• Journal of the Korean Society of Propulsion Engineers
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• v.11 no.5
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• pp.60-71
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• 2007

The startup characteristic of liquid propellant rocket engine should be focused on the stable ignition of combustion chamber and gas generator. Also, to lessen the propellants consumption during this period which doesn't contribute to the flight thrust, the engine has to be transferred to the nominal mode quickly. Because of the risk of test, it is impossible to develop all the startup cyclogram or the specifications of engine by test, so the precedent numerical approach is quite necessary. In this study we developed a mathematical model for the startup phenomena in a liquid rocket engine driven by gas generator-turbopump system based on the commercial 1-D flow system analysis program, Flowmaster. Using this program we proposed a methodology to obtain the specifications of turbine starter and the opening time of shutoff valves for the stable startup of the engine. To verify this methodology we qualitatively compared the analysis results to the typical startup curve of the published engine, then found it is quite well matched.

• Proceedings of the Korea Information Processing Society Conference
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• 2011.04a
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• pp.7-10
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• 2011

본 논문에서는 스마트폰을 이용하여 차량을 원격시동 제어 및 관리하는 원격시동 관리 시스템을 제안한다. 이 시스템은 고가의 차량을 관리 및 제어하는 시스템인 만큼 작동의 신뢰성을 중요시 한다. 그래서 기존의 소형 리모콘 방식의 차량 원격시동 제어관리 시스템을 활용하여 시스템 작동의 신뢰도를 높였으며, 기존의 소형 리모콘 제어 환경에서 스마트폰으로 옮겨옴으로써, 기존의 입력 및 제어의 불편함을 해결하였다. 그리고 기존 존재하는 블루투스와 CDMA를 사용하는 차량 원격시동 제어 관리 시스템의 거리 및 속도, 비용 등의 문제점도 개선하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.23 no.3
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• pp.58-66
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• 2019

In this study, the start-up characteristics of a staged combustion engine were analyzed numerically based on relational equation modeling of the entire engine components. The start-up characteristics were extensively analyzed considering the transient period of the total engine system from the start-up sequence till the steady-state of the engine. The performance characteristics of the engine components such as RPM of engine power-pack, chamber pressure and O/F ratio of pre-burner, and mass flow of propellants in the start-up period were investigated. Furthermore, the calculated engine data were compared satisfactorily with the experimental data. Through the comparison of data, successful validation of present engine start-up analysis has been obtained.

• Proceedings of the KIEE Conference
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• 2008.07a
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• pp.1005-1006
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• 2008

기존의 전자식 안정기 특히 펄스로 시동되는 HID램프용의 안정기에서는 부가적인 시동회로가 필요하게 된다. 하지만 램프 제조업자에 의해 규정된 점화 펄스폭은 제조업자 간에서도 다양하며, 대단히 높게 되어 있으며 그 펄스폭에는 최소 필요한 값이 있고 이것은 통상 $1.5{\sim}2.5us$정도이다. 이와 같은 시동 펄스폭의 조건을 만족하기 위해서는 시동회로 또한 복잡해지고 제작비용도 고가가 된다. 본 연구는 전력소모가 20[%]이상 절감되면서도 광량이 더 많이 방사되는 메탈핼라이드 램프를 UV경화 시스템 즉, LCD, PDP OLED 모듈조립, 평면, 곡면 스크린 인쇄용, 코팅용, 실험용 UV경화 및 UV노광 시스템 등에 사용 가능한 전자식 안정기를 고주파 시동의 이점을 유지해 가면서 지연 시간에 기인하는 램프의 꺼짐 및 대순환 전류의 문제를 해소하고 고압 대용량 램프를 구동할 수 있는 20KW급 전자식 안정기를 제안하여 22KW UV LAMP를 사용하여 전자식 안정기를 구동 실험으로 검증하였다.

