固体火箭发动机的点火是一个十分复杂的物理化学过程，包括三个阶段：点火延迟、火焰传播和燃烧室气体充填。
The ignition of the solid rocket motor (SRM) is a very complex physical and chemistry process, which is composed of three component phases: ignition delay, flame spreading and chamber filling.
在二冲程发动机中你必须混和燃料和气体，因为气缸壁上的孔阻止使用活塞环密封燃烧室。
You have to mix oil into the gas in a two-stroke engine because the holes in the cylinder wall prevent the use of rings to seal the combustion chamber.
应用理想气体状态方程，对柴油机活塞燃烧室容积的检测方法进行了研究。
Based on ideal gas equation, the measurement method of diesel engine piston combustion chamber volume was researched.
相邻的另一端的混合物75燃烧室60气体点火器点燃了圣火20日至77生产。
Adjacent the opposite end of the combustion chamber 60 the gas mixture 75 is ignited by the ignitor 20 to produce flame 77.
这些气体的形式迅速扩大，并通过燃烧室，并通过喷嘴（打击）提供前进推力出后用尽。
The gases which form expand rapidly, and are exhausted through the rear of the combustion chambers and out through the nozzle (blow) providing the forward thrust.
提供一种方法和设备，用于对进入内燃机燃烧室的气体燃料进行精确计量。
A method and apparatus are provided for accurately metering a gaseous into a combustion chamber of an internal combustion engine.
防止了煤孔堵塞，为燃烧室提供了大量的可燃气体，促进了煤充分燃烧。
The clogging of a briquet hole is prevented; a plurality of combustible gas is provided for the combustion chamber, promoting the sufficient combustion of the briquet.
建立了一种适合于循环流化床燃烧室(CFBC)条件下可燃气体的燃烧计算方法。
A method suitable for calculating the burning rate of combustible gas in CFBC has been created.
此外，本文还着重研究了燃烧室形状对缸内气体流动及喷雾的影响。
In addition, the effects of the combustion chamber shape on flow and spray process were discussed.
这样一种气体燃烧室的优点除其它优点 外还具有较大的动力功率范围，改进的火焰前缘和低的生产成本。
The advantages of such a gas bunner am amongst others a large dynamic power range, an improvadflame front and a low production cost.
氢发动机10将氢气、氧气和作为工作气体的氩气供给到燃烧室21以使氢气燃烧。
A hydrogen engine 10 supplies hydrogen, oxygen, and an argon gas serving as a working to a combustion chamber 21 to combust the hydrogen.
氢发动机10将氢气、氧气和作为工作气体的氩气供给到燃烧室21以使氢气燃烧。
A hydrogen engine 10 supplies hydrogen, oxygen, and an argon gas serving as a working to a combustion chamber 21 to combust the hydrogen.
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