• 한국군사과학기술학회지
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• 제20권4호
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• pp.536-542
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• 2017

In this paper, authors described on localization development's results about an electric igniter in thermal battery with a pyrotechnic heat sources. Especially, the development test and evaluation(DT&E) process and the methods in the developments of the electric igniter which is parts of a domestic thermal battery on K-PSAM was in charge of government and developed for defense of a local areas in Korea. We have proposed a process of design and manufacture on the electric igniter. Finally, we verified a quality and a reliability of the electric igniter from test results by Fisher-Snedecor's law and over 99.5 %(C.L. 95 %) for K-PSAM.

• 전기저널
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• 1호통권121호
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• pp.20-25
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• 1987

• 한국연소학회지
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• 제22권2호
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• pp.36-41
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• 2017

Aero gas turbine engines must demonstrate their ability to be ignited on ground conditions or relighted in flight. The electric spark ignition is usually used in current aero gas turbine engines. Experiments on ignition characteristics relating to spark igniter penetration depth under atmospheric pressure and temperature conditions were conducted on the model combustor which is scaled in 1/18. Exciter was operated during 2 seconds, and successful ignition phenomena were confirmed by the pressure rising sharply in combustor. In addition, instantaneous ignition images were captured by a high-speed camera. It showed kernel propagation and successful ignition events in the sector model combustor. Ignition test results showed that ignition limit with increase in penetration depth of the igniter plug was wider. When the penetration depth of the igniter plug increased under the same fuel injection pressure condition, successful ignition events were obtained in higher differential pressure conditions between inlet and outlet of the combustor. The results demonstrate that the ratio of the combustible mixture, which is exposed to the high temperature environment around the igniter plug tip, increases. Thereby affect the combustor ignition performance.

• 한국추진공학회지
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• 제19권1호
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• pp.1-8
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• 2015

MEMS 추력기를 위한 유리 박막 마이크로 점화기를 개발하였다. 수십 마이크로 미터의 두께를 가지는 유리 박막을 사용하여 점화기의 구조적 안정성을 향상시켰다. 마이크로 점화기는 박막 형성을 위한 감광 유리의 이방성 식각과 점화 코일 형성을 위한 Pt/Ti 증착 공정으로 제작되었다. 개발된 점화기는 유리 박막의 구조적 안정성으로 인하여 특별한 장치없이 추진제 충전이 가능하였다. 점화 실험이 성공적으로 이뤄졌으며 최소 점화 지연은 27.5 ms, 최소 점화 에너지는 19.3 mJ 이였다.

• Advances in aircraft and spacecraft science
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• 제7권5호
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• pp.425-440
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• 2020

The work presented herein is a numerical investigation of the flow field inside a resonant igniter, with the aim of predicting the performances in terms of cavity temperature and noise spectrum. A resonance ignition system represens an attractive solution for the ignition of liquid rocket engines in space missions which require multiple engine re-ignitions, like for example debris removal. Furthermore, the current trend in avoiding toxic propellants leads to the adoption of green propellant which does not show hypergolic properties and so the presence of a reliable ignition system becomes fundamental. Resonant igniters are attractive for in-space thrusters due to the low weight and the absence of an electric power source. However, their performances are strongly influenced by several geometrical and environmental parameters. This motivates the study proposed in this work in which the flow field inside a resonant igniter is numerically investigated. The unsteady compressible Reynolds Averaged Navier-Stokes equations are solved by means of a finite volume scheme and the effects of several wall boundary conditions are investigated (adiabatic, isothermal, radiating). The results are compared with some available experimental data in terms of cavity temperature and noise spectrum.

• 조명전기설비학회논문지
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• 제18권5호
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• pp.9-15
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• 2004

메탈핼라이드 램프의 가장 큰 단점중 하나는 아크튜브가 뜨거운 상태에서는 순시 재점등이 불가능하다는 것이다. 메탈핼라이드 램프의 점등중 고온의 아크튜브는 초기 램프가 차가운 상태에서의 방전 전압보다 재점등 방전전압이 높아 재점등 시키는데 압력과 온도가 감소되어지는 약5분정도의 시간이 소요 된다. 만약 램프가 뜨거운 상태에서 재점등시키려면 램프전극 양단에 약20[kV] 이상의 높은 전압펄스를 공급해야한다. 따라서 이러한 목적의 전자식 안정기는 EMII필터, PFC회로, 플라이백 컨버터, 하프브리지 인버터, 고전압 이그나이터 회로로 구성되는데 이것은 순시점등은 물론 램프가 뜨거운 상태에서도 20[kV]의 전압으로 램프를 점등/재점등 할 수 있다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2009년도 제40회 하계학술대회
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• pp.940_941
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• 2009

Dual Buck Inverter구조를 가지는 70W CDM 램프용 전자식 안정기의 제어기를 설계하였다. 전자식 안정기는 EMI filter, Active PFC, Dual Buck Inverter, Igniter, SMPS로 구성 된다. 제어기는 크게 2개로 구분 할 수 있다. MC33262를 이용하여 Inverter의 전압, 전류를 센싱 받아 70kHz의 Zero Voltage Switching을 위한 제어기와 시간의 경과에 따라 PFC의 출력 전압 제어, Ignition Pulse 제어 및 무부하 보호를 위한 제어기로 구성되어 있다. 본 논문은 ATmega8을 이용하여 제어기를 설계하였고 실험으로 시간의 경광 따른 안정기의 제어가 안정적인 동작을 하고 있음을 증명하였다.

• 한국조명전기설비학회:학술대회논문집
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• 한국조명전기설비학회 2003년도 학술대회논문집
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• pp.185-190
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• 2003

The most shortcoming of metalhalide lamps is what the instant restarting cannot be realized when the arc tube is in the hot condition. The discharge starting voltage of arc tube in the hot condition is much higher than in the cold condition. Therefore it takes about five minutes to restart the metalhalide lamps, that is to say, it is possible to start when the pressure and the temperature are decreased. But, if the lamp is restarted in the hot condition, we must supply the high voltage pulse with 20kV at the both sides of lamp. The proposed electronic ballast is consist of a electromagnetic interference (EMI) filter, a power factor correction (PFC) circuit, a flyback converter, a half-bridge inverter, and a high voltage igniter circuit. By this composition we can restart the lamp with the voltage 20kV, even if the lamp is in the hot condition.