• The Transactions of the Korean Institute of Power Electronics
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• v.9 no.1
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• pp.17-24
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• 2004

The starter of the turbo generator is composed of a high speed generator(HSG), an inverter and a boost converter instead of a gearbox, a DC motor and a low-voltage battery in the starter of the turbo shaft generation system. Because turbo generator is needed a high speed motoring at start-up, high speed generator has a low leakage inductance and inverter need a high DC link voltage. In this study, for developing the stater of a turbo generator, a boost converter with a high capacity was developed to convert high voltage from a low battery voltage. And for controlling a high frequency current to be injected to a motor winding with a low leakage inductance, the inverter with a high precision and a high speed operation was designed and for a stable ignition, the starting algorithm of a turbo generator was proposed. Turbo generator was started by the starter developed to verify the performances.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.22 no.2
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• pp.774-780
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• 2021

The auxiliary power unit (APU) of a rotorcraft starts the engine during operation/flying. The APU is composed of a gas turbine engine type. The starting principle of the component is that the electric start motor generates the power required for starting by rotating the shaft. In this study, quality improvement was performed by applying an over-running clutch (ORC) between the APU and the starter motor to secure the operability of the starter motor of the APU mounted on the rotorcraft. The starter motor has the main role of starting the APU, but during operation, it is rotated without load by the rotational force of the APU gear shaft, resulting in friction at the brush. This phenomenon causes abrasion of the brush of the starter motor. Consequently, when the APU operation time increases, the brush life decreases, and the operability of the APU is affected. In this study, an ORC that separates the interlocking between the start motor brush abrasion and the APU operation time was applied to improve the operability/durability of the APU starter motor. The effect was verified through a test, and the technical feasibility of the design change was analyzed.

• Tribology and Lubricants
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• v.26 no.5
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• pp.277-282
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• 2010

The purpose of this paper is to study and analysis the failure examples for parasitic current leakage produced in starting system on gasoline engine. It verified the discharge of battery by electric leakage because of internal wiring damage problem for CD auto changer installed in car. Also, it verified the no-stating phenomenon because of deposit forming by chemical reaction of battery fluid between battery post and cable fixing parts. It verified the damage for brush holder and commutator mixing by internal short phenomenon because of brush carbon a particle and engine oil that was flowed into internal of starting motor. It verified the working phenomenon of audio by a point of contact even if the driver turn to "LOCK" position the key.

• Proceedings of the Korean Society of Computer Information Conference
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• 2022.01a
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• pp.297-298
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• 2022

현재 도로 위 차량은 다양한 기능이 탑재되어 있고, 이는 운전자의 편의와 안전을 위해 발전해왔다. 하지만 음주운전과 안전운전 불이행에 의한 교통사고는 꾸준히 발생하고 있으며, 이 사고율은 단순히 제도적 규제와 운전자의 주의만으로는 감소시키기 어렵다고 판단된다. 본 논문은 제도적인 규범만이 아닌 기계적인 차원에서의 음주운전 사고 예방과 안전운전 불이행 사고의 방지를 하기 위해 '음주측정 시동 및 안전운전 보조시스템'을 제안한다. 이러한 문제를 해결하고자 알코올 측정 센서를 통해 시동을 걸기 전 음주측정을 해 음주운전의 가능성을 차단하고 초음파 센서를 이용하여 전, 후·측방 감지를 하고 주변의 장애물과 운전자의 부주의 시 즉각적인 피드백을 제공해 안전운전 불이행 사고를 방지할 수 있다.

• Proceedings of the Korean Information Science Society Conference
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• 2004.10c
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• pp.595-597
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• 2004

본 논문은 그리드 환경에서 HPC 프로그래임 메커니즘의 성능향상을 위하며 DAG기반의 Co-scheduling시스템의 신뢰성 향상에 관한 것이다. 제안된 Co-Scheduling의 목적은 복수개의 관련된 RPC들의 데이터 입출력 관계를 고려하여 불필요한 네트워크상의 데이터전송을 제거함으로써 전체 RPC의 실행시간을 줄이는 것이다. 사용자로 부터 요청된 어플리케이션을 DAG로 구성하여 실행기반 시스템을 통해 수행된다. 이 논문에서는 신뢰성 향상을 위한 재시동 프로토콜을 구현하여 결함발생시 전체 작업을 정상적으로 완료하기 위한 메커니즘을 소개하고 재시동 프로토콜의 효율성을 검증한다.

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.5
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• pp.54-59
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• 2011

Reliable starting capability of a gas turbine engine calls the engine industry's attention recently. So far the gas turbine engine performance researches have focused on the range between idle to Max rpm, but recent attention on the starting has brought interests in the range of "Sub-dile". As component characteristic maps are essential for the starting research, various kinds of studies have been doing and proposing ways to expand the existing maps toward sub-idle range. In this paper, previous studies were discussed and a new method suggested and validated.