency comparison for different fuel and pilot conditions, fundamental natural mode shapes, frequency responses and transient acceleration responses of the present gyrocopter model.

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Modeling, Dynamic Analysis and Control Design of Full-Bridge LLC Resonant Converters with Sliding-Mode and PI Control Scheme

  • Zheng, Kai;Zhang, Guodong;Zhou, Dongfang;Li, Jianbing;Yin, Shaofeng
    • Journal of Power Electronics
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    • 제18권3호
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    • pp.766-777
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    • 2018
  • In this paper, a sliding mode and proportional plus integral (SM-PI) control combined with self-sustained phase shift modulation (SSPSM) for LLC resonant converters is presented. The proposed control scheme improves the transient response while preserving good steady-state performance. An averaged large signal model of an LLC converter with the ZVS modulation technique is developed for the SM control design. The sliding surface is obtained based on the input-output linearization concept. A system identification method is adopted to obtain the transform function of the LLC resonant converter, which is used to design the PI control. In order to reduce the inherent chattering problem in the steady state, the combined SM-PI control strategy is derived with fuzzy control, where the SM control is responsive during the transient state while the PI control prevails in the steady state. The combination of SSPSM and the SM-PI control provides ZVS operation, robustness and a fast transient response against step load variations. Simulation and experimental results validate the theoretical analysis and the attractive features of the proposed scheme.

Transient vibration analysis of FG-MWCNT reinforced composite plate resting on foundation

  • Kumar, Puneet;Srinivas, J.
    • Steel and Composite Structures
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    • 제29권5호
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    • pp.569-578
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    • 2018
  • This paper aims to investigate the transient vibration behavior of functionally graded carbon nanotube (FG-CNT) reinforced nanocomposite plate resting on Pasternak foundation under pulse excitation. The plate is considered to be composed of matrix material and multi-walled carbon nanotubes (MWCNTs) with distribution as per the functional grading concept. The functionally graded distribution patterns in nanocomposite plate are explained more appropriately with the layer-wise variation of carbon nanotubes weight fraction in the thickness coordinate. The layers are stacked up in such a way that it yields uniform and three other types of distribution patterns. The effective material properties of each layer in nanocomposite plate are obtained by modified Halpin-Tsai model and rule of mixtures. The governing equations of an illustrative case of simply-supported nanocomposite plate resting on the Pasternak foundation are derived from third order shear deformation theory and Navier's solution technique. A converge transient response of nanocompiste plate under uniformly distributed load with triangular pulse is obtained by varying number of layer in thickness direction. The validity and accuracy of the present model is also checked by comparing the results with those available in literature for isotropic case. Then, numerical examples are presented to highlight the effects of distribution patterns, foundation stiffness, carbon nanotube parameters and plate aspect ratio on the central deflection response. The results are extended with the consideration of proportional damping in the system and found that nanocomposite plate with distribution III have minimum settling time as compared to the other distributions.

연성하중해석 모델과 모달과도해석을 이용한 위성체 구조부재의 최적화 연구 (A Study on the Optimization of a Spacecraft Structure by Using Coupled Load Analysis Model and Modal Transient Analysis)

  • 황도순;이영신;김인걸
    • 한국항공우주학회지
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    • 제32권6호
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    • pp.34-48
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    • 2004
  • 본 연구에서는 대형 구조물의 최적설계에서 문제되는 많은 계산시간과 컴퓨터의 계산능력을 최소화할 수 있도록 부분구조합성법의 하나인 구속모드법을 이용한 연성하중해석 모델 및 모달과도해석을 포함한 최적화 절차를 제시하였다. 제안된 방법의 수치모사를 위한 프로그램을 개발하여 위성체 주요 구조부재인 플랫폼에 대한 최적화를 수행함으로써 그 타당성을 검증하였다. 제안된 기법을 통해 초기설계 단계에서 정확성을 유지하면서 계산시간을 단축할 수 있었고 위성체 구조부재에 대한 최적화를 수행하여 각각의 구조부재에 대한 특성을 파악함으로써 설계 활용방안을 제시하였다.

