• Title/Summary/Keyword: ignitor

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Development of Ignitor of Open-Type Propulsion Device for Korean Interceptor (대응탄 개방형 추진장치용 점화기개발)

  • Kwon, Soon-Kil;Kim, Chang-Kee;Yun, Sang-Yong
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.6
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    • pp.1166-1170
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    • 2011
  • For developing the ignition device for the interceptor of Korean active protection system, the design parameters of the ignition device which should have a short ignition delay time and sufficient energy for propellant ignition were studied. The electric primer instead of mechanical primer was adopted for deceasing delay time, and ignition code was used for decreasing the time difference of flame propagation from the flame holes. The developed ignition device showed the ignition delay time of a few ms. When the designed ignition device was applied to the open-type propulsion devices, the stable interior ballistic characteristic was showed in a firing test.

A Study on the Development of Electronic Lighter Epoxy Injuction Machine (전자 라이터용 에폭시 정량공급장치의 개발에 관한 연구)

  • Park, Jung-Su;Jung, Won;Chang, Seok-Jin
    • Journal of Korea Society of Industrial Information Systems
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    • v.5 no.3
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    • pp.51-55
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    • 2000
  • It is automation of manufacturing process that improve productivity, quality level and delivery times in manufacturing environment. Epoxy injection process is very critical process of manufacturing electronic lighter and then controling the quantity of epoxy fluid is another critical factor of them. As development of epoxy injection machine, the product goal is accomplished and maximize the profit of company. The object of this study is implement the mathematical equation to practical examination with this machine.

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Design of Electronic Ballast Reducing Acoustic Resonances Phenomina in Metal Halide Discharge Tube (메탈 할라이드 방전관 내의 음향 공명을 감소시킨 전자식 안정기 설계)

  • 김기정;박종연
    • The Transactions of the Korean Institute of Power Electronics
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    • v.4 no.5
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    • pp.405-412
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    • 1999
  • Meta! Halide Discharge(]\1HD) Iamps have good color rendition, long life and good focusing capability but h have flickers bv acoustic resonances. We have designed the electronic ballast for reducing acoustic resonances in high pressure discharge tube. The ballast consists of main two parts, the first part is a half-bridge inverter to make a square wave form a and the st'Cond part is a flyback converter to combine the low frequency and high frequency component. As a r result of this study, we conclude that MHD lamps of 70 watt 따c very well light(D without acoustic resonance p phenomena by the elestronic ballast.

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Development of Electronic Ballast for Metal Halide Lamp wilts Free Voltage Input (프리볼트입력용 메탈핼라이드램프 전자식안정기 개발)

  • 김기정
    • Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.16 no.1
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    • pp.20-26
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    • 2002
  • HID(high intensity discharge)lamps include high pressure mercury lamp, high pressure sodium lamp and metal halide lamp. Metal halide lamps have been considered to be one of the most erective light sources. These lamps have good efficiency, good color rendering and good focusing capability. The objective of this research is to alum on the metal halide lamp(MH70W) by the developed electronic ballast with free voltage input(AC 100∼277V). The developed electronic ballast consists of a free voltage input converter, a flyback converter & half-bridge inverter, ignitor & protector and control1er. Experimental results show that developed electronic ballast turns on the metal halide lamp(MH70W) with free voltage input(AC 100∼277V) very well.

Determination of Cyclogram for Liquid-Propellant Rocket Engine

  • Ha, Seong-Up;Kwon, Oh-Sung;Lee, Jung-Ho;Kim, Byoung-Hun;Kang, Sun-Il;Han, Sang-Yeop;Cho, In-Hyun;Lee, Dae-Sung
    • International Journal of Aeronautical and Space Sciences
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    • v.3 no.2
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    • pp.59-66
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    • 2002
  • A vertical test stand based on launcher propulsion system was constructed and several tests for the determination of cyclogram were carried out. To make an accurate estimation, static and dynamic pressures were measured and analyzed. Especially, static pressure measurements using fast response sensors without extension tubes were used to determine operation sequence more evidently. The standard operation times of final valves were determined in cold flow tests with an engine head, and fire formation time in combustion chamber was checked in an ignition test with an ignitor only. On the basis of these tests, ignition sequence was established and combustion test cyclogram was finally determined. According to combustion test, test results were well matched with the determined cyclogram within 0.05 sec.

