Design and experiment of ignition motor used for some model airborne missile are explicated in the paper.
文中详细介绍了用于某型号空空导弹固体火箭发动机的点火发动机的设计和试验情况。
According to the analysis of the ignition delay fault,it is obtained that the ignition delay of the ignition rocket motor resulted in that of the ignition motor.
通过对发动机故障试验曲线的分析,得出了点火发动机点火延迟造成主发动机点火延迟的结果,列出了点火发动机点火延迟的故障树,并通过分析及试验对故障树所列因素进行了排查,找到了有可能引起该故障的原因,提出改进措施,改进后的点火发动机能满足使用要求。
Performances of spark ignition engine fueled with DME-LPG blends;
火花点火发动机燃用DME-LPG混合燃料的性能
Combustion characteristics of spark ignition engines with dimethyl ether-LPG blends fuel;
火花点火发动机燃用二甲醚-液化石油气混合燃料时的燃烧特性
A set of electronically controlled throttle system for lean burn spark ignition engine was developed to control NO_x emission using NO_x storage reduction(NSR)catalyst.
为应用吸附还原催化器控制稀燃NO_z排放,建立了一套火花点火发动机的电控节气门系统。
simulated spark-ignition engine
模拟火花点火发动机
compression ignition
(发动机)压缩点火
time for retrofire
制动发动机点火时间
engine wet cycle
无点火的发动机转动
retard thespark,eg of an engine
使点火延迟（如发动机的）.
vehicle engine photoelectric igniter
车辆发动机光电点火器
timing of engine
发动机正时点火调整
generating set, driven by spark-ignition engines, alternating current
火花点燃式发动机驱动交流发电机组
Design and Experiments of Aft-ignition for Small Solid Rocket Motor
小型固体火箭发动机尾部点火设计与实验
Investigation of the Ignition Transient in Large Aspect Ratio Solid Rocket Motors;
大长径比固体火箭发动机点火瞬态过程研究
Study on Problems Related to the Ignition Process of Solid Rocket Motor;
固体火箭发动机点火瞬态相关问题研究
Research on the Improvement and Performance of the Spark Ignition Methanol Engine with Electronic-controlled Injection;
电喷甲醇火花点火式发动机的改进与性能研究
Research of Ignition in Spinning Solid Rocket Motor with Aft-end Ignitor;
某旋转固体火箭发动机尾部点火问题的研究
The Research of Quasi-dimensional Model for Spark-ignited Liquefied Petroleum Gas Engine;
火花点火式液化石油气发动机准维模型研究
The Study on Spark Ignition Engines Fueled with Variable Components of Coal-bed Gas;
火花点火式发动机燃用变组分煤层气研究
Study on Combustion and Emission Characteristics of a Spark Ignition Natural Gas Engine;
火花点火天然气发动机燃烧与排放特性研究
Solid rocket motor igniter integration design and numerical simulation
固体火箭发动机点火系统一体化设计及仿真
Method of amorce mass estimation for solid rocket motor
固体火箭发动机的一种点火药量估算方法