퍼지 제어기를 이용한 병렬 PWM 컨버터의 과도응답특성 개선 (Improvement of Dynamic Response Characteristics of Parallel PWM Converters Using Fuzzy Logic Controller)

  • 민병권;김이훈;김재문;원충연;김규식;최세완
    • 전력전자학회논문지
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    • 제7권3호
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    • pp.303-312
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    • 2002
  • 본 논문에서는 병렬 운전 PWM 컨버터의 고성능 제어를 위하여 우수한 성능을 나타내는 퍼지 제어기를 제안하고 구현하였으며, 제안된 고성능 퍼지 제어기와 Pl 제어기와의 특성 비교를 위하여 PI 제어기도 구현하였다. 시뮬레이션과 실험 결과를 통하여, 특히 부하 급변시 병렬 PWM 컨버터의 U전압 과도응답 특성과 전류제어 과도응답 특성이 기존의 PI 제어기에 비해 제안된 퍼지 제어기가 우수한 특성을 나타내고 있음을 확인하였다. 제안된 퍼지 제어기의 우수한 특성을 입증하고 실제 제품에 적용하기 위하여 7.5kW PWM 컨버터 2대를 병렬 연결한 15kW PWM 컨버터를 구현하고 실험하였다.

An FPGA-Based Modified Adaptive PID Controller for DC/DC Buck Converters

  • Lv, Ling;Chang, Changyuan;Zhou, Zhiqi;Yuan, Yubo
    • Journal of Power Electronics
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    • 제15권2호
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    • pp.346-355
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    • 2015
  • On the basis of the conventional PID control algorithm, a modified adaptive PID (MA-PID) control algorithm is presented to improve the steady-state and dynamic performance of closed-loop systems. The proposed method has a straightforward structure without excessively increasing the complexity and cost. It can adaptively adjust the values of the control parameters ($K_p$, $K_i$ and $K_d$) by following a new control law. Simulation results show that the line transient response of the MA-PID is better than that of the adaptive digital PID because the differential coefficient $K_d$ is introduced to changes. In addition, experimental results based on a FPGA indicate that the MA-PID control algorithm reduces the recovery time by 62.5% in response to a 1V line transient, 50% in response to a 500mA load transient, and 23.6% in response to a steady-state deviation, when compared with the conventional PID control algorithm.

PWM 방식 벅 컨버터의 빠른 과도응답 기술 (Fast Transient Response Techniques for PWM Buck Converter)

  • 석진민;서정덕;공배선
    • 전기전자학회논문지
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    • 제20권1호
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    • pp.103-106
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    • 2016
  • PWM 벅 컨버터는 3형 오차 보상기를 주로 사용하고 있다. 이 오차 보상기는 낮은 슬루율을 갖게 하는 큰 커패시터로 인해, 부하 전류의 과도응답이 발생하였을 때 부하 전압에 의도하지 않은 큰 오버슈트와 언더슈트를 발생시킨다. 또한 기준전압을 변화시켰을 때의 변화에도 느리게 응답한다. 전원장치의 효율적인 사용을 위해 다양한 부하 전류와 전압이 요구되고 있고, PWM 벅 컨버터 역시 부하 전류 변화와 기준 전압 변화에 따른 부하 전압의 빠른 응답특성을 가져야 한다. 본 논문은 PWM 벅 컨버터의 응답시간을 늘이기 위한 여러 가지 빠른 과도응답 기술들의 동작 방식과 이들 방법이 갖고 있는 장점, 한계점들을 소개한다.

위상변이를 이용한 배전용 정지형 보상기의 전류 지령 계산 (Current Reference Calculation for Distribution Static Compensator using Phase Shift)

  • 홍성민;최종우
    • 전력전자학회논문지
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    • 제17권1호
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    • pp.41-47
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    • 2012
  • This paper proposes a calculation of compensation current using phase shift to eliminate ripple components of instantaneous active power under unbalanced or non-linear loads condition. The proposed phase shift method instead of existing method(LPF; Low Pass Filter) to remove ripple components and this proposed method improves performances of transient and steady state response. To compare proposed method with existing method, experiments have been done for calculating an average active power at load side. Their results show that transient response and steady state response of proposed method is improved.