To avoid the affection of micro-combustion due to reducing engine's scale, high-pressure gas was used to drive engine.
为了避免由于发动机尺寸的减小而带来的微燃烧问题，采用高压气体作为动力源；
The characteristic length about micro-combustion system is small, and its flow, heat transfer and combustion has many different characteristic that large size of the combustion systems has.
微型燃烧系统的特征长度很小，其流动、传热和燃烧具有的特性，与大尺寸的燃烧系统有许多不同。
Based on the extensively study of micro scale combustion difficulties, the research trends of some typical micro engines are emphatically introduced.
本文在全面分析微尺度条件燃烧所面临的各种困难的基础上，重点介绍了几种典型的微型发动机的研究概况。
The nozzle spray characteristics of micro-turbine engines affect the stabilization of flame of the combustion chamber, the distribution of temperature, and the efficiency of combustion.
针对微型燃气涡轮发动机喷嘴的雾化对燃烧室火焰稳定性、温度分布和燃烧效率的影响。
In order to improve the combustion property in the micro combustor, the problems in the micro combustor are analyzed and the relevant measures are put forward.
为了改善微型燃烧器内的燃烧性能，分析了微型燃烧器燃烧时存在的主要问题，并提出了相应的燃烧策略。
Despite of great differences in their structures and work theory, they all have a micro-firebox and need a good combustion system to ensure a high energy density.
这两种微动力机电系统在结构和工作原理上有较大差异，但是都具有微型燃烧室，都需要一个良好的燃烧系统保证高能量输出。
The combustion model of micro-void propellant is presented in this paper. The control equations for stable burning of propellant are set up.
建立了一个描述微孔推进剂燃烧的模型，并得到了推进剂稳定燃烧时的控制方程组。
The micro-turbine generator characteristics of the combustion chamber are introduced in this paper.
介绍了微型涡轮发电机燃烧室的特点。
The catalytic activities and ageing resistant performance of above catalysts for methane combustion was evaluated in a continuous-flow micro-reactor.
利用连续流动微型反应装置研究了催化剂的反应性能，抗老化性能及反应条件对反应性能的影响。
The combustion wave temperature profiles and flame structures of fuel-rich propellant containing boron are measured by using W-Re micro-thermal couple and flame photo technique.
通过微热电偶测温和火焰单幅照相技术测试了含硼富燃料推进剂燃烧波温度分布及燃烧火焰结构；
The combustion wave temperature profiles and flame structures of fuel-rich propellant containing boron are measured by using W-Re micro-thermal couple and flame photo technique.
通过微热电偶测温和火焰单幅照相技术测试了含硼富燃料推进剂燃烧波温度分布及燃烧火焰结构；
应用推荐