• Title/Summary/Keyword: Wire Type Actuator

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Vibration Characteristics of a Wire-Bonding Piezoelectric Actuator (와이어 본딩용 압전 액츄에이터의 진동 특성)

  • Kim, Young-Woo;Kim, Kyoung-Up;Lee, Seung-Yop
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2007.11a
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    • pp.578-582
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    • 2007
  • In this paper, vibration modes and frequencies of a ring-type stacked piezoelectric actuator for a wire bonding transducer system are analyzed using FEM simulations. We implement experiments using a commercial product model of the actuator PZT module which consists of 6 layer ring-type PZT and 7 electrodes, combined bolts, nut and tinut. There are two main results: One is that FEM analysis should consider the effect the harmonic voltage input in order to meet the experimental results. The other is that the current wire bonder using exciting frequency of 136 kHz should be modified in order to improve the actuator and bonding performance because the actuator module has the main longitudinal mode of 145 kHz.

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A Study on Fly-By-Wire Helicopter Control Law Design using SAS Actuators (안정성증강 작동기를 이용한 Fly-By-Wire 헬리콥터 제어법칙 설계에 대한 연구)

  • Kim, Eung-Tai;Choi, In-Ho
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.23 no.1
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    • pp.67-73
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    • 2015
  • The previous limited authority system capable of implementing attitude command response type and translational command response type by operating SAS actuator has the problem of early saturation of SAS actuator since SAS actuator should compensate the mechanical linkage displacement caused by control sick movement. In this paper, a limited authority system where flight control computer receives the command from the control stick which is not connected to the mechanical linkage is described. In this system the compensation by the SAS actuator is not necessary and SAS actuator saturate later. SAS actuator saturation problem can be further relaxed by using the trim actuator. This new limited authority system is applied to BO-105 model, simulation is performed for the doublet input and pirouette maneuver is also simulated and analyzed.

Evaluation of Dynamic Characteristics of Coarse Actuator and Design of a 2-Wire Fine Actuator for Small Form Factor ODD (초소형 광디스크 드라이브용 조동구동기의 동특성 평가 및 2-와이어 미세 구동기의 개발)

  • 박세준;이강녕;이동주;박노철;박영필
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2004.05a
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    • pp.351-351
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    • 2004
  • For greeting the era of ubiquitous network, data storage devices have been essentially attached to mobile data devices. As a result, the minimization of the storage device has arisen as major interests in the next generation data storage technology. So, there are many researches for the small form factor ODD. In this paper, we propose a pick up that consists of a linear VCM and 2-wire focusing actuator for a small form factor ODD. For the sake of checking performance of the coarse actuator, PID controller is designed. Experiment with controller and DSP board shows its propriety as a fine tracking actuator. And, 2-wire suspension actuator is designed in order to be contained in a coarse actuator and to satisfy the thickness of a PCMCIA type. Through the experiment of designed actuator, It verifies performance as a focusing actuator.

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Slim Tilt Actuator for High density Recording in the Optical Disc (기록용 고밀도 광디스크를 위한 박형 틸트 구동기)

  • Jeong, Ho-Seop;Lee, Ho-Cheol;Yoon, Yong-Han
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.11b
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    • pp.788-793
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    • 2002
  • Hybrid type slim tilt actuator and 6-wire supported are developed for DVD recording in the optical disc drive of notebook PC, which can compensate the inclination of disc and objective lens. The hybrid actuator uses the actuating method of moving coil in the focus and track direction and that of moving magnet in the tilt direction. Comparing with 6-wire supported actuator and hybrid type actuator, we can choose an actuator for slim super combo pickup. Two actuator are designed through the modal analysis and magnetic field analysis and experimental results shows dynamic characteristics. Finally, it is verified that the actuator can compensate the disc tilt of ${\pm}0.4^{\circ}$.

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Behavior of a Shape Memory Alloy Actuator with Composite Strip and Spring (복합재료 스트립과 스프링을 갖는 형상기억합금 작동기의 거동)

  • Heo, Seok;Hwang, Do-Yeon;Choi, Jae-Won;Park, Hoon-Cheol;Goo, Nam-Seo
    • Composites Research
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    • v.22 no.2
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    • pp.37-42
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    • 2009
  • This paper presents an experimental approach to design a bending-type actuator by using a shape memory alloy wire (SMA), composite strip, and spring. The SMA wire is attached to two edges of the bent strip to apply pre-stress to the SMA wire. The spring is used to provide recovery force right after actuation of the SMA wire. To investigate thermo-mechanical characteristics of the SMA wire, a series of DSC tests have been conducted and tensile tests under various levels of pre-stress and input power have been performed. Based on the measured properties of the SMA wire, bending-type actuators are designed and tested for different combination of strip, number of springs, and input power. It has been found that a bending-type actuator with a proper combination shows fast actuation performance and low power consumption.

