• Title/Summary/Keyword: 급격연소

Search Result 172, Processing Time 0.023 seconds

Influence of Flame Holder on Film Cooling Effectiveness of Ramjet Combustor (화염안정기 형상이 램제트 연소실에서의 슬롯 막냉각 특성에 미치는 영향)

  • Lee, Keon-Woo;Song, J.;Cho, Hyung-Hee;Hwang, Ki-Young
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2008.05a
    • /
    • pp.315-320
    • /
    • 2008
  • This experimental study has been conducted to investigate the effect of the flame holder on the multi-slot film cooling in the ramjet combustor. The turbulent wake which is generated by the flame holder on the entrance of the coolant flow path affects on the slot. Adiabatic film cooling effectiveness on the downstream wall of the slot exit are measured. The results show that the film cooling performance is rapidly decreased after the slot exit by shear layer and high turbulence intensity between separated flows and coolant flows.

  • PDF

The effect of Ca additions on the ignition and combustion behaviors of Mg alloys (Mg 합금의 발화 및 연소특성에 미치는 Ca 첨가의 영향)

  • Chung, D.S.;Cho, H.;Kim, J.K.
    • Journal of the Korean Crystal Growth and Crystal Technology
    • /
    • v.19 no.6
    • /
    • pp.324-327
    • /
    • 2009
  • In the present study, the effect of Ca additions on the ignition and combustion behaviors of Mg alloys has been investigated. Cracks and inclusions were observed at the free surface and interior in as-cast pure magnesium but not in Ca-bearing Mg alloys. There was a tendency that ignition temperature rapidly increased with increasing Ca content in Mg-Ca alloy. Saturated composition for increasing of ignition temperature was related with solid solubility of Ca in Ca-bearing Mg alloys. The protective oxide layers, MgO, could also be found on the combustion surface of Ca-bearing magnesium alloy.

Effect of Igniter's Burning Rate on Negative Differential Pressure of Interior Ballistics (점화제 연소율이 강내탄도의 NDP에 미치는 영향)

  • Sung, Hyung-Gun;Jang, Jin-Sung;Yoo, Seung-Young;Oh, Seok-Hwan;Choi, Dong-Whan;Roh, Tae-Seong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2012.05a
    • /
    • pp.520-526
    • /
    • 2012
  • The appearance of the negative differential pressure(NDP), in which the shot base pressure is higher than the breech pressure, indicates that a potential damage on the gun system is increased. In order to safeguard the gun system, the igniter must be designed to minimize the NDP during the firing process. From this reason, the effect of igniter's burning rate on the NDP of the interior ballistics has been investigated through the numerical simulations. The NDP has been increased with increment of the coefficient in the burning rate of the igniter. A sudden change of the chamber pressure has been shown in case of using a singular coefficient.

  • PDF

Mechanical Properties of Non-cement Matrix Utilizing the Circulating Fluidized Bed Combustion Boiler Fly Ash and Dyeing Sludge Carbide (염색슬러지 탄화물과 순환 유동층 연소 보일러 플라이애시를 활용한 무시멘트 경화체의 역학적 특성)

  • Kim, Tae-Hyun;Lee, Seung-Ho;Lee, Yong;Shin, Jin-Hyun;Lee, Sang-Soo
    • Journal of the Korean Recycled Construction Resources Institute
    • /
    • v.4 no.4
    • /
    • pp.425-430
    • /
    • 2016
  • Both rapid industrial development and society has achieved more comfortable life. But, behind this facts of this industrial development have current pictures that occur global warming and much more by-products by environmental pollution. Therefore, this study used BFS and CFA as by-products to reduce cement usage emitted at a high rate of $CO_2$ gas, to examine sludge recycling strategy more than 200,000ton emitted at local dyeing complex, we suggest basic data research about non-cement matrix properties of utilizing dyeing sludge carbide. As a result, the more dyeing sludge carbide replacement ratio gets higher, the more air content and flow rise. Also, as the dyeing sludge carbide replacement ratio increase more, flexural strength and compressive strength go down.

The Characteristics of DC-shift in Hybrid Rocket (하이브리드 로켓에서의 DC-shift 발생 특성)

  • Kang, Dong-Hoon;Lee, Chang-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.38 no.5
    • /
    • pp.456-466
    • /
    • 2010
  • Typical combustion instability such as DC-Shift found in the hybrid rocket motor is characterized by non-linearity. DC-Shift can occur in two different realizations. One is so-called a positive shift of measured DC voltage where the pressure increase suddenly. The other is a negative shift where the pressure drops abruptly. In the present work, specifically the negative DC-Shift was investigated to analyze the effect of oxidizer flow condition and the resonance between fundamental frequency and other ones, such as Helmholtz frequency, and acoustic frequency. Results show a peak frequency of several hundreds HZ shifts as combustion proceeds. A negative DC-shift was found as the result of phase cancellation between two dominant frequency, combustion frequency and flow related frequency. Still is it required to study further to identify the change of dominance of frequency during the combustion.

