• 제목/요약/키워드: Structure actuator

검색결과 709건 처리시간 0.026초

적층형 압전밸브의 유동특성 해석 (Analysis of Flow Characteristics of Multilayer Type Piezo Valve)

  • 김재민;이종춘;윤석진;정귀상
    • 한국전기전자재료학회:학술대회논문집
    • /
    • 한국전기전자재료학회 2003년도 하계학술대회 논문집 Vol.4 No.2
    • /
    • pp.946-949
    • /
    • 2003
  • This paper reports on the fluid flow simulation results of a multilayer type piezoelectric valve. The mechanical and fluidic analysis are done by finite element method. The designed structure is normally closed type using buckling effect, which is consist of three separate structures; a valve seat die, an actuator die and a MLCA(Multilayer Type Ceramic Actuator). It is confirmed that the complete laminar flow and the lowest flow leakage are strongly depend on the valve seat geometry. In addition, turbulent flow was occurs in valve outlet according to increase seat dimension, height and inlet pressure. From this, we was deducts the optimum geometry of the valve seat and diaphragm deflection that have an great influence fluid flow in valve. Thus, it is expected that our simulation results would be apply for piezoelectric applications such as valve and pump, fluidic control systems.

  • PDF

Analysis of Low-Profile Piezoelectric Butterfly Linear Motor using 3D Laser Vibrometer

  • 이원희;강종윤;백동수;주병권;윤석진
    • 한국전기전자재료학회:학술대회논문집
    • /
    • 한국전기전자재료학회 2010년도 하계학술대회 논문집
    • /
    • pp.325-325
    • /
    • 2010
  • Piezoelectric linear motors have been widely studied for auto focusing devices of digital cameras and cellular phones due to their simple structure. In this paper, we confirmed that novel piezoelectric butterfly linear motor was fabricated and its dynamic properties were analyzed. The piezoelectric transducer (having size $9{\times}8{\times}1\;mm^3$) is composed of an elastic plate, which includes a tip for energy transfer and two fixing protrusions for fixture, and two piezoelectric ceramics. The butterfly linear motor has been designed and optimized using A TILA simulation program. The superposed motion is an elliptical vibration on the tip. The actual movement of the manufactured actuator was confirmed by a 3D laser dopier vibrometer and compared with the simulation results. The results of numerical study and experimental investigation will be used for the future optimization of the actuator and the realization of the advanced ultrasonic motor.

  • PDF

스팀터빈 Exhaust System에서 LP터빈과 Exhaust Hood 사이의 간섭에 대한 수치해석적 연구 (Numerical investigation of LP turbine-exhaust hood interaction in the steam turbine exhaust system)

  • 임지현;주원구;김영상;임홍식
    • 유체기계공업학회:학술대회논문집
    • /
    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
    • /
    • pp.291-294
    • /
    • 2006
  • Exhaust system of steam turbines consists of an annular diffuser and a collector and connects the last stage turbine and the condenser. The system is used to transfer the turbine leaving kinetic energy to potential energy while guiding the flow from turbine exit plane to the downstream condenser. In the steam turbine exhaust system, distorted pressure profile is arisen by the nonaxisymmetric collector structure at the diffuser outlet, and this distorted pressure is propagated to the last stage LP turbine exit plane through the diffuser, then the last stage LP turbine experiences asymmetric back pressure. It is known that the pressure recovery performance of diffuser is strongly influenced by diffuser inflow condition. In this study, the effect of exhaust system due to the changing of inlet flow condition is observed by using CFD, and the interaction of last stage LP turbine and exhaust system is investigated by using actuator disk model as modeling of turbine blade row of exhaust hood inlet.

