• Title/Summary/Keyword: Discharger

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Soft switched Synchronous Boost Converter for Battery Dischargers

  • Dong, Zhiyong;Joung, Gyubum
    • International journal of advanced smart convergence
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    • v.9 no.2
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    • pp.105-113
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    • 2020
  • In this paper, we proposed a soft switched synchronous boost converter, which can perform discharging the battery, is proposed. The proposed converter has low switching loss even at high frequency operation due to its soft switching characteristics. The converter operates in synchronous mode to minimize conduction loss because of changing the rectified diode to MOSFET with a low on resistance. In this reason, the efficiency of the converter can be greatly improved in high frequency. In this paper, the battery discharger with a switching frequency of 100 kHz, has been designed. The designed converter also simulated to prove the converter's characteristics of synchronous operation as well as soft switching operation. The simulation shows that the proposed converter always meets the soft switching conditions of turning on and off switching in the zero voltage and zero current states. Therefore, simulation results have confirmed that the proposed battery discharge had soft switching characteristics. The simulation results have confirmed that the proposed battery discharger had soft switching and synchronous operation characteristics.

An Analysis of Battery Charger$\cdot$Dischrger using Parallel Connected Bi-directional Converter (대용량 병렬 양방향 컨버터를 이용한 배터리 충$\cdot$방전기 해석)

  • Choi Jae-dong;Ahn Jae-whang;Seong Se-jin
    • Proceedings of the KIPE Conference
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    • 2002.07a
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    • pp.773-776
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    • 2002
  • The battery charger of spacecraft has two different modes of operation respectively. One is the bus voltage regulation mode and the other is the charge current regulation mode. And also the battery discharger provide the power during eclipse mode of spacecraft. In this study, a test model of the battery charger and discharger using hi-directional converter are designed and analyzed. These Battery Charger and Discharger is introduced the modular converter method that can be added the converter modules according to the load variation.

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A development of simulator for satellite power system (인공위성용 전력시스템 시뮬레이텨 개발)

  • 김영태;김희준
    • Journal of the Korean Institute of Telematics and Electronics B
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    • v.33B no.3
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    • pp.193-201
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    • 1996
  • The space power system for communication satellite which employs the direct energy transfer (DET) method consists of solar array, battry, shunt regulator, charger/discharger and power control unit (PCU). In this paper, the development of the DET power system charger/discharger unit and a microprocessor based PCU is developed for simplicity and flexiblity in the modificatin of control algorithm. A 28V bus voltage, 400W power rting power simulator is built and tested to verify the operation of the simulator at each mode and the stability of mode transition is analyzed.

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An Experimental Stduy on NOx Reduction in Exhaust Gas from Diesel Engine with Plasma (플라즈마를 이용한 디젤엔진 배기가스 중의 NOx 저감에 관한 실험적 연구)

  • 조기현;황의현
    • Transactions of the Korean Society of Automotive Engineers
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    • v.7 no.8
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    • pp.83-90
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    • 1999
  • To remove nitrogen oxides(NOx) in exhaust gas of diesel engine, three-way catalytic process with plasma discharger has great possbilities. Characteristics of NOx removal depends on NO conversion to $NO_2$ and/or $HNO_3$ due to high activation energies for NO oxidationand reduction. NOx removal efficiency by using three-way catalytic with plasma dischager indicated about 50% at 40 watt power consumption condition.

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A Research on the Static Discharger Installation Design and Test for Air Vehicle (항공기 외표면 정전기 방출기 장착설계 및 시험에 관한 연구)

  • Woo, Hee-Chae;Kim, Yong-Tae;Kim, Bong-Gyu
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.7
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    • pp.574-580
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    • 2017
  • Static dischargers should be installed on air vehicle to emit a static electricity during flight. Especially, If static electricity is not removed by static discharger on the air vehicle, it makes ionization and corona effect on the edge of antenna and wing. Those phenomenon bring about performance degradation for radio communication and equipment operation. In this paper, the conditions such as climate, air vehicle's speed and frontal area were analyzed to design static dischargers. As a result, the static dischargers would be optimally designed for air vehicles and the performance of the static dischargers can verify according to the functional experiment. Therefore the result of this research will be used to make static discharger installation design for new air vehicle that have different size and mission.

