• 제목/요약/키워드: linear actuator

검색결과 632건 처리시간 0.029초

전방향성 선형 압전 액추에이터의 설계와 분석 (Design and analysis of omni-directional linear piezoelectric actuator)

  • 정우석;강종윤;김정도;백동수;조봉희;김영호;윤석진
    • 센서학회지
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    • 제18권3호
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    • pp.185-189
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    • 2009
  • In this paper, we present design and analysis of the omni-directional linear piezoelectric actuator which was consisted of one actuator using the half-wave vibrator. Through calculating vibration speeds on each sector of the actuator, the displacement of contact point of the actuator is theoretically confirmed to be about 33 nm. To confirm an applicable possibility of omni-directional linear piezoelectric actuator, elliptical motion for linear movement, displacement of the tip, changing directions and admittance characteristics are simulated by ATILA. Compared with theoretical result, we obtained similar data with displacement of 32.5 nm at contact point. And then the actuator is simulated elliptical trajectories for linear motions and changing directions according to combination of input signal.

Evaluation of Structural Safety of Electro-Mechanical Linear Actuator and Load Simulator with Plate Spring

  • Kim, Dong-Hyeop;Kim, Young-Cheol;Kim, Sang-Woo;Lee, Jong Whan
    • 항공우주시스템공학회지
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    • 제14권6호
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    • pp.18-25
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    • 2020
  • This study investigated the structural behaviors and safety of an electro-mechanical linear actuator and a load simulator with a plate spring. The material and dimensions of the plate spring were determined by theoretically calculating the stress and torsional angle for the rating load of the actuator. Thereafter, a flexible multibody dynamics (FMBD) analysis was conducted on the linear actuator and load simulator to confirm the performance of the load simulator and acquire the reaction forces acting on the actuator and simulator. The structural safety of the linear actuator and load simulator was evaluated via finite element analysis using the aforementioned reaction forces. Consequently, the proposed linear actuator and load simulator were determined to be structurally safe; however, the safety factors for the actuation rod and the housing on the actuator were excessively high. Therefore, the weight and cost must be reduced to improve their design parameters in the future.

에너지 변환 이론에 의한 직선형 피스톤 액추에이터의 권선부 인가 전압의 특성 해석 (Analysis of the Voltage Characteristics Applied to a Actuator Winding by Electromechanical Energy Conversion Theory)

  • 김양호;손웅태;황석영
    • 한국조명전기설비학회:학술대회논문집
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    • 한국조명전기설비학회 2004년도 춘계학술대회 논문집
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    • pp.469-472
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    • 2004
  • 본 논문에서는 직선형 피스톤 액추에이터의 응용모델을 제안하고 이를 구현하였다. 구성된 액추에이터의 해석을 위해서 패러데이 법칙으로부터 기본 방정식을 유도하였고, 이를 바탕으로 소형, 경량, 고속 응답을 요구하는 시스템에 적용 가능한 실험적 자료를 얻었다. 또한 본 논문에서는 자계로부터 일반적으로 구할 수 있는 전자기력을 에너지 변환 이론적 관점에서 기계 방정식과 결합하고 전원 공급부의 인가 전압의 변화로부터 액추에이터에 나타나는 현상을 Matlab 프로그램을 활용하여 간접적 방법으로 고찰하였다. 그 결과는 실제적인 설계에 적용할 경우 설계 프로그램의 자료나 부분적 변경시 참조 할 수 있으리라 사료된다. 이 결과를 바탕으로 Linear Actuator MfdBl 시스템과 구현된 직선형 피스톤 액추에이터의 동작이 실제 시스템에 활용될 수 있는 방법으로 가능함을 검증할 수 있었다.

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인치웜 구조를 갖는 선형 스테이지의 속도 특성연구 (Speed Property Evaluation of an Inchworm Type Linear Stage)

  • 문찬우
    • 로봇학회논문지
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    • 제2권2호
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    • pp.178-182
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    • 2007
  • Precision stages are essential device for micro machines, fiber optic assembly systems, and biology instruments. In this paper, a precision inchworm type actuator for a linear stage is proposed and evaluated. An analytic method to design an inchworm type motor is proposed. Developed actuator provides fast motion compared with a commercial inchworm actuator, and can be used as an actuator for a stage in substitution for a conventional rotary actuator.

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자왜재료를 이용한 선형 작동기의 유한요소 해석 (Finite Element Analysis of Magnetostrictive Linear Actuator)

  • 김윤창;김재환
    • 한국소음진동공학회논문집
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    • 제17권4호
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    • pp.356-362
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    • 2007
  • Magnetostrictive materials have been used for linear actuators due to its large strain, large force output with moderate frequency band in the presence of magnetic field. However their performance analysis is difficult because of nonlinear material behaviors in terms of coupled strain-magnetic field dependence, nonlinear permeability, pre-stress dependence and hysteresis. This paper presents a finite element analysis technique for magnetostrictive linear actuator. To deal with coupled problems and nonlinear behaviors, a simple finite element approach is proposed, which is based on separate magnetic field calculation and displacement simulation. The finite element formulation and an in-house program development are illustrated, and a simulation model is made for a magnetostrictive linear actuator. The fabrication and performance test of the linear actuator are explained, and the performance comparison with simulation result is shown. Since this approach is simple, it can be applied for analyzing magnetostrictive underwater projectors and ultrasonic transducers.