The Geometrical Analysis of the Response and the Stiffness Matrix of a Wire Type Actuator in the Optical Disc Drive (와이어 지지형 광픽업 액츄에이터의 강성행렬과 기하학적 응답해석)

  • 단병주;최용제
    • Journal of KSNVE
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    • v.9 no.5
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    • pp.984-990
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    • 1999
  • This paper presents the geometrical methodology to decouple the vibration modes of an elastically supported single rigid body in three-dimensional space. It is shown that the vibration modes can be decoupled by placing the center of elasticity at suitable locations and thereby yielding the plane(s) of symmetry for the given stiffness matrix. The developed methodology has been applied to the actuator supported by the 4-wire suspensions in optical discs, which has one plane of symmetry. For this numerical example, the axes of vibrations have been computed and illustrated with the natural frequencies. The forced response at the objective lens is represented and its geometrical interpretation has been explained as the mutual moment between the axis of vibration and the applied wrench times the line coordinates of the axis of vibration.

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DEVELOPMENT OF THE INDEPENDENT-TYPE STEER-BY-WIRE SYSTEM USING HILS

  • Jo, H.Y.;Lee, U.K.;Kam, M.S.
    • International Journal of Automotive Technology
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    • v.7 no.3
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    • pp.321-327
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    • 2006
  • The previous paper described the logic tuning, the vehicle manufacture and the evaluation in the HILS system for the purpose of the development of a Steer-By-Wire(SBW) system. This paper describes the content of applying to a new HILS system, the vehicle manufacture and the result of the evaluation performed in Independent-type SBW(I-SBW) system. Here, the SBW indicates the method of steering both tires by using one motor as the steering gear actuator, similar to the conventional steering system. On the other hand, the I-SBW means the method of steering both front tires independently by using dual motors as the steering gear actuator. As a result, the layout and the kinematical mechanism of the I-SBW system are quite different from those of the typical steering mechanism. Nevertheless, there is no change in the steering column motor system. In the report, we first describe the structure and control logic of the I-SBW system, and then the control effect on this system as applied for both the HILS system and a vehicle. Furthermore, our HILS system involves the actuator mechanism which realizes the reaction force of the road surface with a minimized frictional force in operation. Therefore, it is possible for us to tune the control logic via the HILS system and confirm the effect of the tuned control logic by applying it to a vehicle with the I-SBW system.

Development of Shift-By-Wire System for an Automatic Transmission Equipped Vehicle (자동변속기장착 차량의 Shift-By-Wire 시스템 개발)

  • Kim, Jung-Yun;Yim, Chung-Hyuk;Lim, Won-Sik
    • Transactions of the Korean Society of Automotive Engineers
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    • v.15 no.4
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    • pp.41-46
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    • 2007
  • This article deals with the design and prototyping of Shift-By-Wire system for an automatic transmission equipped vehicle. In order to manipulate the shifting action electronically, Shift-By-Wire system consists of an electronic shift lever, an electric shift actuator and position sensors. The shift lever is designed to transform the driver's shifting command into an electric signal; it includes the position sensor using non-contact type hall sensor and an additional shifting switch acting as Tip-tronic. For the design of an electric shifting actuator, we investigated the stroke angles and shifting efforts of the manual control lever in each shifting section. And the position sensor of the shifting actuator is designed by using a potentiometer with an optical encoder. Finally the prototype of Shift-By-Wire system was built in a conventional 2.4L class SUV vehicle, and we performed road tests in order to verify its performance.

형상기억합금 스프링을 이용한 2방향 BENDING 액츄에이터의 제작

  • 김명순;이승기;이상훈
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1995.10a
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    • pp.1071-1074
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    • 1995
  • This paper proposes two directional bending actator using three link, two shape memory alloys(SMA) of coil-type springs and two guide wires. By the heating of two SMA springs sequentially, the bending and stretching of the actuator is possible. Bending angle, force and repeated bending motion of actuator were measured and characterized. The performance of the actuator has been characterized for the possible application for catheter.

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Aircraft Digital Fly-By-Wire System Technology Development Trend (항공기 디지털 전자식 비행제어 시스템 기술 개발 동향)

  • Seong-Byeong Chae
    • The Journal of the Korea institute of electronic communication sciences
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    • v.18 no.3
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    • pp.509-520
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    • 2023
  • In this paper, the structure and the characteristics of the Fly-By-Wire system applied to the civil aircraft was described. The development trend of the redundant method of the flight control system, data communication system, control surface actuation system and the control laws implemented by the Fly-By-Wire system of the civil aircraft are discussed. The Fly-By-Wire system was first applied to the fighter and its inherent advantages lead to the advent of the Fly-By-Wire civil aircraft. Recently even the small jet aircraft shows the trend of adopting the Fly-By-Wire system. In the future, most of the aircraft are expected to be the Fly-By-Wire type.