首页|Study on Radiant Heat Transfer Characteristics of Gas in a Once Through Combustor

Study on Radiant Heat Transfer Characteristics of Gas in a Once Through Combustor

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As one of the core components of aero-engine,the thermal protection scheme of combustion chamber has an important impact on its service life.In order to improve the design level of high-performance combustion chamber,the radiation heat transfer characteristics of combustion chamber are studied by experimental method.The following results are obtained:1)With the increase of oil-gas ratio,the gas temperature increases first and then tends to be stable,the radiant heat flow increases gradually,the convective heat flow increases gradually and then tends to be stable,and the proportion of radiant heat flow remains basically unchanged;2)With the increase of the inlet temperature,the gas temperature increases gradually,the radiant heat flow,especially in the flame barrel head area,increases significantly,the convective heat flow remains basically unchanged,and the proportion of radiant heat flow increases significantly;3)With the increase of the combustion chamber pressure,the gas temperature increases gradually.When the combustion chamber pressure is low,the radiant heat flow increases sharply with the increase of the pressure;When the combustion chamber pressure is high,the radiant heat flow increases slowly with the increase of the pressure.The convective heat flow gradually decreases and tends to be stable,and the proportion of radiant heat flow gradually increases and tends to be stable.This study is of great significance to improve the calculation accuracy of radiant heat flow of combustion chamber and the reliability design of thermal protection scheme of combustion chamber.

Combustion ChamberRadiant Heat TransferRadiant Heat FlowOil-gas Ratio

Yan-ce Bi、Yu-ang Liu、Wei-hua Yang、Zhi-gang Sun

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College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics

国家科技重大专项

2017-Ⅲ-0003-0027

2024

风机技术
沈阳豉风机研究所(有限公司)

风机技术

影响因子:0.643
ISSN:1006-8155
年,卷(期):2024.66(1)
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