在内夹层的上部设有旋流导向叶片及填料过滤层。
In the upper portion of the sandwich with hydrocyclone guide blade and packing filter layer.
介绍了某型航空发动机可调导向叶片测量的一般原则和内容。
This paper introduces the general principle and the content of the measurement of the adjustable leading vane of aero_engine.
主要用作加力燃烧室、导向叶片、涡轮叶片、涡轮盘、喷嘴等。
It can be used adding force combustion chamber, guide vane, turbo vane, turbo table and nozzle etc.
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。
INLET GUIDE VANES, a fixed set of blades in front of an engine compressor for directing airflow to the compressor.
适用于旋转件和静止件，在恶劣环境中工作的部件，如燃烧室，涡轮叶片，导向叶片等。
It is applicable to rotating and stationary components that work in the harsh environment, such as the combustion chamber, turbine blades, turbine guide vanes, etc.
为降低涡轮机的燃油消耗率，在民用动力装置的涡轮中广泛地采用了可旋导向叶片的结构。
The variable angle guide vanes have been widely used for decreasing specific fuel consumption of the civil turbines.
研究表明该冷却方式在导向叶片上的应用是可行的，但该冷却方法的工程化仍有大量的工作要做。
The results show that it is possible to use effusion cooling on turbine guide vane, but there still remain a lot of work to do for it is really used on an engine.
航空发动机涡轮叶片，包括导向叶片和工作叶片，是将燃气的热能转换为旋转的机械动能的重要的热端部件。
Turbine blade including guide blade and work blade is one of the crucial heated end components of gas turbine engine to convert heat energy of burning gas to revolving mechanism kinetic energy.
经过旋流导向叶片脱油后的空气，继续向上经过填料过滤层，将空气中的油份及其它杂质再一次的进行分离和过滤。
After turning vane rotary flow off the air after oil, continue to up after packing, will the air filter layer of oil and other impurities again for the separation and filtering.
航空发动机、燃机等精铸真空无余量空心涡轮、导向叶片及复杂结构件。多种热处理炉上用料盘，夹具等耐热合金钢精铸件。
The no machining directional solidification hollow turbine blades, hollow guide vans and complex structure parts used in aero engine and gas turbine made by vacuum precision investment casting.
导向器类零件分体式精铸的关键技术之一是切分得到蜡模模具设计的内、外环及叶片单元体即如何实现分割面的生成。
One of the key-technologies of guiding device investment casting is getting internal ring, external ring and blade unit by splitting integral guiding device part for wax-mold design.
在内部流场气-热耦合数值模拟的基础上，研究了某涡轮导向器叶片烧蚀故障的原因。
The cause of turbine stator blades was analyzed on the base of numerical simulation by means of air-thermal coupling for heat transfer and temperature distribution.
在内部流场气-热耦合数值模拟的基础上，研究了某涡轮导向器叶片烧蚀故障的原因。
The cause of turbine stator blades was analyzed on the base of numerical simulation by means of air-thermal coupling for heat transfer and temperature distribution.
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