  • PDF

중력 보상기를 적용한 로봇 매니퓰레이터 연구 (Study on Robot Manipulator applying the Gravity Compensator)

  • 최형식;허재관;서해용;홍성율
    • Journal of Advanced Marine Engineering and Technology
    • /
    • 제34권2호
    • /
    • pp.267-274
    • /
    • 2010
  • 중력보상기의 구조에 대해 연구하였고, 이를 적용하여 로봇 관절의 성능을 개선하기 위하여 새롭게 개발한 6축의 로봇 매니퓰레이터에 대해 설명한다. 로봇의 기구학 해석을 하였다. 또한, 다양한 스프링으로 구성된 중력보상기를 적용한 로봇 관절구동기의 성능에 대하여 시뮬레이션 하였다. 시뮬레이션 결과에 따르면, 중력보상기를 적용한 로봇 매니퓰레이터의 관절에 가해지는 외부부하는 중력보상기에 사용되는 스프링의 강도에 비례하여 줄어드는 것이 검증되었다.

유정압안내면 운동오차보정용 능동제어모세관의 기본특성 (Basic Characteristics of an Active Controlled Capillary for Compensating the Error Motion of Hydrostatic Guideways)

  • Song, Y.C.;Park, C.H.;Kim, S.T.
    • 한국정밀공학회지
    • /
    • 제14권8호
    • /
    • pp.130-136
    • /
    • 1997
  • For compensating the error motion of hydrostatic guideways, we introduce a way that the clearance of table is actively controlled corresponding to the amount of error with the variable capillary. The structure and the theoretical design method of active controlled capillary using piezo actuator, named ACC, are proposed in this paper. Basic characteristics such as the maximum controllable range, micro step response and available dynamic bandwidth are tested for confirmation of structural suitability of ACC, and these characteristics are also tested on the table mounted with ACC for verifying the availability. The experimental result showed that by the use of ACC, the error motion within 2.7 .mu. m of a hydrostatic guideway can be compensated with the resolution of 2.7nm, 1/100 contollable range, and the frequency bandwidth of 5.5 Hz. From these results, it is confirmed that the ACC is very effective to improve the motion accuracy of high or ultra precision hydrostatic guideways.

  • PDF

헬리콥터 로터 공력해석을 위한 수치적 방법 연구 (THE INVESTIGATION OF HELICOPTER ROTOR AERODYNAMIC ANALYSIS METHODS)

  • 박남은;우철훈;노현우;김철호;이석준
    • 한국전산유체공학회:학술대회논문집
    • /
    • 한국전산유체공학회 2007년도 춘계 학술대회논문집
    • /
    • pp.120-124
    • /
    • 2007
  • Helicopters and rotary-wing vehicles encounter a wide variety of complex aerodynamic phenomena and these phenomena present substantial challenges for computational fluid dynamics(CFD) models. This investigation presents the rotor aerodynamic analysis items for the helicopter development and variety aerodynamic analysis methods to provide the better solution to researchers and helicopter developers between aerodynamic problems and numerical aerodynamic analysis methods. The numerical methods to make an analysis of helicopter rotor are as below - CFD Modelling : actuator disk model, BET model, fully rotor model,... - Grid : sliding mesh, chimera mesh / structure mesh, unstructure mesh,... - etc. : panel method periodic boundary, quasi-steady simulation, incompressible,... The choice of CFD methodology and the numerical resolution for the overall problem have been driven mostly by available computer speed and memory at any point in time. The combination of the knowledge of aerodynamic analysis items, available computing power and choice of CFD methods now allows the solution of a number of important rotorcraft aerodynamics design problems.

  • PDF

Fabrication of Electro-active Polymer Actuator Based on Transparent Graphene Electrode

  • Park, Yunjae;Choi, Hyonkwang;Im, Kihong;Kim, Seonpil;Jeon, Minhyon
    • 한국진공학회:학술대회논문집
    • /
    • 한국진공학회 2014년도 제46회 동계 정기학술대회 초록집
    • /
    • pp.386.1-386.1
    • /
    • 2014
  • The ionic polymer-metal composite (IPMC), a type of electro-active polymer material, has received enormous interest in various fields such as robotics, medical sensors, artificial muscles because it has many advantages of flexibility, light weight, high displacement, and low voltage activation, compare to traditional mechanical actuators. Mostly noble metal materials such as gold or platinum were used to form the electrode of an IPMC by using electroless plating process. Furthermore, carbon-based materials, which are carbon nanotube (CNT) and reduced graphene-CNT composite, were used to alter the electrode of IPMC. To form the electrode of IPMC, we employ the synthesized graphene on copper foil by chemical vapor deposition method and use the transfer process by using a support of PET/silicone film. The properties of graphene were evaluated by Raman spectroscopy, UV/Vis spectroscopy, and 4-point probe. The structure and surface of IPMC were analyzed via field emission scanning electron microscope. The fabricated IPMC performance such as displacement and operating frequency was measured in underwater.

