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1·To start the engine, one must first light the small flame beneath the hot ignition tube and crank the engine once using the crank; these preparations take only a minute.

要启动发动机，首先得点燃热管，再转动曲柄轴，发动机便启动，这些准备工作只需一分钟。

2·The technology of ignition and flame spreading is one of key technology of charge design in large caliber guns, which almost chose center core igniter system.

点传火技术是大口径火炮装药中的关键技术之一，现代火炮装药中几乎全部选择了中心点火的结构形式。

3·The effects of temperature and equivalence ratio of supersonic premixed combustible flow on the structure of supersonic combustion flow field, ignition and flame propagation were studied.

研究了超声速预混可燃气流的温度以及当量比对超声速燃烧流场结构、点火与火焰传播特性的影响。

4·This paper explained the design of nozzles, injectors and burner cones of new ignition with producer gas on forced pre-mixing and the method of flame stability.

根据发生炉煤气的特性，采用强制预混燃烧方式，设计了点火器的喷嘴、引射器及烧嘴，并对稳定火焰的方法也进行了研究。

5·These flow characteristics can be favorable to ignition, flame stabilization and combustion intensification.

这些特征都有利于点火，火焰稳定及强化燃烧。

6·Piezoelectric ceramic electron flame, ignition convenient, saves time and manpower.

压电陶瓷电子打火，点火方便，省时省力。

7·Experiments show that a new-type pulverized coal burner with a slit bluff-body designed on the said principle is suitable for the ignition and flame stability of low volatile pulverized coal.

实验证明，根据这一原则设计的开缝纯体燃烧器对低挥发分煤粉的着火与火焰稳定具有较好的适应性。

8·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.

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。

9·Temperature in fuel spray field has a determinant influence on fuel evaporating, mixture formation, ignition and flame spreading and is very important for numerical simulating.

喷雾场的温度对燃油的蒸发，混合气的形成，着火以及火焰传播有着决定性影响。

10·Match with the ignite electrode, detect electrode and gas solenoid valve to realize the burner auto. ignition and flame-out protection.

配合点火探测电极和燃气电磁阀用来完成烧嘴的自动点火和熄火保护。