As the fuel burns, gases expand to fill the combustion chamber at a high pressure.

At first the volatile a coal particle when the particle comes into a combustion chamber.

当煤粉颗粒进入高温的燃烧室时,首先受热析出挥发份,所以,挥发份的析出方式直接影响颗粒的运动和弥散.

Ionic current signal was detected in progress of combustionconstant volume combustion chamber on this system.

利用火花塞离子电流法建立了相应的离子电流检测系统.

Can adapt to any type of combustion chamber.

能适应任何类型的燃烧室.

Nevertheless , particle size distribute does not change with the combustion chamber pressure and propellant powder percentage.

粒子尺寸分布不随燃烧室压强和推进剂铝粉含量变化.

The hot decomposition gases from the combustion chamber are cooled in the recuperator.

在燃烧室分解后的热气体在换热器中被冷却.

This inhibiting of flow oscillations adds stability to the combustion chamber.

对流动振荡的这种抑制作用提高了燃烧室的稳定性.

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

控油环间隙位于燃烧室凹口的左30度.

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.