给出了航天电脉冲点火器的参数、设计方案和工作原理。
The parameters, design scheme and operation principle for the aerospace electrical pulse igniter were given.
目前的计算表明，实现点火需要1.2MJ的能量，而NIF可以实现1.8 MJ的脉冲激光能量。
The current calculations show that about 1.2 megaJoules of energy will be enough for ignition, and currently Nif can run as high as 1.8 megaJoules.
电器转速表从点火系统中接受电压脉冲，通常是线圈。
An electrical tachometer receives voltage pulses from the ignition system, usually the coil.
脉冲燃烧器的最佳运行工况应能顺利点火并在低过剩空气系数下高强度稳定燃烧。
The optimum operation of pulse combustor means successful ignition and stable combustion with high intensity, low excess air and low co emission.
建立了微型脉冲推力器点火启动模型，模型中考虑了两相流动和颗粒对推进剂表面的冲击传热。
Ignition start-up model of impulse micro-thruster is established, considering two phase flow and impact heat transfer of particle on the surface of propellant.
通过加速寿命试验促使电火工品老化，利用瞬态脉冲试验，得到电火工品的温升曲线，点火压力的变化及50%发火点。
By means of speeding up the aging of the EIP and transient pulse test, the temperature-rising curve of EIP, the variation of the ignition pressure and 50% ignition point are obtained.
介绍了一种通过点火脉冲和硬件测量汽油机转速的实现方法。
This paper introduces a method to measure the speed gasoline engine by igniting impulse and hardware.
触发器用来产生激励脉冲，供闸流管点火。
The trigger is used for generating excitation pulse for the thyratron to ignite.
针对具有侧向脉冲推力和气动力复合控制的动能拦截弹，需要解决姿控发动机的组合点火问题。
To the kinetic interceptor with lateral impulse thrust and aerodynamic force, it is required to solve the problem of combined fire of motors for attitude control.
为了实现快速短距起爆，火焰射流点火系统被尝试应用在脉冲爆震火箭发动机上。
In order to achieve a rapid initiation of detonation in a short distance, a flame jet ignition system was applied to the pulse detonation rocket engine (PDRE).
地磁传感器测量的数据不仅用于解算弹体飞行姿态，同时可通过计算给出点火脉冲发动机选择的方向基准。
The data measured by magnetic sensor can be used in calculating the flight attitude of the projectile and giving the direction benchmark of firing pulse jet.
分析了系列脉冲激光LSD波点火的积累效应以及LSD波的屏蔽效应。
The accumulation effects of LSDWs ignition and shielding effects of LSD Ws have been analysed.
点火控制算法基于极坐标的形式，该法可充分利用脉冲矢量发动机，且可灵活控制直接力的指向。
Ignition control algorithm is based on the polar coordinates, which can take full advantage of the motors, and regulate the direction of the direct force.
主要采取了提高压缩比、改变点火提前角及采用进气脉冲增压技术。
The major technologies used include increasing compression ratio, changing spark advance Angle and using intake pulse turbo-charging.
选用名厂燃气配件，全自动脉冲式电子点火，大小火力可调节，操作简便。
With the fuel gas parts from the reliable manufacturer, it is controlled by automatically electronic impulse ignition, and the power can be adjusted at your option, easy to operate.
介绍了内燃机点火技术的研究进展，阐述了内燃机脉冲电晕放电点火新技术所涉及的点火能量、点火效率、燃烧时间和相关化学反应等问题。
The ignition energy, efficiency, burning time and main chemical reactions of the pulsed corona discharge ignition(PCD) used on internal combustion engine are discussed in detail.
介绍一种为大电流开关点火的精密长延迟纳秒高压脉冲源的研制。
A high voltage nanosecond pulse generator is developed for firing a large current switch.
在CAI不能工作，而火花助燃hcci能稳定工作的工况，点火脉冲个数和脉冲间隔对燃烧有一定影响。
Under the condition that CAI cannot work but HCCI with spark assistance can stably work, pulses times and pulses intervals can influence combustion.
报道了用脉冲激光引爆并测定粉尘云最小点火能量的方法。
A new experimental set-up has been developed using pulsed-laser to blast various dust clouds with minimum ignition energy determined at once.
通过实验研究了多脉冲火花助燃hcci的燃烧性质，和点火参数对火花助燃hcci燃烧的影响。
Through tests, we investigate the quality of HCCI combustion with multi-pulse spark ignition, and the influence of ignition parameter to HCCI combustion process with spark ignition.
本文研究了发动机点火工作中需要的大电流脉冲恒流源系统的设计与实现。
This paper studied the design and implementation of large pulse constant current source system required by engine ignition.
研究结果对脉冲发动机的点火起控点选择以及脉冲发动机的个数选择都有一定参考价值。
So the research is important to the selection of the fire time and number of the impulse engine and serves as theory reference.
研究了发动机点火工作中需要的大电流脉冲恒流源系统的设计与实现。
The design and implementation of large pulse constant current source system required by engine ignition are studied.
针对两相无阀脉冲爆震发动机（PDE），研究了点火能量、工作频率、发动机直径、进气方式和燃料种类等对PDE点火-起爆性能的影响。
The ignition-detonation performance of two-phase valveless pulse detonation engines(PDEs) with the inner diameters of 50 mm and 120 mm in different operation cases was investigated.
针对两相无阀脉冲爆震发动机（PDE），研究了点火能量、工作频率、发动机直径、进气方式和燃料种类等对PDE点火-起爆性能的影响。
The ignition-detonation performance of two-phase valveless pulse detonation engines(PDEs) with the inner diameters of 50 mm and 120 mm in different operation cases was investigated.
应用推荐