굴곡 진동모드를 이용한 초음파 선형 압전 액추에이터 개발 (Development of ultrasonic linear piezoelectric actuator with flexuralvibration mode)

  • 윤장호;최우천;강종윤;강진규;윤석진
    • 센서학회지
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    • 제18권6호
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    • pp.461-466
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    • 2009
  • This paper represents a piezoelectric ultrasonic linear actuator with flexural vibration mode. The actuator is composed of two piezo ceramics, the elastic body, and the connecting tip. It is driven by the frictional force between the connecting tip and the linear motion guide. Unimorph actuators have flexural vibration. Its middle point is fixed so that suitable to the flexural vibration of $3/2\lambda$. These vibrations contribute to elliptical motion by mixed mode between longitudinal and transverse mode. It was generated when the ultrasonic electrical signals with 90 degree phase difference are applied to two ceramics. A linear movement can be easily obtained using the elliptical motion. The ATILA, FEM simulator has been used to design actuator and verify the kinetic and dynamic analysis. We used the ceramics of $20\times10\times1$ mm size and confirmed the flexural vibration of the $3/2\lambda$ at the 79 kHz through the scanning of 3D-vibrometer. The maximum velocity of actuator was 221 mm/sec and the thrust force of actuator was 2.7 N in 200Vp-p of additional voltage.

항공기 플랩 제어를 위한 선형 구동기의 구조 안전성 평가 (Evaluation of Structural Safety of Linear Actuator for Flap Control of Aircraft)

  • 김동협;김상우
    • 항공우주시스템공학회지
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    • 제13권4호
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    • pp.66-73
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    • 2019
  • 본 연구에서는 항공기 플랩 제어를 위한 선형 구동기의 기본 설계에 대한 구조 안전성을 평가하였다. 다물체 동역학 분석을 통해 선형 구동기의 기계적 운동을 이해하였고, 접촉 하중을 산출하여 유한요소해석 기반의 구조 분석에 적용하였다. 구조 분석에서는 선형 구동기의 설계 속도 조건에 대한 열, 정적 거동을 검토하였고, 구조적 안전성을 평가하였다. 또한 모드 해석을 수행하여 동적 거동을 분석하였다. 분석 결과, 모터가 225 rpm으로 작동 시 구동 로드는 약 5 mm/s로 병진 운동하였고, 기어 간 최대 32.83 N의 접촉 하중이 발생하였다. 한편, 최대 열 응력과 정 응력은 철의 항복강도의 약 1.57%, 78%로 발생하였고, 각 부품은 서로의 공진 주파수를 회피하였다. 따라서 제안된 선형 구동기의 기본설계는 구조적으로 안전하며, 공진에 대해 안정적임을 밝혔다.

Design and Analysis of A Mini Linear Optical Pickup Actuator

  • Park, Joon-Hyuk;Baek, Yoon-Su;Park, Young-Pil
    • Journal of Mechanical Science and Technology
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    • 제17권11호
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    • pp.1616-1627
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    • 2003
  • This paper describes a mini linear optical pickup actuator. To reduce the size, inner yokes are designed to guide the mover and outer yokes of permanent magnets are removed. Magnetic circuit method is used to determine the thrust force. Virtual path method is proposed to analyze the open magnetic circuit analysis. The magnetic circuit of the proposed actuator can be a closed circuit due to the virtual path model of the outer magnetic flux. The validity of virtual path method is evaluated by comparing to the FEM analysis. Structural vibration is investigated using FEM and the design of the mover is modified to improve the vibration characteristic. Dynamic characteristic experiments shows that the performance of the proposed actuator is enough to be used as a coarse and fine seeking actuator simultaneously and the thrust force margin for loading a focusing actuator is guaranteed.

Testing and experimental characterization of a linear permanent magnet actuator for active vehicle suspension

  • Wang, Jiabin;Wang, Weiya
    • Journal of international Conference on Electrical Machines and Systems
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    • 제1권4호
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    • pp.509-516
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    • 2012
  • This paper describes the testing and experimental characterization of a linear permanent magnet actuator, which is designed and developed for active vehicle suspension, under both static and dynamic conditions. Since the active suspension unit operates over a wide force-velocity range with varying duty ratios, it is essential to establish an effective thermal model which can be used for assessing temperature rise of the actuator under various operating conditions. The temperature rise of the actuator is measured and the results are compared with the prediction by the derived transient thermal model. It is shown that the measured actuator parameters and characteristics are closed to their predicted values. The linear actuator is controlled by a dSPACE system via a three phase inverter and its velocity tracking performance is presented.

Position Control of Linear Actuator with Time Delay Using the Smith Predictor

  • Kang, Seung-Won;Park, Gi-sang
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.68.1-68
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    • 2001
  • This paper discusses tracking position control of linear actuator that has a time delay. The time delay happens when the process reads the sensor data and sends the control input to the plant located at a remote site in distributed control system. In this thesis, the time delay between the linear actuator and the discrete PID controller has constant value due to buffer device so the time delay can be modeled by Pade approximation but the large position error of the linear actuator is generated by the time delay. Therefore, the Smith predictor is used for tracking position control of the linear actuator with the time delay in order to minimize the effect of the time delay. The experimental and simulation results show that the ...

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