Oil control ring gap to be located 30 degrees to the left of combustion chamber recess.

Fuel gushes into the combustion chamber.

燃料喷进燃烧室.

You can accomplish this by forcing more air into the combustion chamber.

你可以通过把更多空气强制压入燃烧室来实现.

Using a ball end mill to form part of the combustion chamber.

用球头铣刀的组成部分燃烧室.

It is shown that the engine with spherical combustion chamber is beneficial to its output.

简要分析了改善发动机性能的措施.结果表明,采用球形燃烧室有益于提高输出功率.

Usually a gas cooler is used between the combustion chamber and hydrator.

通常在燃烧室和水合器之间设置一个气体冷却器.

When the beetle needs protection, the chemicals flood the combustion chamber.

当甲虫需要保护, 化学药物充斥燃烧膛.

A combustion chamber and its igniters, injectors, and other related apparatus in jet engine or turbine.

覆盖在往复式发电机引擎的汽缸内腔的封闭一端的可分离的盘状物体.

It can provide a powerful tool for the engineering analysis ofgeometry optimization for the combustion chamber.

数值试验的结果表明,本文所建立的数值分析平台对燃烧室的设计优化提供了一个实用的工具.

Given sufficient turbulence in the combustion chamber, detonation is unlikely to occur.

假定在燃烧室中形成充分的湍流, 就不可能产生爆燃.

Excess heat the combustion chamber also a problem, often leaking to other components the engine.

另外,燃烧室排出的过量热气经常泄漏到发动机的其他零件中,这也是一个问题.

All these works done were hoped to be available for the combustor configuration design.

为燃烧室结构设计与设计参数选择提供了参考.

The experimental results of the axial velocity and the tangential velocity in combustor have been given.

给出了燃烧室内的轴向速度和切向速度的试验结果.

These results can provide some reference for maintain and design for gas turbine combustor.

本文研究结果可为发动机火焰筒的维修和改进设计提供参考.

Flame-out protection device: Wher the combustor quenches by accident , combustion proportional value will be closed automatically.

熄火保护功能: 燃烧器以外熄火时, 燃气比例阀自动关闭.

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.

Micro combustor is one of the most important components in a micro-thermo-photovoltaic MTP system.

最大化提高微燃烧室的燃烧效率对于微热光电系统是非常关键的.

Computations are done on flow configurations that resemble the reaction zone in the scramjet combustor flows.

本文通过数值模拟得到了超燃冲压发动机燃烧室化学反应流流场的流动结构.

Fig. 2 Schematic of the combustor model.

图2微燃烧器数值模型内部结构.

Scramjet nozzle was installed at the exit of the combustor.

尾喷管直接安装在模型发动机的燃烧室出口.

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.