• Title/Summary/Keyword: 소염기

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A Study on Designing Flash Suppressor for Reducing Muzzle Flash (총구화염저감용 소염기 설계에 관한 연구)

  • Lee, Joon-Ho;Chae, Je-Wook;Lee, Sung-Bae;Kim, Hyun-Jun
    • Journal of the Korea Institute of Military Science and Technology
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    • v.12 no.2
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    • pp.146-151
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    • 2009
  • It is known that muzzle flash can be generated by the reaction between the oxygen in the air and unburned gunpowder contained in the propellant gas if a barrel is not long enough to burn gunpowder fully inside of the barrel. A hugh muzzle flash, which is a characteristic of small arms with short barrel length, disturbs a shooter in aiming at the target at night by making the shooter blind for a while and endangers the shooter's life by revealing firing position to enemies. In addition, the heat of muzzle flash can deteriorate the performance of thermal sights, which are attached to small arms for effective night combat. In this paper, flash suppressors of different shapes were designed for a newly developed 5.56mm caliber rifle with short barrel length and the performance of each flash suppressor to reduce the muzzle flash was compared by on-site test firing. Through the test firing, a highly efficient design of flash suppressor for reducing the muzzle flash was identified. The result of the paper can be referred when designing flash suppressors for small arms with short barrel length.

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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Thermal and Chemical Quenching Phenomena in a Microscale Combustor (II)- Effects of Physical and Chemical Properties of SiOx(x≤2) Plates on flame Quenching - (마이크로 연소기에서 발생하는 열 소염과 화학 소염 현상 (II)- SiOx(x≤2) 플레이트의 물리, 화학적 성질이 소염에 미치는 영향 -)

  • Kim Kyu-Tae;Lee Dae-Hoon;Kwon Se-Jin
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.30 no.5 s.248
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    • pp.405-412
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    • 2006
  • In order to realize a stably propagating flame in a narrow channel, flame instabilities resulting from flame-wall interaction should be avoided. In particular flame quenching is a significant issue in micro combustion devices; quenching is caused either by excessive heat loss or by active radical adsorptions at the wall. In this paper, the relative significance of thermal and chemical effects on flame quenching is examined by means of quenching distance measurement. Emphasis is placed on the effects of surface defect density on flame quenching. To investigate chemical quenching phenomenon, thermally grown silicon oxide plates with well-defined defect distribution were prepared. ion implantation technique was used to control defect density, i.e. the number of oxygen vacancies. It has been found that when the surface temperature is under $300^{\circ}C$, the quenching distance is decreased on account of reduced heat loss; as the surface temperature is increased over $300^{\circ}C$, however, quenching distance is increased despite reduced heat loss effect. Such abberant behavior is caused by heterogeneous surface reactions between active radicals and surface defects. The higher defect density, the larger quenching distance. This result means that chemical quenching is governed by radical adsorption that can be parameterized by oxygen vacancy density on the surface.

Thermal and Chemical Quenching Phenomena in a Microscale Combustor (I) -Fabrication of SiOx(≤2) Plates Using ion Implantation and Their Structural, Compositional Analysis- (마이크로 연소기에서 발생하는 열 소염과 화학 소염 현상 (I) -이온 주입법을 이용한 SiOx(≤2) 플레이트 제작과 구조 화학적 분석-)

  • Kim Kyu-Tae;Lee Dae-Hoon;Kwon Se-Jin
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.30 no.5 s.248
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    • pp.397-404
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    • 2006
  • Effects of surface defect distribution on flame instability during flame-surface interaction are experimentally investigated. To examine chemical quenching phenomenon which is caused by radical adsorption and recombination processes on the surface, thermally grown silicon oxide plates with well-defined defect density were prepared. ion implantation technique was used to control the number of defects, i.e. oxygen vacancies. In an attempt to preferentially remove oxygen atoms from silicon dioxide surface, argon ions with low energy level from 3keV to 5keV were irradiated at the incident angle of $60^{\circ}$. Compositional and structural modification of $SiO_2$ induced by low-energy $Ar^+$ ion irradiation has been characterized by Atomic Force Microscopy (AFM) and X-ray Photoelectron Spectroscopy (XPS). It has been found that as the ion energy is increased, the number of structural defect is also increased and non-stoichiometric condition of $SiO_x({\le}2)$ is enhanced.

