查询词典 combustor

The invention relates to a combustor for industrial kilin which comprises air-inlet tube, oil-intake tube and combustion chamber.

本发明涉及一种工业炉窑用燃烧器，有进风管，进油管，燃烧腔。

The whole geometric structures of combustor,combustion chamber and furnace tube in delayed coking furnace were accurately calculated by the whole-coupling method.

采用分区耦合的计算方法，实现了对工业焦化炉从燃烧器、炉膛、炉管整体几何结构的仿真，并且对焦化炉内流动、燃烧和传热全部工艺过程进行了模拟。

The plasma igniter with pilot-hydrogen and high-power plasma igniter are adopted in the direct-connected experiment of supersonic combustor.

采用等离子体点火、凹槽火焰稳定器和从壁面喷射燃料方式，实现了煤油的可靠点火和稳定燃烧。

The preliminary study on the influential factors of scramjet combustor wall pressure was carried out on the direct-connected test facilities under the simulated condition of 25km, 6Ma.

采用试验研究的方法，在模拟飞行高度25km、来流马赫数6的情况下，在直连式试验台上对超燃冲压发动机燃烧室压力影响因素进行了初步研究。

In the paper, the resistance heated and continuous facility is adopted to finish scramjet combustor experiment research on hydrogen-fueled and ethylene-fueled ignition and combustion at different equivalence ratio. The continuous clean airflow of flow ratio 0.73kg/s, total temperature Tt=1000K, Mach number M=2.0, total pressure Pt=0.8MPa is available to the inlet of direct-connected experimental model.

本文采用电阻加热的连续式实验设备，在燃烧室进口气流为高温纯净空气、Ma数M=2、总温Tt=1000K，总压Pt=0.8MPa条件下，进行了不同当量油气比的氢和乙烯燃料的超音速燃烧室直连式实验。

The parameters of pulse combustor such asfrequency,length of feed tube drying tube effecting on drying property were analyzed.It ispropitious to dry high surface-water containing,small granule or liquid materials.

分析了脉动燃烧器频率、热负荷、干燥管长等参数对干燥性能的影响；发现脉动燃烧器尾管内干燥更适合于含表面水高的小颗粒物料或液体物料，可充分利用脉动气流和声波能的作用，使物料分散雾化，增大表面积，提高干燥效率；研究了脉动燃烧器尾管内干燥颗粒物料的传热特性，并将试验结果与其它类型的干燥器进行了比较。

The results demonstrated that supersonic airflows will form a low-frequency oscillation in the combustor after the inlet cover is open, and the attenuation of the oscillation is very slow.

计算结果表明，在进气道整流罩打开以后，超声速气流会在燃烧室通道内形成振幅衰减较慢的低频剧烈振荡。

The engine is provided with a compact annular combustor with airblast atomisers.

它还拥有气动雾化的短环燃烧室。

Some difficulties encountered in burning of these gases in gas turbine combustors are considered and their solutions are proposed through several typical examples of combustor configuration.

本文概述了航机在改烧低热值煤气时会遇到的各种问题及其对策，力图为航机的改型工作提供参考素材。

The spraying system, including core components such as nozzle and nozzle-loop etc., is one of the most important components in aeroengine combustor, each component has immediate impact on the combustors performance.

喷油系统是航空发动机燃烧室的关键组成部分之一，包括喷油环及喷嘴等核心部件，各部件的性能直接关系到燃烧室的性能。

So that more consumers can enjoy more delicious quality, technology is even better than wine.

让更多的消费者可以品尝到品质更为鲜美，工艺更为精湛的葡萄酒。

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