• Title/Summary/Keyword: Actuator disc

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Development and Performance Evaluation of Polymer Micro-actuator using Segmented Polyurethane and Polymer Composite Electrode (세그먼트화 폴리우레탄을 이용한 고분자 마이크로 액츄에이터의 제작 및 고분자 전극의 상태에 따른 구동성능)

  • Jung Young Dae;Park Han Soo;Jo Nam Ju;Jeong Hae Do
    • Journal of the Korean Society for Precision Engineering
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    • v.22 no.2
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    • pp.180-187
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    • 2005
  • This paper is focused on the development of the flexible electrode for disc-type polymer actuators using Segmented Polyurethane(SPU). This paper consists of two parts. The one is about the mechanical property such as elastic modulus. these parameters mainly affect behaviors of polymer actuators and the other is about the electro-chemical property such as the surface resistance of the composite electrode affects the strength of electrostatic force, results in the deformation of polymer actuators. The Young's modulus was measured by UTM. As result, by increasing the modulus of a body of polymer actuators, the maximum displacement of polymer actuators are decreased. The surface resistance of the electrode was measured by 4 point probe system. Compared with the conductive silver grease, the displacement of polymer actuators using carbon black(CB) composite electrodes is comparably small but CB composite electrode should be the practical approach for the improvement of the performance of all-solid actuators, compared with another types of electrode materials.

Flow in a High Speed Compressor Due to Axisymmetric Tip (대칭 팁 간극에 기인한 고속으로 회전하는 압축기에서의 유동)

  • Joo, Hyun Suh;Song, Seung Jin
    • 유체기계공업학회:학술대회논문집
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    • 2002.12a
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    • pp.279-283
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    • 2002
  • The effects of finite gap at the tip of turbomachinery blades have long been topics of both theoretical and experimental research because tip clearance degrades turbomachinery performance. This paper presents an analytical study of radial flow redistribution in a high speed compressor stage with axisymmetric tip clearance. The flow is assumed to be inviscid and compressible. The stage is modeled as an actuator disc and the analysis is carried out in the meridional plane. Upon going through the stage, the radially uniform upstream flow splits into the tip clearance and passage flows. The tip clearance flow is modeled as a jet driven by blade loading, or pressure difference between the pressure and suction sides. The model takes into consideration the detached shocks which occur in the rotor passage at the design point. This shock model is used to calculate the density ratio across the stage. Thus, the model is capable of predicting the kinematic effects of tip clearance in the high speed compressor flow field.

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Design and Analysis of a Linear Motor for Slim-line ODD (소형 광디스크 드라이브용 선형 구동기의 설계 및 특성 해석)

  • Shim, Min-Taek;Park, Joon-Hyuk;Baek, Yoon Su
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.11b
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    • pp.794-798
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    • 2002
  • This paper deals with a moving coil type linear motor for fast access of the miniature ODD. This slim-line motor is composed of the mover supported by guide mechanism, the coil wound into it, and the yoke attached to the permanent magnet for stator. The driving force is generated by the PM of the stator and the current in the coils of the mover. Magnetic circuit analysis and Finite Element Method are applied to estimate the thrust force at air gap. In order to compare the force characteristics between two methods, various experiment results are applied to verify on a prototype. Also the flexible modes of the motor are predicted through the FEM and the structural components are modified to locate this on high frequency region.

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Gap Servo for High Density Near Field Optical Storage Devices (근접장 광 저장 장치의 Gap 서보)

  • Lee JeongUk;Seo JeongKyo;Shin Yunsup;Park JinMoo;Jeong MiHyeon;Choi InHo
    • 정보저장시스템학회:학술대회논문집
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    • 2005.10a
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    • pp.12-13
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    • 2005
  • Near field recording (NFR) technology with SIL has been thought as the most promising generation optical storage device. A gap distance between the SIL and the disc should be controlled to be 20${\~}$40nm. We observed gap error signal in our NFR test-bed using a blue LD (405nm). The digital gap servo filter and control algorithm were developed to maintain a constant air gap by adopting a conventional actuator.

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DVD/CD Compatibility using Single Objective Lens in Optical Pickup for BD(Blu-ray Disc) (BD용 광픽업에서 1매대물렌즈를 이용한 DVD/CD호환)

  • ;;N.KAIHO;N.TAKEYA;H.SHINDO;I.MORISHITA
    • Proceedings of the Optical Society of Korea Conference
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    • 2003.02a
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    • pp.258-259
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    • 2003
  • 보호층 0.1mm두께의 20GB이상의 광디스크를 기록·재생하는 High Density Optical System에서는 Blue-violet laser와 NA(Numerical Aperture)0.85의 High NA의 대물렌즈를 사용한 Optical Pick Up이 필요로 된다. 종래의 대물렌즈는 glass 또는 plastic제의 2매 조합 대물렌즈가 많이 사용되어지고 있는데, 이는 두 렌즈간의 거리를 일정하게 유지시키기 위한 홀더 조립시의 공차가 엄격히 요구되며, 2매 조합 대물렌즈를 구동시키기 위한 actuator의 부피와 무게를 증가시킴으로서 구동감도를 감소시키는 단점이 있다. (중략)

