• 제목/요약/키워드: 구동 장치

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Power Conversion System for Electric Power Take-off of Agricultural Electric Vehicle (농업용 전기차량의 전기식 동력인출장치용 전력변환시스템)

  • Kwak, Bongwoo;Kim, Jonghoon
    • Journal of IKEEE
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    • v.23 no.3
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    • pp.994-1002
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    • 2019
  • In this paper, we propose the development of a power conversion system for electric power take-off (e-PTO) of agricultural electric vehicles. Most e-PTOs use commercial power $220V_{AC}$. A bidirectional power conversion system having a two-stage structure consisting of a DC-DC converter and a DC-AC inverter for supplying a high output voltage using a low battery voltage of an agricultural electric vehicle is suitable. we propose a power conversion system consisting of the one-stage dual active bridge (DAB) converter and the two-stage bidirectional full bridge inverter. In addition, we propose a soft start algorithm for reducing the inrush current generated by the link capacitor charging during the initial operation. A 3kW prototype system and its corresponding algorithms have been implemented to verify its effectiveness through experiments.

M4 Semi-Freejet Test with Full-scale Vehicle Model (실기체급 비행체 모델에 대한 M4 준자유류 시험)

  • Juhyun Bae;Changwon Lim;Hojin Choi;Sangwook Jin;Jeongwoo Kim
    • Journal of the Korean Society of Propulsion Engineers
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    • v.26 no.5
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    • pp.63-73
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    • 2022
  • Investigation on operation of the test apparatus for the M4 semi-freejet tests with a full-scale vehicle model was carried out utilizing domestic facilities. An integrated design of the experimental apparatus and the vehicle model was obtained through iterative computational fluid dynamics (CFD) analysis. The test results showed that the M4 nozzle of the apparatus was fully expanded to provide required test conditions. It was also found that the intake of the vehicle model successfully started, and the corresponding shadowgraph images were recorded during the test. A variable nozzle of the model was set to adjust the back pressure of the model combustor, and wall-static pressures were measured to obtain the pressure distribution at the main locations of the model. The flame of torch ignitors and pilot fuel ignition were observed in a flame-holder of the combustor.

Development of Marking Robot by using Arc Welding for Shipbuilding (조선 적용을 위한 문자마킹 자동용접장치 개발)

  • Park, Chul-Sung;Park, Jin-Whi;Ryu, Young-Soo;Lee, Jeong-Soo
    • Proceedings of the KWS Conference
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    • 2009.11a
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    • pp.3-3
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    • 2009
  • 선박의 건조과정에서 필수적으로 선체 외판에는 선박의 안전과 운항 및 정비 등에 필요한 정보를 나타내기 위해 다양한 종류의 마크 및 문자가 마킹되어진다. 하지만, 단순한 도장 작업만으로는 해상과 같은 부식 환경에서 마크 및 문자가 쉽게 지워지거나 손상되기 때문에 마크 및 문자를 용접 비드(welding bead)로 표시하거나 미리 절단된 강판(steel plate)을 수동으로 용접한 뒤 도장을 함으로써 마크 및 문자의 손상을 방지하고 있다. 이러한 문자마킹작업을 하기 위해서는 작업자가 수작업으로 기준선과 마크 및 문자의 위치를 먹줄 등을 이용하여 마킹을 하고, 해당 마크 및 문자의 템플렛(template)을 이용하여 펀칭을 실시한 후 수동으로 용접을 실시한다. 하지만, 수작업을 통한 선체외판 문자마킹 작업은 작업자의 기량에 따라 품질이 상이하여 품질 저하의 원인이 된다. 또한 대조립 및 탑재 단계에서 문자 마킹 작업시 수직자세의 용접을 요구함으로써 작업자가 안전사고에 노출되어 있으며, 선박의 각 단계별 주요 공정보다 작업시간이 길어져 전체 선박 건조공정을 지연시키는 문제점 등을 야기시킬 수 있다. 이러한 문제점들을 해결하기 위해 조선업계에서는 선체 외판의 마크 및 문자를 자동으로 용접할 수 있는 장치를 개발하기 위해 노력해왔으며, 몇몇 개발 사례가 보고되고 있다. 하지만, 그 실효성 부분에서는 아직까지 해결하지 못한 문제점들로 인해 현장 적용에는 어려움을 보이고 있다. 본 연구에서는 선박외판 문자 자동용접장치의 기능성뿐만 아니라 현업 적용성을 가장 우선적으로 고려하여 문자마킹장치(Marking Robot for Shipbuilding) 개발을 진행하였다. 우선, 적절한 용접 재료를 선정하기 위해서 솔리드 와이어(Solid Wire)와 플럭스 코어드 와이어(Flux Cored Wire)에 대한 비드온 용접(Bead-On Welding)을 아래보기자세와 수직자세에 대해서 실시하여 적절한 용접 조건을 설정하였다. 본 연구에서 개발된 문자마킹 자동용접장치는 3축으로 구성되어 있으며 각 축들을 분리할 수 있도록 개발하여 이동성을 향상시켰으며, 작업면과 용접토치간의 거리를 일정하게 유지시킬 수 있도록 용접전류 센서(Welding Current Sensor)를 이용하여 토치 높이(Wire Extension)를 제어함으로써 균일한 품질의 용접비드를 얻을 수 있었다. 또한 문자마킹 자동용접장치는 본체 구동부와 제어부(Touch Screen)가 쉽게 분리되고 장착이 가능한 구조로 개발되었으며, 용접시 각 용접자세별로 용접전압, 전류 그리고 용접속도 설정이 가능하여 아래보기 자세뿐만 아니라 어떠한 자세에서도 같은 모양의 비드형상을 가지는 문자마킹용접이 가능하도록 개발하였으며, 이는 실험과 현장적용을 통해 검증하였다.