  • PDF

ECAM Control System Based on Auto-tuning PID Velocity Controller with Disturbance Observer and Velocity Compensator

  • Tran, Quang-Vinh;Kim, Won-Ho;Shin, Jin-Ho;Baek, Woon-Bo
    • International Journal of Fuzzy Logic and Intelligent Systems
    • /
    • 제10권2호
    • /
    • pp.113-118
    • /
    • 2010
  • This paper proposed an ECAM (Electronic cam) control system which has simple and general structure. The proposed cam controller adopted the linear and polynomial curve-fitting method to generates a smooth cam profile curve function. Smooth motion trajectory of master actuator guarantees the good performance of slave motion and has an important effect on the interpolation quality of ECAM. The auto-tuning PID velocity controller was applied to overcome the uncertainties in ECAM, and the gains of the controller are updated continuously to ensure the consistency of system performance under varying working conditions. The robustness of system against the varying load torque disturbances and noises is guaranteed by using the load torque disturbance observer to suppress the disturbance on master actuator. The velocity compensator was applied to compensate the degradation of performance of slave motion caused from the varying driving speed of master motion. The stability and validity of the proposed ECAM control system was verified by simulation results.

MR 유체를 이용한 새로운 액추에이터의 제안, 설계 및 제어 (Propose, Design and Control of a New Actuator Using MR Fluid)

  • 김정수;안경관;;안영공
    • 한국정밀공학회:학술대회논문집
    • /
    • 한국정밀공학회 2006년도 춘계학술대회 논문집
    • /
    • pp.111-112
    • /
    • 2006
  • A new MR cylinder with built-in valves using Magneto - Rheological fluid (MR valve) is proposed for fluid power control systems. The MR fluid is a newly developed functional fluid whose obvious viscosity is controlled by the applied magnetic field intensity. This MR cylinder, which is composed of cylinder with small clearance and piston with electromagnet, has the characteristics of simple, compact and reliable structure. This paper presents a method to control the pressure of MR cylinder by using Generalized Predictive Control (GPC) algorithm. The differential pressure is controlled by applying magnetic field intensity to MR fluid. The use of GPC controller is to generate a control sequence by minimizing a cost function in such a way that the future system output is driven close to reference over finite prediction horizons. Experimental results from real time control using GPC method compared with conventional PID control method are also shown in this paper.

  • PDF

가동차 위치에 따른 인덕턴스 변화와 Push/Pull 효과를 고려한 가동코일형 LOA의 동특성 (Dynamic Characteristics of Moving Coil Linear Oscillatory Actuator Considering the Variable Inductance and Push/pull Effects)

  • 정상섭;장석명
    • 대한전기학회논문지:전기기기및에너지변환시스템부문B
    • /
    • 제50권7호
    • /
    • pp.307-314
    • /
    • 2001
  • A moving coil linear oscillatory actuator is consisted of the NdFeB permanent magnets with high specific energy as the stator, a coil-wrapped nonmagnetic hollow rectangular structure and an iron core as a pathway for magnetic flux. The variation of mover position and the consequent changes of coil flux path affect the coil inductance, because coil flux leaks at the open region of LOA stator. The interaction between permanent magnet and armature field is to shift the airgap flux density variation due to the magnet alone by a certain amount. The unbalanced reciprocation force due to armature reaction field decreases the advantage of moving coil LOA, such as a high degree of linearity and controllability in the force ad motion control. This paper firstly describes the coil inductance, the deviation of flux density, and the unbalanced reciprocation force, which are derived form the permeance model of LOA. Secondly, the analytical method are verified using the 2D finite element method and tests. Finally, the dynamic simulation algorithm taking the armature reaction effect and variable inductance into account, is proposed and confirmed through the experiment.

  • PDF