aeroengine的例句大全

With the increase of aeroengine control variables, the research of aeroengine multi-variable control is very important.

随着航空发动机控制变量的增加, 航空发动机多变量控制的研究已成为十分重要的工作.

The establishment and existing problems of metallurgy model standard for an aeroengine are introduced.

介绍了某型航空发动机冶金型号标准的编制情况及其尚存在的问题.

Abstract: The foundation and simulation of aeroengine starter for flight simulator is discussed in this paper.

文摘: 在飞行模拟训练器的研制中,发动机的起动过程是需要重点研究和模拟的过程之一.

Modeling and gas path fault diagnosis based on model are important research areas in aeroengine.

航空发动机建模以及基于模型的航空发动机气路故障诊断等是航空发动机领域的重要研究方向.

The research work of this thesis belongs to the scope of manufacturing technology of the aeroengine.

论文研究的内容属于航空发动机制造工艺的范畴.

The experimental results indicate that this primary module of an electronic aeroengine controller is viable.

试验结果表明,本文设计的基于DSP和 CAN总线 的航空发动机电子控制器核心模块是可行的.

In this paper, the theory and method of intelligence control are used to aeroengine multivariable control.

本文将智能控制理论和方法引入到航空发动机多变量控制中.

Generally, there are multiple critical features with same structure , stress and temperature in an aeroengine disk.

航空发动机轮盘低循环疲劳危险部位一般是多个,而且具有相同的温度和应力水平.

It is introduced several evaluating methods of high temperature oxidative stability of aeroengine lubricating oil.

介绍了几种评定航空发动机润滑油高温氧化安定性的方法.

This research can accumulate experiences and properties data for manufacturing aeroengine components with EBW.

研究旨在为航空发动机构件的电子束焊接加工制造积累经验和性能数据.

Therefore, the demands of aeroengine designing and manufacturing very strict.

因此航空发动机的设计和制造要求非常高.

Aeroengine has the features of high cost , short life and hard maintenance.

航空发动机成本高,工作条件恶劣, 工作人员难以维护.

This provides an effective way for aeroengine failure detection.

为飞机发动机状态监测问题提供了一种有效的方法.

Plane wrecks caused by aeroengine failure often happen , so people attach importance to aeroengine failure.

发动机故障造成飞机失事的例子时有发生, 倍受人们的重视.

Aeroengine distributed simulation systems based on both serial components level and parallel engines level are developed.

分别开发了基于部件级串行和整机并发的航空发动机分布式仿真系统.

Three kinds of integrator wind-up protection ( IWP) algorithms are proposed for aeroengine digital control system.

提出了航空发动机数控系统三种抗积分器饱和算法。

LQL ( Linear quadratic L_2 bounded uncertainties) control method was applied to the aeroengine control system.

将LQL（Linear quadratic L2bounded uncertainties）控制方法应用于航空发动机控制系统设计。

The augmented LQL method was proposed, then the aeroengine control system was designed by using the method.

并提出了增广LQL控制方法，应用其设计了航空发动机控制系统。

Augmented LQL method and its application to aeroengine control

增广LQL方法及其在航空发动机控制中的应用

A research on cracked failures of fir-tree serration in aeroengine turbine disc

航空发动机涡轮盘榫齿裂纹故障研究