Analysis of the battery charging and discharging system for spacecrafts (인공위성용 총방전 시스템의 해석)

  • 김영태;김희진
    • Journal of the Korean Institute of Telematics and Electronics B
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    • v.32B no.6
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    • pp.932-942
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    • 1995
  • A spacecraft power system can be divided into two types : DET system(Direct Energy Transfer system) and PPT system(Peak Power Tracking system). In a DET system employing the regulated bus voltage control method, the battery charger and discharger are widely used for the bus voltage regulation. The battery charger has two different modes of operation. One is the bus voltage regulation mode and the other is the charge current regulation mode. The battery discharger is employed to provide the power when the spacecraft is in the earth's shadow or the sun is eclipsed. The operating mode, charging or discharging, is selected by a power control circuit. In this paper, small-signal dynamic characteristics of battery charging and discharging system are analyzed to facilitate design of control loop for optimum performance. Control loop designs in various operating modes are discussed. Anaylses are verified through experiments.

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A CHARGER/DISCHARGER FOR MODELING OF SERIAL/PARALLEL CONNECTED NI-MH BATTERY

  • Heo, Min-Ho;Ahn, Jae-Young;Kim, Kwang-Heon
    • Proceedings of the KIPE Conference
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    • 1998.10a
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    • pp.554-559
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    • 1998
  • Equalizing the state of charge of cell that affects the charge/discharge quality and efficiency of the battery through the charge/discharge characteristic experiments of battery source, we develope the high efficiency charge/discharge system which would be used in serial HEV with the constant engine-generator output. For this, establishes the electrical model of Ni-MH battery appropriate to the high efficiency charge/discharge conditions. There is no model of Ni-MH cell, so we used Ni-Cd model and obtain the Ni-MH model through the experiment. A reason that each cell has the same charge/discharge property for applying the cell model to serial/parallel connected battery source extensively is needed. Therefore, in this paper, propose the Ni-MH charger/discharger has the equalization charging function and selectable cut-off function.

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Grid connected 3-phase inverter with photovoltaic generation, battery charger/discharger, and UPS function (태양광 발전-충방전기능-UPS 기능을 갖는 계통 연계형 15kW급 3상 인버터)

  • Kwon, Jungmin
    • 한국신재생에너지학회:학술대회논문집
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    • 2011.11a
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    • pp.50.1-50.1
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    • 2011
  • 전력수요가 적을 때 잉여전력을 저장하고 전력수요가 많은 시간대나 전기료가 비싼 시간대에 저장된 전력을 사용함으로서 전력의 활용 효율을 높이고, 전력공급 시스템을 안정화하기 위해 에너지저장시스템의 연구가 최근에 활발히 진행되고 있다. 또한 공장, 산업용빌딩이나 병원 등 고르고 안정적인 전력의 수요는 늘어나고 있으며, 화석 연료 고갈 문제로 인한 신재생에너지 발전의 중요성도 대두되고 있다. 본 논문에서는 무정전 전원장치, 태양광발전시스템, 에너지 저장 시스템을 모두 통합하였다. 제안한 시스템은 3상 인버터, 부스트 컨버터, 양방향 컨버터, 사이리스터 스위치로 구성된다. 인버터는 계통과 연계되거나 UPS 동작 시 AC 전력을 만든다. 부스트 컨버터는 태양광 패널과 연결되어 MPPT 제어를 수행한다. 양방향 컨버터는 잉여전력을 배터리에 저장을 하고, 전력이 부족할 시에는 배터리의 전력을 방전한다. 사이리스터 스위치는 정전 시 계통과 부하를 끊어주는 역할을 한다. 본 논문에서는 15kW급 시스템으로 구현하여 검증하였다.

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New Secondary Battery Charger/Discharger Available for Zero Voltage Discharge (영전압 방전이 가능한 새로운 방식의 2차전지 충/방전기)

  • Chae, Soo-Yong;Chung, Dae-Taek;Kim, Dong-Wook;Hong, Soon-Chan
    • Proceedings of the KIPE Conference
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    • 2012.07a
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    • pp.250-251
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    • 2012
  • This paper proposes a new secondary battery charger/discharger available for zero voltage discharge which is used for test equipments and formation. The proposed system is able to discharge the battery to zero voltage which does not matter to voltage drop of circuit. The validity of proposed system is verified by experiment.

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