• Title/Summary/Keyword: 4축 스테이지

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Vibration Analysis of a Nano Imprinting Stage Using CAE (CAE를 이용한 나노 임프린팅 스테이지의 진동 해석)

  • Lee, Kang-Wook;Lee, Jae-Woo;Lee, Sung-Hoon;Lim, Si-Hhyung;Jung, Jae-Il;Yim, Hong-Jae
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2008.04a
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    • pp.579-584
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    • 2008
  • A nano-imprinting stage has been widely used in various fields of nanotechnology. In this study, an analysis method of a nano-imprinting stage machine using FEM and flexible multi-body vibration has been presented. The simulation using CAE for the imprinting machine is to analyze vibration characteristics of 3-axis nano-imprinting stage and 4-axis nano-imprinting stage. Structural components such as the upper plate have been modeled with finite elements to analyze flexibility effects during the precision stage motion. In this paper flexible multi-body dynamic simulation is executed to support robust design of the precision stage mechanism.

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The vibrational characteristics of nano-imprinting stages with respect to supporter types (지지방식의 차이에 따른 나노 임프린팅 스테이지의 진동 특성 비교)

  • Lee, Sung-Hoon;Park, Sung-Bin;Lee, Kang-Wook;Jeong, Jay-I.;Yim, Hong-Jae
    • Proceedings of the KSME Conference
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    • 2008.11a
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    • pp.948-954
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    • 2008
  • In this study, vibrational characteristics of two nano-imprinting stages is analyzed and compared with respect to the methodology to support the upper-plate of the stage. The first type of the stage has three supporters at each corners of the stage and one thrust bearing at the center of the stage. The other type of the stage has four supporter in each corner of the stage without a thrust bearing. The FEM software with flexible modeling is used for the normal mode analysis. The result depicts the difference of vibrational characteristics caused by the difference of support methods. The design criteria for the precision nano-imprinting stage is also discussed.

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Dynamic Analysis of a 4-Axis Nano Imprinting Stage Mechanism considering Flexibility (유연성을 고려한 4축 나노임프린팅 스테이지의 동적 해석)

  • Park, Sung-Bin;Jeong, Jae-I.;Yim, Hong-Jae
    • Proceedings of the KSME Conference
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    • 2008.11a
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    • pp.844-849
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    • 2008
  • A nano-imprinting stage has been widely used in various fields of nano-technology. In this study, A 4-axis nano-imprinting stage is modeled with using the 3D-CAD Tool. Structural components such as an upper-plate, bearings and cross-roller-guides are modeled with finite elements to analyze flexibility effect during the precision stage motion. In addition, Dynamic analysis is executed to reproduce actual motion of 4-axis nano imprinting stage.

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Dynamic Analysis of a Nano Imprinting Stage Using CAE (CAE를 이용한 나노 임프린트 스테이지의 동적 거동해석)

  • Lee, Kang-Wook;Lee, Min-Gyu;Lee, Jae-Woo;Lim, Si-Hyung;Shin, Dong-Hoon;Jang, Si-Youl;Jeong, Jae-Il;Yim, Hong-Jae
    • Transactions of the Korean Society of Machine Tool Engineers
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    • v.16 no.5
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    • pp.211-217
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    • 2007
  • A nano-imprinting stage has been widely used in various fields of nanotechnology. In this study, an analysis method of a nano-imprinting stage machine using FEM and flexible multi-body kinematics and dynamics has been presented. We have developed a virtual imprinting machine to evaluate the prototype design in the early design stage. The simulation using CAE for the imprinting machine is not only to analyze static and dynamic characteristics of the machine but also to determine design parameters of the components for the imprinting machine, such as dimensions and specifications of actuators and sensors. Structural components as the upper plate, the rotator, the shaft and the translator have been modeled with finite elements to analyze flexibility effects during the precision stage motion. In this paper flexible multi-body dynamic simulation is executed to support robust design of the precision stage mechanism. In addition, we made the 4-axis stage model to compare the dynamic behavior with that of 3-axis stage model.