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Characterization of Piezoelectric-Actuated PDMS Micropump (PDMS로 제작된 압전력 구동 방식의 마이크로 펌프의 특성)

  • Kim, Jin-Ho;Na, Kwang-Ho;Kim, Young-Ho;Kim, Yong-Sang
    • Proceedings of the KIEE Conference
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    • 2003.07c
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    • pp.1926-1928
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    • 2003
  • The low-cost, simple structured micropump which is actuated by piezoelectricdiscs, is fabricated with polydimethylsiloxane (PDMS) and the performances of the micropump, such as pump rate and backward pressure, are characterized. The PDMS micropump with diffusers instead of passive check valves as a flow-rectifying element was fabricated. While the square wave driving voltage is applied to the piezoelectric disc of the actuator, the flow rate is measured by fluid displacement variation of the outlet tube. The flow rate of micropump increases with enhancing the applied voltage due to the increase of diaphragm deflection. The flow rate and the backward pressure of the micropump with diffusers are about $32.9{\mu}{\el}$/min and 173Pa respectively for the above mentioned deflection conditions.

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Center Compensation Servo and Eccentric Compensation Control for High Speed CD-RW Drive System (고배속 CD-RW Drive를 위한 중점 서보 및 편심 보상 제어)

  • Kim Dongwon;Park Gwi-Tae;Seo Sam-Jun
    • Journal of Institute of Control, Robotics and Systems
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    • v.10 no.12
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    • pp.1202-1209
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    • 2004
  • This paper presents a design methodology of a Digital Servo Signal Processor for high speed CD-RW drive systems. The proposed Digital Servo Signal Processor enables us to develop CD-related systems for the very high speed applications and is one of the key components of the CD-RW systems. The proposed center compensation servo control is newly built for an actuator shaking due to the fast response of a step motor when it jumps to a long distance. A control method compensating for eccentricity of a disc is implemented for operating robustly at a higher rotational speed. This servo mechanism is more size efficient and less power consumed because it is implemented using a ARM7 embedded processor and hardware digital filters. Furthermore, it is convenient to upgrade firmware for the future required functions. From experimental results, we can see that the performance of the control system is improved greatly. The proposed servo algorithm shows a shorter setting time including a pull-in time and a faster access time. It can be applied easily to the DVD-ROM and the DVD-RAM which have the same optical structure.

CFD Study on Aerodynamic Power Output of 6 MW Offshore Wind Farm According to the Wind Turbine Separation Distance (CFD를 활용한 6 MW 해상풍력발전단지의 풍력터빈 이격거리에 따른 공기역학적 출력 변화연구)

  • Choi, Nak-Joon;Nam, Sang-Hyun;Jeong, Jong-Hyun;Kim, Kyung-Chun
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.8
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    • pp.1063-1069
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    • 2011
  • This paper presents aerodynamic power outputs of wind turbine of 6 MW wind farm composed of 3 sets of 2 MW wind turbine according to the separation distance by using CFD. Layout design including offshore wind farm and onshore wind farm is key factor for the initial investment cost, annual energy production and maintenance cost. For each wind turbine rotor, not actuator disc model with momentum source but full 3-dimensional model is used for CFD and it has a great technical meaning. The results of this study can be applied to the offshore wind farm layout design effectively.

Prediction of Trajectories of Projectiles Launched from Helicopters (헬리콥터에서 발사되는 발사체의 궤적 예측)

  • Gong, Hyojoon;Kwak, Einkeun;Lee, Seungsoo;Park, Jae Seong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.3
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    • pp.213-220
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    • 2014
  • A program that predicts trajectories of projectiles influenced by the interference flow field of helicopters is developed. The interference flow field are computed using a compressible inviscid solver in conjunction with an actuator disc model. The trajectories are predicted using 6-DOF (Degree of Freedom) equations as well as an alternative form of modified point mass equations of motion. The method for the interference flow field prediction method are validated with ROBIN(ROtor Body INteraction) model. A Sierra international bullet and a 105mm projectile are used to validate the trajectory method. Trajectories of a Sierra International bullet and a HYDRA 70 rocket firing from a helicopter are predicted.

CFD validation and grid sensitivity studies of full scale ship self propulsion

  • Jasak, Hrvoje;Vukcevic, Vuko;Gatin, Inno;Lalovic, Igor
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.11 no.1
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    • pp.33-43
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    • 2019
  • A comparison between sea trial measurements and full-scale CFD results is presented for two self-propelled ships. Two ships considered in the present study are: a general cargo carrier at Froude number $F_n=0:182$ and a car carrier at $F_n=0:254$. For the general cargo carrier, the propeller rotation rate is fixed and the achieved speed and trim are compared to sea trials, while for the car carrier, the propeller rotation rate is adjusted to achieve the 80% MCR. In addition, three grids are used for each ship in order to assess the grid refinement sensitivity. All simulations are performed using the Naval Hydro pack based on foam-extend, a community driven fork of the OpenFOAM software. The results demonstrate the possibility of using high-fidelity numerical methods to directly calculate ship scale flow characteristics, including the effects of free surface, non-linearity, turbulence and the interaction between propeller, hull and the flow field.