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A Study on Design of Vacuum Silo for Batch Treatment System for Dredged Soil (준설토 일괄처리시스템을 위한 진공사이로 설계에 관한 연구)

  • Kim, Yong-Seok;Yang, Hae-Rim;Kim, Hac-Sun;Jeoung, Chan-Se;Yang, Soon-Yong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.36 no.5
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    • pp.571-577
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    • 2012
  • In this study, a small movable batch treatment system for dredging soil deposited in a rain water tube is proposed; further, a vacuum silo sorting separation device with a vacuum silo, first-stage sorting separator, and conveyor is designed. The vacuum silo sorting separation device also consists of a storage tank, transferring screw, vacuum gate, screen bar, screen bar cleaner, and vacuum discharging device. In view of the fact that the flow of drawn air in the storage tank is a major factor influencing the sorting separation performance, the optimum shape of the tank is determined by CFD flow analysis. In addition, by using CAE structure analysis, the safety of a storage tank made of boards is examined. The specifications of the vacuum silo sorting separation device are determined by conducting mechanical and dynamic simulations of the driving mechanism of the vacuum silo sorting separation device through 3D-CAD modeling. Following this study, we will design a drum-screen-type second sorter, a decanter-type dehydration device, and waste water tank and pump as a secondary device. Further, on the basis of this design, we will construct a prototype model and carry out a field test.

A Study on the Determination of Slot's Number of Rotor to Reduce Noise and Vibration and Design the 3-Phase Induction Motor Considering Kinetic Energy in Flywheel Energy Storage System (운동 에너지를 고려한 Flywheel Energy Storage System 설계와 진동 저감을 위한 3상 유도기의 슬롯수 산정에 관한 연구)

  • Ryu, Jae Ho;Kim, Hui Min;Lee, Chee Woo;Park, Gwan Soo;Jeong, Dong Wook
    • Journal of the Korean Magnetics Society
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    • v.27 no.1
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    • pp.1-8
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    • 2017
  • Flywheel Energy Storage System (FESS) is composed by flywheel generating rotating potential energy and motor/generator set charging and discharging electric potential energy. The flywheel and motor/generator is connected by rotating shaft. And torque characteristics of motor/generator part can influence charging and mechanical traits of FESS. This paper analyze about motor/generator design method of 5 [kWh] FESS and torque ripple, harmonic effects by change of slots. At First, this paper proposes a method to estimate the flywheel size and the rotor size of the motor from the the rotational kinetic energy by inertia of FESS. The number of induction motor rotor slots for torque ripple reduction in the high speed operation region is selected. This paper performs to reduce the noise and vibration of the flywheel composed of coaxial with motor/generator and flywheel and realize the high efficiency.

