对燃室用英语怎么说，对燃室的英文翻译

词语导航

基本信息

词语：对燃室

繁体：對燃室

拼音：duì rán shì

英语翻译

【机】 antechamber

分词翻译

对的英语翻译：

right; answer; reply; at; check; compare; couple; mutual; opposite; versus; vs
face to face
【计】 P
【化】 dyad
【医】 Adv.; contra-; corps; ob-; p-; pair; par; para-
【经】 vs

燃的英语翻译：

burn; ignite; light
【医】 ignition; inflame

室的英语翻译：

chamber; loculus; room; thalamus; ventricle
【医】 camera; camerae; cell; chamber; room; thalamo-; ventricle; ventriculo-
ventriculus

翻译例句

1. 研究表明，补燃室压强的变化对燃烧效率的影响是有限的，喷管损失主要与喷管结构尺寸有关；

The results show that the effect of combustion efficiency on chamber pressure is limited, nozzle loss is mainly caused by its structure and size.

2. 测试结果表明：工业锅炉中，炉内燃烧室与燃烬室之间的折烟墙的形状对炉内燃料燃烧有较大影响。

It indicates that the fold smoke wall"s shape of firebox and reburning chamber may influence the burn efficiency in the industrial boiler.

3. 在高空模拟实验器上，利用已有的航空发动机预燃室点火器，研究了燃油预热增温对高空低压点火性能的影响。

The effect of advanced fuel temperature on the high altitude ignition performance in the prechamber taken from an existent aero-engine at simulated high altitude facility was studied.

4. 采用遗传算法对某试验超燃冲压模型发动机的燃烧室构型参数进行了优化设计，所得方案的性能大大优于实际方案。

Scramjet combustor design optimization for a test scramjet model engine is conducted by employing genetic algorithms, and an optimal design much better than original design is obtained.

5. 考虑了进气道尺寸、进气夹角、头部距离、一次喷嘴扩张比和喷嘴数目等结构因素对补燃室掺混与燃烧性能的影响。

The effect of inlet size, inlet Angle, dome height, primary nozzle expansion ratio and nozzle Numbers on combustion efficiency were taken into account.

6. 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。

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

7. 在此基础上，对预燃室喷嘴直径进行了优化试验研究。

Experimental studies on the diameter of spray nozzle of the pre-chamber have been optimized.

8. 对选作高速柴油机预燃室喷咀材料的八种耐热钢及高温合金的燃气热疲劳性能进行了试验研究。

The thermal fatigue resistance high temperature combustion gases of eight heat resistant steels and superalloys in fatigue properties were studied on test rigs heated by combustion flue gas.

9. 为了分析发动机设计参数对反应流场的影响，用不同的条件进行计算，并由此分析了补燃室几何结构和液体燃料初始颗粒直径对燃烧效率的影响。

Calculations were carried out under different chamber configurations and initial droplet diameters, from which the effects of these conditions on the combustion efficiency were analyzed.

10. 本文从实验和数值模拟两方面，对静止和旋转增程固体火箭发动机补燃室燃烧流场进行了研究。

The combustion flow field in secondary combustion chamber for static and spinning extended solid rocket ramjet were studied experimentally and numerically in detail.

11. 采用CFD软件FLUENT对多火孔无焰陶瓷燃烧器的顶燃式热风炉燃烧室的燃烧情况进行了数值模拟。

The numerical Simulation which applying CFD software FLUENT to the hot blast shaftless stove with Multi-burner-port Annular Flameless Ceramic burner is introduced in this paper.

12. 气液同轴直流离心式喷嘴对补燃发动机燃烧室高频燃烧稳定性有显著影响。

The bipropellant gas-liquid coaxial orifice-swirl injector has great effects on the high-frequency combustion instability of the LOX/kerosene staged combustion cycled engine.

13. 论述了速燃及新型燃烧室对发动机运行经济性及排放性能的影响，并对新型燃烧室的实验结果进行对比分析，指出了新型燃烧室的特点。

The effects on the operation economical efficiency of the engine and the discharge capability of the new quick burning firebox were discussed in this paper.WWw.wEnTIyI.com

14. 论述了速燃及新型燃烧室对发动机运行经济性及排放性能的影响，并对新型燃烧室的实验结果进行对比分析，指出了新型燃烧室的特点。

The effects on the operation economical efficiency of the engine and the discharge capability of the new quick burning firebox were discussed in this paper.