• Proceedings of the KIPE Conference
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• 2018.07a
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• pp.231-233
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• 2018

바나듐 산화 환원 유동 배터리는 긴 수명주기와 높은 에너지효율로 리튬 이온 배터리를 대체할 차세대 배터리로 주목받고 있다. 에너지가 저장되는 전해질을 순환시키면서 충전 과방전이 이루어진다는 이차전지 인 만큼 유지 보수 비용을 획기적으로 절감할 수 있고 사용자의 요구조건에 따라 출력과 에너지 용량을 매우 쉽게 조절할 수 있다는 장점이 있다. 하지만, 바나듐 산화 환원 유동 배터리를 다양한 어플리케이션에 적용하기 위하여 바나듐 배터리 운용에서 여러 가지 요소들을 고려하여야 한다. 본 논문에서는 충전 및 방전을 지속했을 때의 용량 감소하는 바나듐 산화 환원 유동 배터리의 특성을 고려하여 가장 까다로운 문제 중 하나인 휴지 기간에서의 자가 방전에 대해 온도와 SOC에 따라 특성 분석을 실시하였다.

• The Transactions of the Korean Institute of Power Electronics
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• v.7 no.5
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• pp.482-489
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• 2002

This paper studies the stand-alone photovoltaic system for the solar lighting lamp. The solar lighting lamp has PV modules, batteries, and charge & discharge system. The charge efficiency is improved for the control of each battery which is divided the charge from the discharge to change the structure of existing solar lighting lamp charge & discharge system. so, the charge and discharge times are reduced of 50% and the depth of discharge control can be controlled in the discharge cut off voltage. It can be effective of the battery use. If a battery is out of order, this system can be executed for a regular period. So we saved the repair cost and developed of system's stabilization. It Is possible to make economical effects to apply for solar lighting lamp used photovoltaic system.

• Proceedings of the KIPE Conference
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• 2014.11a
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• pp.165-166
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• 2014

위성의 전력 시스템 초기 설계를 위해 고려해야 하는 중요한 설계 요소에는 위성 운용 기간 동안의 전력 소모량 예측 및 전이궤도와 운용궤도에서의 태양 전지판과 배터리의 운용 개념 설계이다. 이를 토대로 태양 전지판에서 생성되는 전력의 정류 개념과 배터리 충전/방전 토폴로지를 구현해야 한다. 본 논문에서는 2.5KW급 정지궤도 위성의 전력 시스템 초기 설계를 위해 고려해야 하는 설계 요소들을 나열하고, 이들에 대한 전반적인 검토 사항을 기술한다.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1994.05a
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• pp.114-117
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• 1994

아연-산화은 전지는 높은 에너지 및 전력밀도를 가지고 있으나 비싼 제작비용 때문에 우주항공, 군사무기 등 특수한 분야에서 주로 이용되며, 특히 전해액이 별도의 용기에 보관되어 있다가 외부 신호에 의해 충전된 dry상태의 전지에 주입되어 활성화되는 1차 또는 비축형 아연산화은 전지는 우수한 고율방전 특성, 장시간의 저장기간 및 활성화와 동시에 부하를 인가 할 수 있는 특성 때문에 많은 무기체계에서 이용하고 있다. 이러한 아연-산화은 전지의 아연전극은 높은 다공도와 반응 면적을 가져야 하며, 특히 방전중 아연전극의 전위는 가역 수소전위 보다 더 음전위이기 때문에 수소가스가 다량 발생하게 되므로 수은과 같은 높은 과전압을 갖는 물질을 첨가하여 가스 발생량을 줄이고 부동태화(passivation)를 억제하게 된다. 그러나 국내 여건상 수은을 사용하여 전지를 제작하는 것은 환경문제 등으로 인하여 어렵기 때문에 본 연구에서는 수은을 사용하지 않고 비축형 아연-산화은 전지의 음극판을 제작하기 위하여 전착법(electro deposit)과 mesh 제작방법을 혼합하여 아연전극을 제작하였으며, 기판에 석출된 아연과 아연 mesh의 질량비율에 따른 전지의 성능을 평가하였다.

• Proceedings of the Korean Information Science Society Conference
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• 2007.10b
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• pp.238-242
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• 2007

일반적인 휴대용 기기와 마찬가지로 모바일 피씨(Mobile PC, laptop)에서도 배터리(Battery)는 빼놓을 수 없는 부분으로 이에 대한 테스트는 매우 중요하다. 배터리에 대한 테스트는 모바일 피씨 개발 시 충전과 방전을 수백 회를 반복하여 수행을 하게 되고, 이 배터리 테스트에 상당한 시간이 걸리게 된다. 컴퓨터 관련 부품의 빠른 발전과 함께 모바일 피씨에 대한 사용자들의 다양한 요구에 의해 모바일 피씨의 종류가 다양하게 분화되고, 또한 개발 기간이 짧아지는 추세에 있다. 이에 따라 많은 시간을 요구하는 배터리 테스트에 대한 개선을 위한 노력이 행하여져 왔다. 본 논문에서는 이러한 개선 사항에 대하여 알아보고, 이를 바탕으로 추가적인 개선점을 제시하고 그에 대한 시스템을 구현하고자 한다.