A Prototype Design of the Control Rod Drive Mechanism for Nuclear Power Plants (원전용 제어봉 구동장치 원형 설계)

  • Lee, J.M.;Kweon, S.M.;Pyon, H.S.;Kim, K.H.;Chang, K.C.
    • Proceedings of the KIEE Conference
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    • 2002.07b
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    • pp.638-640
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    • 2002
  • This paper introduces the design method of a Control Rod Drive Mechanism that consists of 3 coils -lift, movable gripper and stationary gripper coil. The vertical attraction forces of the lift, movable gripper, and stationary gripper armatures are calculated by FEM, then the dynamics with full load is demonstrated.

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Hall Sensor Fault Detection and Fault-Tolerant Control of High-Speed PMSM Drive System (고속 영구자석 동기전동기 구동장치의 홀센서 고장검출 및 보호제어)

  • Jang, Myung-Hyuk;Lee, Kwang-Woon
    • The Transactions of the Korean Institute of Power Electronics
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    • v.18 no.3
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    • pp.205-210
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    • 2013
  • This paper presents a novel hall sensor fault detection and fault-tolerant control method for a high-speed permanent magnet synchronous motor (PMSM) drive system. A phase locked loop (PLL) type position estimator is used with a conventional interpolation based rotor position estimator to reduce position errors due to misalignment of hall sensors. The expected trigger time of hall sensor's output is used for detecting hall sensor fault condition and the PLL type position estimator is reconfigured for fault-tolerant control at the hall sensor fault condition. The proposed method can minimize current ripples during the transition from sensored control using hall sensors to sensorless control. Experimental results have been proposed to prove the validity of the proposed method.

A Study on the Manufacture of Single Axis Tracking Solar Power Generation System for BIPV (BIPV를 위한 단축 구동 태양광 전력 발생장치 제작에 관한 연구)

  • Cho, Jae-Cheol;Lee, Jin
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.61 no.2
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    • pp.335-338
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    • 2012
  • Recently, the energy has been used much more than ever, but there has been many problems including atmospheric pollution. So we need alternative energy resources, which are solar heat, solar light, wind power, small water power, etc. The field, which is most popular these days, is the energy source by solar light which transform electric energy using the solar cell and it is available with many researches. In this paper, we manufactured the solar power generation system over 90W using solar module which was 9.90V for Voc, 0.93 A for Isc, 8.64 V for Vmp, 0.75 A for Imp, 6.5 W for power. System was controlled by step motor with worm gear to operate optimum condition between $0^{\circ}{\sim}70^{\circ}$ angle. This system was very effective in tracking space use because it need less space than general solar module.

PWM 압전 변압기의 위상 및 펄스폭 제어

  • Yun, Seok-Taek;Park, Hong-Won;Won, Yeong-Jin;Lee, Jin-Ho;Kim, Jin-Hui
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2009.11a
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    • pp.223-223
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    • 2009
  • 압전 변압기(PT)는 전자제품의 전원 공급 장치에서 마그네틱 변압기의 대안으로서 소형화와 높은 절연 내압의 특성 등을 가지고 있다. 이는 시스템의 소형화와 절연 특성을 크게 높일수있는 장점을 지니고있다. 본 논문에서는 고정주파수 펄스폭 변조 압전 변압기의 구동을 위해, AM modulation을 이용한, 한 점에서의 센싱을 통한 위상제어와 펄스폭 변조 제어를 제안하였다. 이를 위해 EDF 소신호 분석을 하였고, 루프를 설계하여 검증하여 보았다.

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QFT application on force controller design for aircraft control surface load simulator (항공기 조종면 부하재현 구동장치의 force control)

  • 남윤수;이진영;이기두
    • 제어로봇시스템학회:학술대회논문집
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    • 1997.10a
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    • pp.1684-1687
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    • 1997
  • A dynamic load simulator which can reproduce on-ground the hinge moment of aircraft control surface is and essential rig for the loaded performance test of aircraft test of aircraft acutation system. The hinge moment varies wide in the aricraft flight enveloped depending on specific flight condition and maneuvering status. To replicate the wide spectrum of this hinge moment variation within some accuracy bounds, a force controller is designed based on the Quantiative Feedback Theory (AFT). Through the analysis on hinge moment dynamics, a design specification for the force controller is suggested. The efficacy of QFT force controller is verivied by simulation, in which combined aricraft dynamics/flight control law and hydraulic actuation system dynamics of aircraft control surface are considered.

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