Bond Graph Modeling, Analysis and Control of Dual Stage System (본드그래프를 이용한 듀얼 스테이지 시스템의 모델링, 해석, 및 제어)

  • Wang, Wei-Jun;Han, Chang-Soo
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.13 no.4
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    • pp.1453-1459
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    • 2012
  • The dual stage manipulator is composed of the voice coil motor (VCM) and piezoelectric ceramics transducer (PZT), which can produce the high precise displacement and express a well dynamic performance. However, inaccurate modeling of the dual stage will exacerbate the positioning accuracy. This paper presents an approach to model the dual stage system by using bond graph theory. And the state space equations can be derived through the bond graph straightforwardly, which can be used in computing simulations. Through designing the compensators for the dual stage system and simulating, the dual stage performs better dynamics characteristic than the single actuator system.

Modeling of a 4-axis redundant stage by using SimMechanics (SimMechanics를 이용한 4축 과구동 스테이지의 모델링)

  • Lee, Jin-Young;Park, Won-Jun;Won, Chong-Jin;Jeong, Jay-I.
    • Proceedings of the KSME Conference
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    • 2008.11a
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    • pp.827-831
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    • 2008
  • In this paper, kinematic analysis for a planar 3-DOF redundant stage which has four actuators is presented by using SimMechanics software package. SimMechanics is a block sets of the Matlab/Simulink package. The SimMechanics enables a simplified model for a complex kinematic mechanism, since kinematic relationship between joints and linkages for the kinematic chains are expressed as line vectors and block diagrams. Here, positional error and limit values of movement ranges of the stage are evaluated by using the SimMechanics. The validity of the kinematic characteristics model was compared with theoretical kinematic analyses for the 3-DOF stage.

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Numerical Analysis of the Turbine Rotor Flow with the Unsteady Passing Wake from a Stator (정익에서 발생한 비정상 후류를 지나는 터빈 동익 유동장 수치해석)

  • Lee, Eun-Seok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.4
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    • pp.275-280
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    • 2007
  • A turbine stage consists of stators and rotors. The stator provides the required inlet flow conditions so that the rotor can produce the necessary power. Passing wakes generated from the trailing edge of the stator make an interaction with the rotor. In the present study, this flow mechanism is investigated using the numerical analysis. In case of a large gap distance between the stator and rotor, the flow can be solved independently. First, only the stator flow field is solved. Second, the rotor flow field is solved including the passing wake characteristics obtained from the stator analysis. The passing wake experiences the shearing as it approaches to the rotor blade leading edge. And it is chopped when it strikes the rotor blade. After that, the chopped wakes becomes the prolongation as it travels downstream. The flow according to the variation of the gap distance is also studied. Pressure jumps due to the passing wakes result in the pressure and lift loss and it gets stronger with the closer gap distance.

The Modified Two-axis Vector Controller of Linear Induction Motor to Apply to the Non-contact Stage with Large Workspace (대면적 비접촉 스테이지에 구동기 적용을 위한 선형유도기의 변형된 2축 벡터 제어기)

  • Jung, Kwang-Suk;Lee, Sang-Heon
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.4
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    • pp.385-391
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    • 2008
  • To effectively cope with a complexity of kinematic metrology due to workspace enlargement of the planar stage, the linear induction motor is suggested as its new driving source. Especially, the linear induction motor under uniform plate type of secondary doesn't inherently have a periodical force ripple which is generally shown in the brushless DC motor. But, it presents a poor transient characteristic at zero or low speed zone owing to time delay of flux settling, resulting in slow response. To improve the servo property of linear induction motor and apply successfully it to the precision stage, this paper discusses a modified vector control methodology. The controller has a novel input form, fixed d-axis current, q-axis current and forward-fed DC current, to control thrust force and normal force of the linear induction motor independently. Influence of the newly introduced input and the feasibility of controller are validated experimentally.