• Transactions of the Korean Society of Automotive Engineers
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• v.9 no.6
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• pp.40-46
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• 2001

An experimental investigation is proceeded to study on the relationship between spark ignition characteristics and the performances of an S. I. engine. The ignition parameters examined in this study are the ignition energy and discharging duration. The combustion pressure and exhaust gas are measured during the experiment. From the measured data of cylinder pressure, the heat release rate, the mass fraction burned, and the COV of IMEP are calculated. The dwell time and the injection time are varied. A single cylinder engine and a 30kW dynamometer are employed. Four different kinds of ignition systems are assembled, and one commercial ignition system is adopted. The experimental results show that the ignition energy is increased as the dwell time extended until the ignition energy is saturated. The higher ignition energy is effective in achieving the laster burning velocity and less producing HC emission. However, when the amount of ignition energy is similar, while the discharge duration becomes longer, the burning velocity is reduced but the engine operation becomes stable in terms of the COV of IMEP.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.21 no.12
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• pp.339-345
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• 2020

In the field of defense, one-shot devices such as missiles are stored for a long period of time after they are manufactured, so it is essential to predict their storage life. A study was conducted to find the shelf life of a Li-ion battery used in one-shot devices. To do this, a Li-ion battery that has been used in weapon systems for more than 5 years was secured. A non-functional test was performed on the battery to check for external changes or failures. After the non-functional test, a discharge test was performed to measure the performance after storing it. Through the test, the performance was checked, including the initial charging voltage, discharge time, and battery temperature, and the trend of the change was identified. An F-test, One-way ANOVA, and regression analysis were performed to verify the aging, and the shelf life of the battery was estimated by an approximation formula that was derived through a regression analysis. As a result of the ANOVA, the p-value was less than the reference value of 0.05, and the performance of the battery decreased by more than 15% after a certain period of time. This change is assumed to result from the change in physical properties of the lithium polymer cell.

• Journal of Astronomy and Space Sciences
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• v.15 no.2
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• pp.449-458
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• 1998

The Korea Muliti-Purpose Satellite(KOMPSAT) uses a sun-synchronous orbit with an altitude 685km as mission orbit and undergoes earth eclipses and infrequently lunar eclipses. Lunar eclipses occur when the moon is located between the sun and the satellite and blocks partially or fully the sunlight. The eclipse causes the satellite to increase battery discharge times and affects satellite lifetime and mission operation. The KOMPSAT lunar eclipses can cause additional effects to energy balance and battery disc of the KOMPSAT lunar eclipse for 3 year mission lifetime. Also mission planning scenario is presented for lunar eclipses at the KOMPSAT Grouns Station(KGS).

• Aerospace Engineering and Technology
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• v.2 no.1
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• pp.108-116
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• 2003

This research presents the design and analysis of PCDU(Power Control & Distribution Unit) of communication satellite. The PCDU of a spacecraft must provide adequate power to each subsystem and payload during mission life, and it also needs high reliability and performance in space environment. A control circuit of the PCDU include bus sensing and filter circuits, error signal amplification circuit, error compensation circuit of SAS(Shunt Assembly Switch) and BPC(Battery Power Converter). The phase margin and DC gain for the designed circuits are analyzed through the frequency response characteristics of the compensated control circuit. And also the transfer function of the battery power converter circuit are discussed at the battery CCCM(Charge Continuous Conduction Mode) and battery C/DCCM(Continuous/Discontinuous Conduction Mode).

• Journal of the Korea Academia-Industrial cooperation Society
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• v.21 no.3
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• pp.585-593
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• 2020

Until now, 29 fire accidents have occurred; 22 of them were caused by the interconnection of renewable energy sources that occurred during the rest period after the lithium-ion battery had been fully charged regardless of the seasons. The fire accidents of ESS were attributed to thermal runaway due to the overcharging of a few cells with the phenomenon of self-energy balancing, which is unintentional current flow from cells with a high SOC to the low cells if the SOC condition of each cell connected in parallel is different. Therefore, this paper proposes a novel configuration and operation algorithm of the BMS to prevent the self-energy balancing of ESS and presents a hybrid SOC estimation algorithm. From the test results of the self-energy balancing phenomenon between aging and normal cells based on the proposed algorithm and BMS, it was confirmed the possibility of self-energy balancing, which is unintentional current flow from cells with a high SOC to cells with a low SOC. In addition, the proposed configuration of the BMS is useful and practical to improve the safety of lithium-ion batteries because the BMS can reliably disconnect a parallel connection of the cells if the self-energy balancing current becomes excessively high.