Ammonia Combustion Characteristics and Technology Development Trend (암모니아 연소 특성 및 기술개발 동향)

  • Min Jung Lee;Yusung Kim;Chaewoon Ma;Junhee Bae;Chanbin Yeom
    • Journal of the Korean Institute of Gas
    • /
    • v.27 no.3
    • /
    • pp.11-18
    • /
    • 2023
  • This study explained the need for ammonia fuel and the value chain as a hydrogen carrier. The basic concept of ammonia combustion characteristics and the development of flame stability and low NOx combustion technology were introduced. In addition, through the trend of ammonia combustion technology, the characteristics of ammonia combustion technology in the power generation and industrial sectors were examined, and the author's opinions were included. Through this paper, the author intends to give some overview of basic knowledge about ammonia fuel and its future development direction and meaning.

Study of spatial temperature distribution during combustion process in a high temperature and pressure constant volume chamber (고온 고압 정적 연소실에서 연소과정에 따른 온도 분포 측정)

  • Kim, Ki-hyun
    • Journal of the Korea Academia-Industrial cooperation Society
    • /
    • v.18 no.1
    • /
    • pp.345-350
    • /
    • 2017
  • Downsizing is widely applied to diesel engines in order to improve fuel efficiency and reduce exhaust emissions. Engine sizes are becoming smaller but pressure and temperature inside combustion chambers are increasing. Therefore, research for fuel spray under high pressure and temperature conditions is important. A constant volume chamber which simulates high temperature and pressure likely to be found in diesel engines was developed in this study. Pressure and temperature were increased abruptly because of ignition of the pre-mixture in the constant volume chamber. Then pressure and temperature were gradually decreased due to the heat loss through the chamber wall. Fuel spray occurred when temperature and pressure were reached at the target condition. In this experiment, the temperature condition should be exactly defined to understand the relation between fuel evaporation and ambient temperature. A fast response thermocouple was developed and used to measure the temporal and spatial temperature distribution during the combustion process inside the combustion chamber. In the results, the core temperature was slightly higher than the bulk temperature calculated by the gas equation. Ed-note: do you want to say 'ideal gas equation'? This was attributed to the heat transfer loss through the chamber wall. The vertical temperature deviation was higher than the horizontal temperature deviation by 5% which resulted from the buoyancy effect.

Effects of Hexaaluminate Manufacturing on the Synthetic Time of Hydrothermal Synthesis Using Urea (요소를 이용한 수열합성의 합성시간에 따른 Hexaaluminate 제조의 영향)

  • Kim, Seo Young;Park, Ji Yun;Rhee, Young Woo
    • Clean Technology
    • /
    • v.25 no.4
    • /
    • pp.331-335
    • /
    • 2019
  • Interest in environmental pollution is increasing all over the world, and technology development to solve it is actively carried out. In areas where heat is used, especially, combustion is causing countless pollutants in the air environment. Combustion catalyst is a technology that reduces NOx and CO by lowering combustion temperature and enabling complete combustion. Traditional combustion catalysts are expensive and complex in the synthesis process using precious metal catalyst. In this study, hexaaluminate, a high-temperature combustion catalyst, was manufactured using urea, and the properties were investigated according to the synthesis time. The combustion performance and characteristics were evaluated using this catalyst. As the temperature increased, the changing methane conversion rate was shown in two patterns. The conversion rates for 1 hour, 9 hours, and 12 hours were similar, while the conversion rates for 3 hours and 6 hours showed similar patterns. Methane combustion performance increased rapidly as the synthesis time increased from 6 hours to 9 hours, whereas the temperature at T50 was approximately 745 ℃. The performance of the synthesized combustion catalyst for 9 hours was optimum as the NOx emission of this combustion catalyst was not present and the maximum emission of CO was 72 ppm.

A Study on Characteristic of Extinguishment for Solid Propellants Composition by Rapid Depressurization (압력 강하에 따른 추진제 조성별 소화 특성 분석)

  • Choi, Jaesung;Lee, Choonghee;Lim, Jaeil;Lee, Hyoungjin
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.21 no.5
    • /
    • pp.37-45
    • /
    • 2017
  • Extinguishment of a burning solid propellant is difficult, however, dynamic extinction can be induced by fast depressurization in combustion chamber. This paper describes experimental results for the characteristics of extinguishment for composite solid propellants by rapid depressurization. For various composition of solid propellants, depressurization ratio which can induce extinguishment of combustion was obtained using experimental apparatus with rupture disk. Experimental results showed that particle size of oxidizer, mixing ratio of oxidizers with different particle size and contents of metal fuel can affect on the characteristics extinguishement for solid propellant.

Analysis of Cavity Resonances caused by Knocking in Chamber of High Power Engine (고출력 엔진에서 연소실 내의 노킹음에 의한 공진현상 분석)

  • Lee, Du-Gon;Jang, Seok-Hyung;Yi, Chong-Ho;Park, Kyung-Suk;Jun, Kye-Suk
    • The Journal of the Acoustical Society of Korea
    • /
    • v.11 no.4
    • /
    • pp.31-35
    • /
    • 1992
  • Cavity resonances are caused by combustion such as the rapid of pressure rise that occurs from knock in high power gasoline engines. These resonances generally occur at frequencies greater than 5KHz. Analysis of these resonances is important for knock control system design in high power gasoline engines. In this paper, in order to design knock control system for the high power gasoline engine, knock phenomena that occur in chamber were analized theoretically and resonance frequencies of knock signals were predicted. Also, experiments were performed using Soupe x-engine and non-resonance type knock sensor of Bosch co. in Germany. In the result, good agreement was obtained between theoretical prediction and experimental observation.

  • PDF