Study of a Pressure Tube for Measuring pressure of a Solid Rocket Motor at High Altitude Environment (고고도환경을 고려한 SRM 압력계측배관에 관한 연구)

  • Lee, Dong-Won;Lee, Won-Bok;Koh, Hyeon-Seok;Kil, Gyoung-Sub
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.05a
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    • pp.53-56
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    • 2008
  • When someone measuring for pressure of a Solid Rocket Motor(SRM) at Static Firing Test, generally, used with pressure tube to be filled in Oil. But, if you used pressure tube with oil, you were worried about possibility of spilled oil when you measured pressure in SRM at high altitude environment. Because it usually connected at ignitor. In this paper, We described how to make a pressure tube without oil and matters to be attended to design it.

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Ignition and Extinction Characteristics of a Low Thrust Combustion Chamber using Green Propellant according to Sequence of the Combustion Test (친환경 추진제를 사용하는 저추력 액체로켓엔진의 연소시험 시퀀스에 따른 점화 및 소염 특성)

  • Kim, Young-Mun;Jeon, Jun-Su;Choi, Yu-Ri;Ko, Young-Sung;Kim, Yoo;Kim, Sun-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.130-133
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    • 2009
  • The sequence of the propellant supply is very important for the reliable and safe operation of a LRE combustion test. So combustion performance tests were performed to find an optimum test sequence by changing supply time of propellants and purge gas in the moment of ignition and extinction. The liquid rocket engine consisted of a catalytic ignitor and six swirl-coaxial injectors which used hydrogen peroxide and kerosene. Conclusively, an optimum sequence was found for stable combustion in the moment of ignition and extinction.

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A Study on Acceleration Aging Characteristics of B-KNO3 Igniter (B-KNO3 점화제의 가속 노화 특성 연구)

  • Paik, Jong Gyu;Ryu, Byung Tae;Kwon, Mira
    • Korean Chemical Engineering Research
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    • v.52 no.2
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    • pp.166-174
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    • 2014
  • This research investigated the aging properties of the $B-KNO_3$ system as the igniter. The $B-KNO_3$ system showed the degradation in ignition properties depending on the method and period of storage. It should be found out the cause of the degradation to predict the reliability of the igniters. The changes of the properties by the degradation after aging tests were analyzed by microstructure analysis, XRD analysis and thermal analysis using DSC. It was found out that the lattice parameters of the $KNO_3$ as the oxidizer in the ignition system was changed into the JCPDS values as the aging time increased. Conclusively, the changes of the crystal structure of oxidizer affected the activation energy increasing as aging time increased.

The Electronic Ballast Design of Acoustic Resonance Free and Transient Over Current Limit for High Power MHL (음향 공명 제거 및 과도 상태 전류를 제한시킨 고출력 메탈 헬라이드 램프용 전자식 안정기 설계)

  • Kim, Ki-Nam;Park, Jong-Yun;Choi, Young-Min
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.59 no.5
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    • pp.904-911
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    • 2010
  • This paper presents the design of acoustic resonance free and over current limit during transient state consideration electronic ballast for 1.5kW Metal-Halide Lamp(MHL) that employs frequency modulation (FM) technique. The proposed ballast consists of a Full-Bridge(FB) rectifier, a passive power factor correction (PFC) circuit, a full-bridge inverter, an ignitor using LC resonance and a control circuit for frequency modulation. The frequency modulation technique is the most effective solution to eliminate acoustic resonance among other technique. It spreads power spectrum of lamp to reduce the supplied power spectrum under the energy level of eigen-value frequency. Moreover, the proposed ballast is simple and cost effective above conventional ballast. A new PFC circuit is proposed which combines with LCD type and PCSR filter. A new PFC circuit has higher PF and lower THD than conventional LCD type and secure high reliability. Finally, to protected switching components in transient state, the surge current into ballast is limited by increase the switching frequency. Performance of the proposed ballast was validated through computer simulation using Pspice, experimentation and by applying it to an electronic ballast for a prototype 1.5kW MHL.

Design Method of Adaptive Ignitor for HID Lamps (HID 램프를 위한 상태 적응형 점화기 설계 방법)

  • Jo, Gye-Hyun;Song, Myoung-Suk;Park, Chong-Yeun
    • Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.18 no.3
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    • pp.7-14
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    • 2004
  • The metal halide lamps are now widely used in the application and commercial lighting due to their attracting properties such as good color rendering and high efficiency. But, they have a serious problem of acoustic resonance using high frequency operation and they need a high voltage to ignite. So, they have not been applied to indoors. Over the past few years, a considerable number of studies have been conducted on the electronic ballast with hot restarting and resonance phenomenon. But, Very few attempts have been made at adaptive ignition method according to lamp state. In this paper is proposed electronicballast for metal halide lamps with an igniter for adaptive ignition. The proposed electronic bllast can generate a different ignition voltage according to the arc tube state.