The metal's high ignition temperature of more than 6,920 degrees Fahrenheit forces exhaust gases out at high velocity to propel rockets upward.
这种金属高达6,920华氏度的燃点，释放高温度的气体推进火箭前进。
In circulating fluidized beds, but with existing problems of high ignition temperature, large content of carbon in the fly ash and relatively low efficiency of combustion.
试验结果发现循环流化床能够有效燃烧无烟煤，但存在着火温度高，飞灰含碳量大，燃烧效率较低等问题。
Through the catalysis of modifier, it successfully solves the problems of low-carbon fuel with poor ignition performance at low temperature and gas lock at high temperature.
通过改性剂的催化作用，成功解决了低碳燃料低温引燃性差、高温时易发生气阻的问题；
Automatic ignition and combustion, fan, high temperature, warming faster size can automatically adjust the flame.
自动点火，风机助燃，升温快，温度高，火焰大小可自动调整。
The shape of rich soot combustion area at high temperature coincides with the share of spray area before ignition.
速燃期内高温富碳燃烧区的形状与着火前一时刻喷雾场的形状相吻合；
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.
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。
High temperature air non-oil ignition is the advanced burning technology with vast prospect.
高温空气无油点火技术是一种先进的燃烧技术，具有广阔的应用前景。
The ignition delay was shortened by increase intake pressure due to higher intake temperature, which resulted in higher smoke, and this phenomenon was more obvious at high EGR rate situation.
提高进气压力由于进气温度的影响使滞燃期缩短，大EGR率尤其明显，导致碳烟峰值随进气压力升高而增大。
After the spark plug ignition, the water molecule can generate much oxygen in the high temperature and high pressure to supply the fuel combustion.
在火花塞点火后，水分子在高温高压下产生大量的氧气，供油分子充分燃烧。
The results show that: the ignition process is influenced both by the electromagnetic filed and the wall with high temperature;
研究表明：煤粉气流在感应式加热无油直接点火器中的着火过程，是交变电磁场与高温壁面加热协同作用的结果。
The results show that: the ignition process is influenced both by the electromagnetic filed and the wall with high temperature;
研究表明：煤粉气流在感应式加热无油直接点火器中的着火过程，是交变电磁场与高温壁面加热协同作用的结果。
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