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- The effect of combustor pressure on soot concentrati on and flame radiation was investigated in a small model gas turbine combustor with an air-blast atomizer. 在一个小型高压燃烧试验台上研究了燃烧室采用空气雾化喷嘴后,燃烧室压力对燃烧室内烟粒浓度和火焰辐射的影响。
- Numerical simulation was used to retrofit a gas turbine combustor with diesel oil and natural gas as fuel in order to burning medium-heating-value syngas efficiently and clearly. 采用数值模拟方法对设计燃料为天然气和柴油的某型号燃气轮机燃烧室进行了改造,使其能够高效洁净地燃烧中热值的合成气。
- In studying the working principles of the gas turbine combustor, theories in gas dynamics, heat transfer, mass transfer and chemical reactions have to be applied. 燃烧室的工作过程远比燃气轮机其它部件复杂,它涉及气体流动、传热、传质以及化学反应等一系列复杂过程。
- Experiments of pulverization and evaporation performance of two kinds evaporating tubes as fuel spray properties for the e turbine combustor have been presented. 摘要为了研究满足燃烧室雾化要求的雾化方式,设计了采用侧喷和逆喷供油方式的两种蒸发管,并对其分别进行了雾化和蒸发率两方面的实验。
- Study on Grid Generation of Gas Turbine Combustor 燃烧室三维贴体网格的生成方法研究
- Numerical Study of Cold Flow Field in Gas Turbine Combustor 燃烧室冷态流场的数值研究
- Application of multi-fluids model to three-dimensions reacting flows in a model gas turbine combustor 多流体模型在燃气轮机燃烧室三维反应流中的应用
- EFFECTS OF INLET TEMPERATURE ON COMBUSTION CHARACTERISTICS WITHIN A MICRO GAS TURBINE COMBUSTOR 进气温度对微燃机燃烧室燃烧特性的影响分析
- EXPERIMENTAL INVESTIGATION ON THE DYNAMIC CHARACTERISTICS OF A GAS TURBINE COMBUSTOR FIRING SYNGAS 燃气轮机合成气燃烧室动态特性的实验研究
- The gas turbine feeds on the fuel it pumps. 燃气轮机以它所抽入的燃料为能源。
- Numerical Calculation of the Three-dimensional Turbulent Flow Field of a Gas Turbine Combustor 三维紊流燃烧室流场的数值计算
- Numerical Simulation Studies on the Discharge Coefficient of Gas Turbine Combustor Liner Air Holes 燃气轮机燃烧室进气孔流量系数的数值模拟
- Numerical Simulation of Three-Dimensional Spray Combustion in a Gas Turbine Combustor 数值模拟环形燃烧室两相反应流场
- Calculational Methods of Main Impact Factors to Exit Temperature of Turbine Combustor 掺混孔参数影响燃烧室出口温度场的计算方法
- EXPERIMENTAL STUDY OF FLAME EXTINCTION CHARACTERISTICS FOR A GAS TURBINE COMBUSTOR BURNING LOW BTU GAS 低热值煤气燃烧稳定性的试验研究
- A disadvantage of the turbine is that it is not reversible. 涡轮机的一个缺点就是它不可以反转。
- EFFECT OF PRESSURE ON SOOT CONCENTRATION AND FLAME RADIATION IN A SMALL MODEL GAS TURBINE COMBUSTOR WITH AN AIR-BLAST ATOMIZER 带空气雾化喷嘴的燃烧室压力对烟粒浓度及火焰辐射的影响
- Full-Scalc Liquid Fuel Ramjet Combustor Tests. 全尺寸液体冲压发动机燃烧室试验。
- Fig. 2 Schematic of the combustor model. 图2微燃烧器数值模型内部结构。
- Then the steam passes into the turbine. 然后蒸气进入汽轮机。