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。
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。
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。
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。
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。
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 three-dimensional simulation model of the spiral inlet duct of a diesel engine is created with the FIRE software, and CFD simulation of inlet flow is carried out.
利用FIRE软件建立了某柴油机螺旋进气道的三维仿真模型，对进气流动进行了CFD模拟计算。
A new technique for improving the performance of the tumble inlet ports of multi-valve SI engine was proposed.
旨在探究一种能够提高多气门汽油机滚流进气道进气性能的新技术。
In order to find out the effects of inlet system dimensions on the gas exchange quality of gasoline engines, a FDM code was used to simulate the gas exchange process of a 3 - cylinder gasoline engine.
为研究进气系统结构参数对汽油机换气过程的影响，用有限差分法编制的程序对某3缸汽油机的换气过程进行模拟计算。
Applying CFD to simulate the fluid field of a inlet port in a kind of 385 diesel engine, and with 3d analog computing as well, we analyze these results and prove its effectuality.
本文利用CFD技术对某型号385柴油机的进气道流场进行了三维模拟计算，并对结果进行了分析，验证了其有效性。
Valve rotator is an important device to ensure the normal operation of the inlet and exhaust valves of a medium speed diesel engine.
旋阀机构是保证中速柴油机进、气阀正常工作的重要装置。
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。
A brief view and results of tests for the effects of the inlet total pressure distortion on the performance and the stability of a two-spool turbojet engine are presented.
介绍进气总压畸变对双轴涡喷发动机性能和稳定性影响的试验及其结果。
The engine tool still further comprises an air inlet (38) for introducing external air provided at a front part of the engine tool.
另外，发动机工具在其前方具有用于吸入外部气体的吸入口（38）。
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。
Driven by the thermoacoustic engine, a single stage double-inlet PTC obtained the lowest refrigeration temperature of 80.9K with operating frequency of 45Hz.
该热声发动机驱动双向进气型单级脉管制冷机达到80.9K的最低制冷温度。
Driven by the thermoacoustic engine, a single stage double-inlet PTC obtained the lowest refrigeration temperature of 80.9K with operating frequency of 45Hz.
该热声发动机驱动双向进气型单级脉管制冷机达到80.9K的最低制冷温度。
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