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。
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。
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 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。
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；
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。
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 near deadbeat control design was applied to an aeroengine speed simulation system for flight handling simulation.
本文研究了飞行训练用航空发动机转速模拟系统拟最少拍控制设计。
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 blade is one of the important parts of aeroengine. Efficiency and precision are important for the blades' machining.
叶片是航空发动机的重要零件之一，叶片的加工精度和效率对于叶片的加工来说至关重要。
The transient thermal analysis of the main thrust ball bearing was performed during fuel cut off for an aeroengine oil system.
对在航空发动机滑油系统断油时的主推力球轴承瞬态热进行了分析。
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。
Through summarizing the laws and characteristics of aeroengine research and development, the existing major problems are analyzed.
通过阐述航空发动机科研试制的规律和特点，分析了目前航空发动机试制存在的主要问题。
The operation stability is described for an aeroengine during weapon launch, and effects on the aeroengine operation are analyzed.
论述了在武器发射时，某型发动机的工作稳定性；分析了对发动机工作的影响。
Summarizing the whole work, Expectation the using of neural-network modeling and intelligent digital filtering technology on the aeroengine.
总结全文，展望神经网络建模和智能数字滤波技术在航空发动机领域的重要性及其应用。
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。
As a very important component of aeroengines, low pressure turbine affects the mass, the specific fuel consumption, the efficiency of aeroengine greatly.
作为航空发动机非常重要的组成部分，低压涡轮+对整个发动机质量、耗油率和效率都有很大的影响。
The development of engineering database for aeroengine test has improved the efficiency of aeroengine test and ensured veracity and security of aeroengine test.
某型发动机试车数据库的开发提高了发动机的试车效率，保证了试车数据的安全性和一致性。
The development of engineering database for aeroengine test has improved the efficiency of aeroengine test and ensured veracity and security of aeroengine test.
某型发动机试车数据库的开发提高了发动机的试车效率，保证了试车数据的安全性和一致性。
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