combustor的例句大全

study on aero-engine combustor creep buckling

航空发动机燃烧室蠕变屈曲研究

A gas turbine combustor includes a pilot burner, and a plurality of main burners disposed around the periphery of the pilot burner on the radially outer side.

一种燃气轮机燃烧装置，包括：引燃燃烧器；以及在引燃燃烧器周围的半径方向外侧设置的多个主燃烧器。

Developing Metal Fiber Combustor To Improve Natural Gas Application Technology

开发金属纤维燃烧器&提高天然气应用技术

Heat loss of the combustor is estimated to be below 3%, and the degree of complete combustion is almost perfect.

主燃烧室散热损失

Repairing of Single-Cylinder Combustor of Low calorie value Gas Turbine

低热值燃气轮机单筒燃烧室修复

The results indicate a micro flame tube combustor with a backward facing step is one of the most effective combustors for micro-TPV application.

研究结果表明，带有台阶的微火焰管燃烧室非常适合于微热光电系统的应用。

Effects of fuel chemical properties on exhaust smoke from gas turbine combustor

燃料化学性质对燃烧室排气冒烟的影响

Study of Heat Evolution Characteristics in the Combustor with Plasma-Chemical Auxiliary Device

具有等离子化学辅助装置燃烧室的放热特性研究

Combustion Performance of liquid fuel used in DF chemical laser combustor, energy/ mass ratio and comprehensiVe comparison of liquid fuel with gaseous fuel C_2H_4 are described.

本文叙述了液态燃料作为氟化氘化学激光燃烧室的燃料时的燃烧性能、提供的质量比能量及与气态燃料乙烯的综合比较。

Numerical Study of Compositions Match in Combustor of DF Chemical Laser

DF化学激光器燃烧室中化学配比的数值研究

Experimental Study of Combustor of Combustion-Driven All Gas-Phase Iodine Laser

燃烧驱动全气相化学碘激光燃烧室实验研究

Thermodynamic calculation method of chemical equilibrium and chemical non-equilibrium for water ramjet together with corresponding applicable conditions were introduced. Then the temperature in the ramjet combustor was calculated and compared with experimental data. Thermodynamic calculation method of tailrace tunnel ventilation process in hydropower stations

简述了水冲压发动机化学平衡与非化学平衡热力计算方法及相应的适用条件，计算了试验发动机补燃室温度，并与试验数据进行了对比分析。水电站无压尾水洞引风过程热工计算方法

Numerical Simulation of Flow and Heat Transfer in Pulse Combustor Tail Pipe

脉动燃烧器尾管流动与传热数值模拟

Tail pipe as the important part of pulse combustor is a very good heat transfer device, in which high-temperature high-frequency pulsatile flow lead to heat transfer coefficient enhancement.

尾管作为脉动燃烧器重要的组成部件，能够产生高温高频脉动气流，可成倍提高传热系数，是一种非常理想的换热装置。

the study of one-dimensional flow analysis model of the combustor in supersonic combustion experiments

超燃燃烧室一维流场分析模型的研究

the existent one-dimensional flow analysis models for supersonic combustor were studied.

对公开发表的用于超声速燃烧流场分析的几种一维模型进行了研究，指出了其中存在的问题。

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。

sheet metal-combustor housing, plenums, valve bodies

喷射引擎高压燃烧室，管体，钣金

numerical simulation of three-dimensional nonreacting flows in marine gas turbine combustor

船用燃气轮机燃烧室三维冷态湍流数值模拟

The temperature distribution inside the porous medium combustor and the levels of NO and CO emissions are measured at various working parameters.

在各种工况参数下，对多孔介质内轴向温度分布以及NO、CO和CO2气体等污染物排放的浓度进行了系统测量。