The result indicates that the smart position actuator can be applied to aeroengine distributed control systems.
实验结果表明该智能位置控制器适用于航空发动机分布式控制系统。
Advanced aeroengine alloys such as titanium and nickel-based alloys are widely used for casing and compressor blades.
航空发动机重要零件如机匣、压气机风扇叶片等广泛采用钛、镍基合金等先进结构材料。
Compressor is one of the most important parts in the aeroengine, because the designing work is critical for the performance of engines to a degree.
压气机是航空发动机最为关键的部件之一，其设计好坏在很大程度上决定了整台发动机的性能。
From the perspective of functional analysis, the prediction of the aeroengine exhaust gas temperature could be seen as a functional approximation problem in nature.
从泛函分析的角度出发，将航空发动机排气温度预测问题转换为一种泛函逼近问题。
Therefore, the accurate measurement of the labyrinth gap of aeroengine is very necessary and required in the process of research, improvement, maintenance and manufacturing.
因此，准确测量发动机的篦齿间隙在航空发动机研发、改进、制造以及维护的过程中是十分必要也是必需的。
The turbine blade is one of the key components in aeroengine.
涡轮叶片是航空发动机中的关键部件之一。
The article mainly researched into the blade containment in the aeroengine.
本文主要研究航空发动机机匣对断裂叶片的包容性问题。
Structural reliability analysis of an aeroengine 2nd-stage compressor disk is presented.
对某型发动机压气机第2级轮盘进行了结构可靠性分析。
Low cycle multiaxial fatigue failure is the main failure mode of aeroengine compressor disk.
低循环多轴疲劳失效是航空发动机低压压气机轮盘的主要失效形式。
The development of computer aided testing system for certain aeroengine test-run is discussed.
讨论了某型航空发动机试车计算机辅助试验系统的开发；
In this paper, an RBF neural network approach is applied to aeroengine gas path fault diagnosis.
本文将径向基函数(RBF)神经网络应用到航空发动机故障诊断中。
The optimal control of aeroengine acceleration and deceleration processes is deeply investigated.
深入研究了航空发动机加速过程和减速过程的最优控制问题。
Adaptive inverse control structure for nonlinear systems is applied for aeroengine control systems.
研究了航空发动机的非线性自适应逆控制方案。
On the basis of the method present, the function is achieved and has been used for aeroengine test.
根据本文所论述的方法，实现了该功能并已投入了某型航空发动机试车实验使用。
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。
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。
The rotor system of an aeroengine is taken as an example to verify the effectiveness of the stated method.
并以某航空发动机转子系统为例验证了方法的有效性。
In this paper a new method based on neural networks is proposed for aeroengine adaptive real time modeling.
提出了一种新的基于神经网络的发动机自适应实时模型的建模方法。
The wall thickness of the hollow aeroengine turbine blade is a critical parameter for ensuring its strength.
航空发动机空心涡轮叶片的壁厚是保证叶片强度的一个关键参数。
The domestic manufacturing technology for the external duct fairing of aeroengine is introduced in this paper.
本文介绍了某型飞机发动机外涵道整流罩的国产化研制技术；
Design concept, function and features of the test process management system for aeroengine test were presented.
介绍了航空发动机整机试车试验流程管理系统的设计思想、功能和特点。
The fuel supply regulator was the major execution module of the comprehensive control system for an aeroengine.
供油调节器是航空发动机综合控制系统的主要执行机构。
Dynamic balance accuracy of aeroengine main shaft bearing cage is of the utmost importance to bearing performance.
航空发动机主轴轴承保持架动平衡精度对轴承的性能至关重要。
The fault tree of rotor uncontained top event was established combining the structure characteristics of an aeroengine.
结合某型航空发动机的结构特点，创建了转子非包容顶层事件故障树。
The structural design for serrated shroud of turbine blade was very important for the reliability, life and safety of aeroengine.
涡轮叶片锯齿冠的设计对于保证发动机的可靠性、寿命和安全至关重要。
The structural design for serrated shroud of turbine blade was very important for the reliability, life and safety of aeroengine.
涡轮叶片锯齿冠的设计对于保证发动机的可靠性、寿命和安全至关重要。
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