A temperature distortion generator burning hydrogen in front of engine inlet produces thermal disturbance.
热扰动是由安装在发动机进口前的氢燃烧温度畸变发生器产生的。
Finally the standard equipment and method of data processing are proposed to facilitate comparing the data of engine inlet port tests.
建议规定一种标准的试验设备和数据处理方法，以利于发动机气道试验数据的对比。
Finally, the effect of the helicopter engine inlet and outlet was analyzed using a simplified engine model and the rotor-fuselage-engine interactions were obtained.
最后运用简单的发动机模型分析了发动机进出口对直升机流场的影响。
The flow field of the core engine inlet was numerically calculated to solve the problem that the air flow measured in the air simulated test facility was inconsistent with ground test.
针对某型核心机地面台和高空台试验中空气流量测量不一致的问题，开展了核心机进口流场的数值计算分析和试验研究。
Injecting fuel directly into the engine (rather than into the inlet manifold, upstream of the inlet valves) also has beneficial effects.
燃油直喷到引擎(而不是到进气总管、进气阀门的上边)也有有益效果。
The outlet hose ran to the engine manifold, and the inlet hose ran to the dashboard, where it was attached to a small dial.
出口软管接连发动机歧管，内口软管接入仪器板，并连接至一个小盘表。
Inlet temperature distortion is one of the key factors effecting engine stability.
发动机进口温度畸变是影响发动机稳定性的关键因素之一。
Temperature distortion on inlet flow of engine is more important than pressure distortion for engine stability.
进口流场的温度畸变对军用飞机发动机稳定性具有比压力畸变更大的影响。
Engine pressure ratio (EPR), the ratio of inlet pressure over exhaust-let pressure measurements. The ratio is used as the primary parameter to set thrust on some engines.
发动机压力比(epr)，进气压力与排气压力值的比，某些发动机以此作为设定推力的主要依据。
This engine consists of an inlet, a combustor, and a nozzle .
这台发动机由一个进气道，一个燃烧室和一个尾喷管组成。
The dramatic side swoop that doubles as a much-needed engine cooling air inlet.
引人注目的侧边波浪线，同时还是必不可少的引擎冷却进气口。
INLET GUIDE VANES, a fixed set of blades in front of an engine compressor for directing airflow to the compressor.
进口导向叶片，发动机压气机前的一组固定叶片，用以引导气流进人压气机。
As against an inlet manifold engine of the same power, the turbo engine requires a smaller installation space and as such has a better power-weight ratio.
与相同功率的进气歧管发动机的相比，涡轮增压发动机需要相对较小的安装空间，同时也具有较好的功率重量比。
The engine-feed system interface is at the turbopump inlet flanges .
发动机与供应系统的交界是在涡轮泵的进口法兰盘处。
This paper introduces the parameter estimation research for the turbine inlet temperature and compressor exit pressure by using the engine variables measured under the different flight conditions.
本文研究利用不同飞行状态下测量的发动机变量估计涡轮进口温度和压气机出口压力。
No. 1 main generator engine fresh water cooling outlet to turbine inlet damaged, to be renewed.
从1号发电机淡水冷却出口到涡轮机进口这一段淡水冷却管损坏，需换新。
Project Background: the inlet and outlet valve seats of auto engine are main components of various auto engines and internal auto manufacturers import the product mostly.
项目建设背景：汽车发动机进排气阀座是各种汽车发动机的主要部件，目前该产品国内汽车生产厂家大部分从国外进口。
The dynamic distortion data of a engine compressor inlet flow are studied with inlet shield.
对某型发动机压气机进口档板动态畸变流场数据进行了研究。
With the elevation of inlet working temperature of gas turbine engine, thermal barrier coatings (TBCs)are receiving a great deal of attention.
前言：随着燃气涡轮发动机进口工作温度的提高，热障涂层技术受到了广泛的关注。
This design is the main engine will take the step motor actuators provide an idle by-pass inlet channel.
本设计主要是将汽油机的带步进电机的怠速执行器提供一个旁通的进气通道。
Vacuum operated actuators open valves to select a longer, 680mm, inlet tract at low revs, increasing the rate of both the airflow and the engine torque.
真空操作打开阀门致动器来选择较长，680毫米，进道在低转速，提高利率的同时气流和发动机扭矩。
The produce gas of biomass contents 1.0-10.0% tar, which will be condensed on boilers, pipelines of transportation and the inlet devices of diesel engine in the process of utilization.
生物质气化气中含有1.0-10.0%的焦油，在使用过程中它们凝结在锅炉，传输管道，和内燃机的入口装置上。
While the effect of engine speed on the required inlet air temperature for autoignition is different for different octane Numbers.
而发动机转速对自燃所需进气温度的影响则随所用燃料辛烷值的大小而异。
Some fundamental problems in designing the tangential inlet passage are involved when the turbulent combustion system for model CA6102 gasoline engine is researched and developed.
研究开发CA6102型汽油机紊流燃烧系统时，涉及到一些切向进气道设计中的基本问题。
The engine-feed system interface is at the turbopump inlet flanges.
发动机与供应系统的交界是在涡轮泵的进口法兰盘处。
With the increase of the turbine inlet temperature of high performance aero-engine day by day, the turbine coating blade coating technology has been widely used.
随着高性能航空发动机涡轮进口温度日益提高，涂层技术在涡轮叶片上得以广泛应用。
This paper introduced the fast detection device of acting length of the sealing face which is suitable for on line detection of inlet and exhaust valve of the engine.
本文介绍了密封面作用长度的快速检测装置，此装置适用于发动机中进排气门的在线检测。
The expansion engine which has a inlet valve without exhaust valve, is a short piston engine.
膨胀机为进气有阀、排气无阀的短活塞型。
Working medium inlet and exhaust non-return valves balance hole for Stirling engine is introduced.
对热气机工质进排气单向阀平衡孔作了简介。
Working medium inlet and exhaust non-return valves balance hole for Stirling engine is introduced.
对热气机工质进排气单向阀平衡孔作了简介。
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