1) some turbofan engine
某涡扇发动机
1.
The fuel adjustment of some turbofan engines fuel-pump adjustor is continuous change following the engine s inlet temperature.
某涡扇发动机主燃油泵调节器的燃油调节具有随发动机进口总温变化而不断修正的特性,在实验室采用常规PID控制方式不能满足发动机进口总温大范围变化时的控制要求,为此,兼顾神经网络的自适应性,提出了一种基于RBF网络的参数自整定PID控制器。
2) turbofan engine
涡扇发动机
1.
A decentralized multivariable PI controller for turbofan engine;
涡扇发动机分路式多变量PI解耦控制
2.
Design of a new turbofan engine preservation equipment;
新型涡扇发动机油封设备的研制
3.
Numerical simulation of the start-up process of augmented turbofan engines;
某型涡扇发动机起动过程数值模拟
4) turbofan
[英]['tə:bəufæn] [美]['tɝbo,fæn]
涡扇发动机
1.
Key turbomachinery technology of civil high-bypass-ratio turbofan engine;
民用大涵道比涡扇发动机叶轮机某些关键技术
2.
The key technologies and future trend for several novel turbofan engines are described.
总结了多电发动机、智能发动机、双外涵变循环发动机、复合材料发动机、外骨架发动机、绿色发动机等未来涡扇发动机的研究进展、关键技术和发展趋势。
3.
To simulate the starting characteristics of turbofan engine in different atmospheric environments, particularly in plateau regions and at high or low temperature, a generalized description of engine starting mathematical model based on state space is given.
针对不同大气条件尤其是高原和高、低温条件,及不同起动机和负载扭矩特性下涡扇发动机起动过程的数值模拟问题,给出了通用起动模型状态空间描述形式,研究了基于支持向量机的起动模型辨识和起动性能仿真方法。
5) turbojet/turbofan engine
涡喷/涡扇发动机
1.
A computer program is developed to analyze the effects of circumferential inlet total-pressure distortion on the stability and performance parameters of turbojet/turbofan engines.
开发了一种用于计算进气总压周向畸变对涡喷/涡扇发动机气动稳定性和主要性能参数影响的软件。
6) Turbofan engine
涡轮风扇发动机
1.
In this paper,the current status of stealthy technology and infrared stealthy technology are presented,the features of turbofan engines and their superiority in the infrared stealthy of aircrafts are described in detail and the application prospect of the turbofan engines on stealthy aircrafts is analyzed.
本文简要介绍了隐身技术、红外隐身技术的现状,详细阐述了涡轮风扇发动机的特点和在红外隐身方面的优势,分析了涡扇发动机在隐身飞机上的应用前景。
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条