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1·Combustion gas flows in the space.

燃烧气体在该空间中流动。

2·Electricity is normally generated by turbines driven by combustion gas, steam or an expanding gas.

电一般是由燃气、汽或某种膨胀气体驱动透平机而产生的。

3·In addition, there are limits of the high combustion gas mixture is suitable for lean burn performance.

另外，还有混合气发火界限高，适于稀燃的性能。

4·Fuel-efficient: fuel system cleaner, oil products increased atomization, incomplete combustion gas mixture, to maximize power.

省油：燃油系统清洁，油品的雾化程度提高，混合气完全燃烧，功率达到最大化。

5·The utility model provides a double-sealed special valve for combustion gas, belonging to a special valve for the combustion gas.

本实用新型提供的双密封燃气专用阀属于一种燃气专用阀。

6·Furthermore the internal combustion engine is provided with an ignition device which extends into the combustion chamber for igniting the combustion gas.

并且还具有伸入到该燃烧室中的点火装置，用于点燃燃气。

7·Valve bodies are engines of ventilators, ventilation process: on time and turn off the control valve to ensure full combustion gas mixed with gas and emissions.

配气机构是发动机的换气机构，换气过程：控制气门按时关了，保证气配时充分燃烧混合气和排撂废气。

8·The method for setting up the radiant coefficient is put forward to solve the infrared radiation temperature measurement problem for motor combustion gas flow field.

提出了解决发动机燃气流场红外辐射测温时辐射系数设置的方法。

9·The combustion gas flow was analyzed, the velocity and temperature distributions were calculated according to this model, the results fitted well with the actual flame.

在此基础上进行了喷枪内外燃气流场分析，结果表明，燃气温度分布、速度分布与实际焰流有较好的一致性。

10·Aim A new scheme of vertical launching system was presented to solve the problems of combustion gas exhaust and protection, guarding against unexpected firing and so on.

目的为解决战术导弹自力垂直发射中的燃气排导、防护及防意外点火等问题，提出了一种自力垂直发射系统的新方案；