• Either stall or surge may result in combustor blowout.

    不管是喘振或者爆音,都将引起燃烧室的熄火。

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  • This engine consists of an inlet, a combustor, and a nozzle .

    这台发动机由一个进气道,一个燃烧室和一个尾喷管组成。

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  • Totally 4 combustor groups are there at the front and back of boiler.

    锅炉前后各有两组燃烧器,每三个燃烧器为一组,共有4组。

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  • The annular multi-hole radial jets have important effect on combustor liner.

    环向径向射流对燃烧室火焰筒内的流场有着重要的影响。

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  • The vortex is maintained by blades that rotate on the inner casing of the combustor.

    内燃机内盒里的桨叶可以维持这种漩涡式的气流。

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  • The distribution of radiative heat flux to the combustor wall has been obtained by.

    通过计算,获得了燃烧室壁面的辐射热流分布。

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  • The fragmentation influences the char combustion behavior in a fluidized bed combustor.

    利用下行气流振动床代替流化床 ,研究了煤的碎裂特性 。

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  • The combustor is of the vaporiser type, and hence is equipped with three preheat burners.

    燃烧室是汽化器的类型,因此是有三个预热刻录机。

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  • This paper presents a dump combustor which was designed based on research accomplishment.

    文中介绍了一种基于现有研究成果设计的突扩燃烧室。

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  • An annular combustor with evaporation tubes was designed for certain micro-turbojet engine.

    为某微型涡喷发动机设计了一个蒸发管环形燃烧室。

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  • Annular reverse flow zone can be found too in the combustor with the flat-straight slag baffle.

    简单环形挡渣板也能产生环形回流区,在旋风燃烧室设计中可取代锥形缩口挡渣板。

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  • Micro combustor is one of the most important components of micro thermophotovoltaic (MTPV) system.

    微燃烧室是微热光电(MTPV)系统的一个重要组成部分。

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  • The model of combustion efficiency for scramjet combustor is analyzed and presented in this paper.

    本文分析及提出了超音速燃烧冲压发动机燃烧室燃烧效率的数学模型。

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  • The first phase, which focused on the combustor and high-pressure turbine, was completed in September 2009.

    第一阶段致力于燃烧室和高压涡轮的测试已于2009年12月完成。

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  • A quasi one dimensional unsteady numerical analysis of supersonic combustor performance has been conducted.

    完成了超音速燃烧室内非定常准一维流的数值模拟研究。

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  • The combustion characteristics of an improved Rijke tube pulsating combustor burning diesel oil were studied.

    研究了水平安置燃烧柴油的改型瑞克管脉动燃烧器的燃烧特性。

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  • It was found that an increase in the stability of the combustor was obtained simply by gelling the hydrazine.

    发现简单地通过肼胶化的方法可使燃烧室的稳定性提高。

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  • SOFC power generation system with chemical looping combustor is a kind of new solid oxide fuel cell combined cycle.

    化学链式燃烧器和固体氧化物燃料电池相结合的发电系统是一种新型联合循环。

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  • Measurements were also conducted for the time-averaged gas temperature and species concentrations in the combustor.

    同时还测量了该燃烧室内气体平均温度和组分浓度分布。

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  • A power plant pulverized boiler used swirling combustor and happened combustion regulation worse during the operation.

    某电站煤粉锅炉采用旋流燃烧器,在运行中燃烧器出现调节能力差的问题。

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  • The location of the instability zones is dictated by the combustor geometry and the steady-state combustion characteristics.

    不稳定性区域的位置取决于燃烧室几何特性和稳定燃烧特性。

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  • These methods have already been used for the gas temperature measurement at the exit of the high temperature rise combustor.

    分析和比较了两种计算方法,这些方法已应用到燃烧室出口高温燃气温度测量中。

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  • Compared with other natural gas combustor, this combustor can generate the second combustion and form circumfluence of smoke.

    同一般天然气燃烧器相比,这种燃烧器既能产生二段燃烧,又能促进一定量的烟气回流。

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  • The location of the instability zones is dictated by the combustor geometry and the steady - state combustion characteristics.

    不稳定性区域的位置取决于燃烧室几何特性和稳定燃烧特性。

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  • The Ground start ignition, altitude restart ignition and combustion stability are important performance indexes to the combustor.

    地面起动点火和高空起动点火及燃烧稳定性是燃烧室的重要性能指标。

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  • The three-dimensional flow field of annular combustor for aero-derivative gas turbine burning gas fuel was numerically simulated.

    采用数值模拟方法对燃用天然气的某型航改燃气轮机环形燃烧室进行三维流场分析。

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  • The numerical modeling of pulverized coal combustion in an oxygen coal combustor was made by using the continuum trajectory model.

    本文采用颗粒相连续介质-轨道模型对同轴射流渐扩式高炉氧煤燃烧器内煤粉燃烧过程进行了数值模拟。

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  • In this paper, the method and some results of cold experimental investigations of liquid slagging coal-fired combustor are described.

    本文叙述了液态排渣燃煤燃烧室冷态试验的研究方法和某些结果。

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  • Based on a turbofan engine, the afterburner is replaced with pulse detonation combustor to form a turbofan-pulse detonation hybrid engine.

    在涡扇发动机基础上,以脉冲爆震燃烧室代替普通加力燃烧室构成涡扇-脉冲爆震组合发动机。

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  • Based on a turbofan engine, the afterburner is replaced with pulse detonation combustor to form a turbofan-pulse detonation hybrid engine.

    在涡扇发动机基础上,以脉冲爆震燃烧室代替普通加力燃烧室构成涡扇-脉冲爆震组合发动机。

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