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combustor相关的网络例句

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与 combustor 相关的网络例句 [注:此内容来源于网络,仅供参考]

The influence of acoustic perturbation on the pressure oscillation of a premixed conical flame combustor is experimentally investigated.

研究表明,V形预混火焰的锋面皱褶的频率与声波扰动的频率相同,其幅值与声波扰动的频率成反比。

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。

In this paper, experimental study (Ma=2.0 of cold flow) on a scramjet combustor model without combustion was carried on direct-connected facility. The effects of inflow parameter, length of isolator and back pressure on combustor and isolator flow field were analyzed and compared. The flow field of combustor was simulated with CFD software and the experimental results were compared.

文中在超燃冲压发动机燃烧室直连式实验设备上,对超音速燃烧室模型进行( Ma =2.0)冷流实验研究,比较了不同的来流条件、不同的隔离段长高比和不同的燃烧室出口反压对燃烧室内部流场以及燃烧室隔离段的抗扰动能力的影响,并利用数值模拟的方法对燃烧室内部流场进行了模拟。

The combination of the compressor, combustor, and high pressure turbine are often called the gas generator.

压缩机的组合, combustor,和高压涡轮经常称气体发电器。

This is impractical for engineering problem. It is necessary to break the shear layer in order to enchance mixing. It is very useful for combustor design with cavity or dual-cavity. In such combustor the fuel jet can break the

要使超声速混合增强,必须打破稳定的剪切层,燃烧室采用凹槽或双凹槽设计是一种行之有效的方法,它产生的燃料射流就能打破剪切层,从而使混合和燃烧效率进一步提高。

2Theory of pulse combustion was analyzed and its mechanism were discussed with planewave transferring theory in the thesis.Models of pulse combustor were reviewed and analyzed.Theone-dimensional unsteady nonlinear model of pulse combustor was simplified with lineal method.The phase relation between pulse pressure and combustion heat discharge which may prompt ordamp pulse combustion process were discussed.

对脉动燃烧理论进行了分析探讨,从平面波的传递理论出发,分析了脉动燃烧的机理;在归纳综合现有的脉动燃烧器理论模型的基础上,采用线性化分析方法,对一维非线性脉动燃烧器理论模型进行了简化,并定性分析了脉动压力与燃烧放热之间的相位关系对脉动燃烧过程的激励和阻尼作用。

Although a dual-mode scramjets configuration is simple and mainly consists of inlet, combustor and wake nozzle, its working process is complicated, especially in the combustor, involving a lot of subjects, including hypersonic aerodynamics, combustion chemistry, etc.

虽然双模态冲压发动机结构简单,主要由进气道、燃烧室和尾喷管三部分组成,但其工作过程却十分复杂,尤以超音速燃烧室的工作规律最为复杂,设计难度最大。

A two stage high pressure turbine on the exhaust end of the combustor drives the compressor.

一个两 阶段高压涡轮在combustor 的尾气末端驾驶压缩机。

Its concluded that, there is a proper combustor exit plane area helpful for reaching maximum thrust; the combustor exit plane area should be increased with the flight Mach number increasing, insuring the exhaust expanding properly.

研究结果表明,不同的飞行马赫数下,存在最佳的燃烧室出口面积使发动机推力达到最大;飞行马赫数增加时燃烧室出口面积应尽量增大,以保证燃气实现完全膨胀从而实现发动机推力最大。

Fluidization and Sounding Pressure Characters Experimental Research on Pulsating Fluidized Bed After verifying experimentally the Rijke type self-exciting pulsating fluidized bed combustion, under different operating conditions (different empty cross-section wind speed and inaction bed height), experimental research the oscillation characters of sounding pressure in the pulsating fluidized bed. The results indicate that the sound characters in the Rijke type self-exciting pulsating fluidized bed combustor are the same with it in the Rijke type combustor, the pressure in the combustor oscillate up and down in the sinusoidal manner and the pressure is the superposition of the multiple harmonic waves.

脉动流化床流化与声学压力特性实验研究在实验验证了Rijke型自激脉动流化燃烧概念后,在不同运行条件(空截面风速、静止床层高度)下,实验研究了Rijke型自激式脉动流化床的声压振动特性,研究结果表明:脉动流化床内建立起的声波特性和Rijke型脉动燃烧器内的一样,各点压力呈正弦规律上下振动,且压力是基波幅值最大的多次谐波的叠加。

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