Raumliche flammenausbreitung und "flame quenching" bei ottomotorischer verbrennung (오토엔진의 공간적 화염전파와 "Flame Quenching")

  • Pischinger, F.;Spicher, U.
    • Journal of the korean Society of Automotive Engineers
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    • v.6 no.3
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    • pp.58-67
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    • 1984
  • 공간적 화염전파에 대한 실험적인 파악을 통하여 오토엔진에서의 연소과정과 진행을 위한 깊은 통찰을 할 수 있다. 그것을 통하면 매우 희박한 공기, 연료 혼합기의 경우 실린더에서 직접소염 과정을 확인할 수도 있고 hydrocarbon의 불완전 연소와 나타나는 qunching zone간의 관계를 조사할 수도 있다. 광전도 섬유기술(Lichtleit-fasertechnik)을 사용하여 새로 개발된 측정방법을 이용하여 단기통 오토엔진에서 화염면의 공간적인 전파과정과 매우 희박한 공기 연료 혼합기 에서의 quench zone의 출현을 조사하였다. 측정결과들은 공기연료 혼합기가 희박해 질수록 화 염전파 과정이 점점 느려지는 것을 보여준다. 아주 높은 공기 과잉율을 갖는 엔진 운전에서는 화염속도와 연소속도가 매우 급하게 감소한다. 그리하여 화염면은 팽창 단계에서 상대적으로 증가하는 피스톤속도 때문에 더이상 피스톤을 따를 수가 없으며 그로 인해 직접 피스톤상부에 소염대가 형성된다. 그에 의해 배기가스에서의 hydrocarbon 방출의 급격한 증가와 효율이 급격히 감소하는 엔진 운전과 관련이 지어진다.

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A Study on Designing Flash Hider to Shorten the Length of Small Arms (전장축소형 무화염 소염기 형상설계 연구)

  • Kim, Hyun-Jun;Lee, Joon-Ho;Chae, Je-Wook;Lee, Sung-Bae;Kim, In-Woo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.6
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    • pp.979-985
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    • 2011
  • This paper includes that there are results of designing the flash hider and analyzing fluid dynamics of a front area of the barrel to shorten the length of small arms. Generally, the muzzle flash can be generated out of the barrel by the reaction between the oxygen in the air and unburned gunpowder contained in the propellant gas if a barrel is not long enough to burn gunpowder fully inside of the barrel. Though, the hugh muzzle flash, which is a characteristic of small arms with short barrel length, caused a soldier to aim at the target at night by making the soldier blind for a while and endangers his life by revealing firing position to enemies. Besides, the heat of muzzle flash can weaken the performance of thermal sights, which are attached to small arms for night battlefield. In this paper, flash hiders with several different shapes were designed for a newly developed 5.56mm caliber rifle with short barrel length. The performance of each flash hider to reduce the muzzle flash was compared theoretically and experimentally. Through the authorized test procedure, a highly efficient design of flash hider for reducing the muzzle flash was identified. The result of the paper can be helpful when designing flash hiders for small arms with short barrel length.

Effect of Scale and Fuel Type on Heat-recirculating Swiss-roll Combustor Performance for Fuel Cell Reformer Applications (연료전지 개질기로 활용을 위한 스위스 롤 연소기의 크기와 연료의 종류에 따른 특성연구)

  • Kim, Youn-Ho;Huh, Hwan-Il;Ronney, Paul D.
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.1
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    • pp.11-18
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    • 2011
  • The geometrically similar swiss roll reactors of different physical sizes were tested with the aim of independently determining the effects of Re and Da. It is found that the difference between catalytic and non-catalytic combustions extinction limits are narrowed as scale decreases. In addition to assess the importance of fuel chemistry, different families of fuels including alkanes and ethers were tested. From these results the effect of scale and fuel type on microscale reactor performance and implications for practical micro combustion devices are discussed.

Effect of Scale and Geometry on the Performance of Heat-Recirculating Swiss roll combustors for Micro Power Generation Applications (마이크로 동력발생용 소형 스위스롤 연소기의 크기와 형상 효과에 대한 연구)

  • Oh, Hwa-Young;Huh, Hwan-Il;Ronney, Paul D.
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.1
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    • pp.1-10
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    • 2011
  • Combustion and extinction limits in heat-recirculating excess enthalpy reactors employing both gas-phase and catalytic reaction have been examined with an emphasis Reynolds number (Re) effects and possible application to microscale combustion devices. In this paper, geometrically similar reactors of different physical sizes and different numbers of turns were tested with the aim of estimating for combustor characteristics. Combustion efficiency is estimated by measuring exhausted gases through the gas chromatograph. From these results the effect of scale and number of turns are demonstrated and optimal operating conditions for Swiss roll combustors are identified.