• Title/Summary/Keyword: 열재순환

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다공성 물질에 의한 열재순환 화염에 관한 실험적 연구 I

  • 유영돈;민대기;신현동
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.12 no.5
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    • pp.1113-1120
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    • 1988
  • This paper presents the results of an experimental investigation on one dimensional excess enthalpy flame formed in a porous block. The investigation is undertaken in order to further the physical understanding of internal heat recirculation from reaction zone to unburned mixture. Two porous blocks are placed at both sides of combustion block to control the temperature distribution in the combustion block by means of radiation heat transfer. Mean temperature measurement reveals the general nature of the reaction zone in the porous material. It is conformed that the temperature of reaction zone exceeds the adiabatic flame temperature and the flame is stabilized at the out range of flammibility limit derived by conventional burner.

Combustion Characteristics in a Heat-recirculating Microemitter for a Micro Thermophotovoltaic System (초소형 열광전변환 장치용 열재순환 초소형 이미터 내 연소특성에 관한 연구)

  • Lee, Kyoung-Ho;Kwon, Oh-Chae
    • Proceedings of the KSME Conference
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    • 2007.05b
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    • pp.2360-2365
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    • 2007
  • A new microemitter (microcombustor) configuration for a micro thermophotovoltaic system in which thermal energy is directly converted into electrical energy through thermal radiation was investigated experimentally and computationally. The microemitter as a thermal heat source was designed for a few watt power-generating micro thermophotovoltaic system. In order to satisfy the primary requirements for designing the microemitter, i.e., stable burning in the small confinement and maximum heat transfer through the emitting walls but uniform distribution of temperature along the walls, the present microemitter is cylindrical with an annular-type shield for heat recirculation to apply for the excessive enthalpy concept. Results show that the heat recirculation substantially improves the performance of the microemitter: the observed and predicted thermal radiation from the microemitter walls indicated that heat generated in the microemitter is uniformly emitted.

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A Numerical Study on the Combustion Phenmena in Porous Media( I ) (다공질 내부의 연소현상에 대한 수치적 연구( I ))

  • Lee, Yong-Il;Sin, Hyeon-Dong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.20 no.1
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    • pp.328-335
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    • 1996
  • The one-dimensional flame analysis was carried out to understand the combustion phenomena in porous media. The downstream as well as upstream solution corresponding to upper and lower solutions could be obtained. While upper flame temperature gets higher, lower flame temperature gets lower, as the flame approaches the central part of the combustor. The reason why upstream flame and downstream flame exist at the same flow condition is that the regions where net heat recirculation is identical exist in upstream and downstream of the combustor. In order for the downstream flame to be stabilized, more heats needed to be recirculated towards upstream because of larger radiation loss of downstream flame.

Determination of Ignition Squence and Estimation of Injector Life Extension Technique in Liquid Rocket Engine (소형 액체 로켓 엔진에서의 점화 시퀀스 결정 및 인젝터 수명 연장 기법 평가)

  • Park, Jeong;Kim, Yong-Wook;Kim, Young-Han; Moon, Il-Yoon;Lee, Jae-Yong;Kang, Sun-Il;Chung, Yong-Gahp;Cho, Nam-Kyung;Oh, Seung-Hyup
    • Journal of the Korean Society of Combustion
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    • v.5 no.1
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    • pp.43-53
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    • 2000
  • Experimental studies on determination of the supply leading time of propellants to combustion chamber have been made to stably and efficiently guarantee the ignition process with liquid rocket engine. The propellant used is a Jet A-1 as fuel and a liquid oxygen as oxidizer. Unlike impinging FOOF type of injectors are arranged radially and the designed O/F ratio is 2.34. The present experiment program also includes the stability on the quadlet type of ignitor using the triethylalumimum as an ignition source and injector life tests. Experimental results clarifies that the propellant supply through LOx leading to combustion chamber is proper for stable ignition and combustion processes based on the fuel and oxidizer manifold pressures, combustion chamber pressure, and the variation of flame length from the nozzle exit with lapse time, and shows that the leading supply time of propellants affects the engine performance little. The effect of positioning cooling holes is remarkable to protect the injector face.

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