1·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。
2·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。
3·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。
4·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。
5·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；
6·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。
7·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。
8·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。
9·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。
10·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。
1·Aerogine has the features of high rev, heavy air flux and high exhaust temperature, fierceness of noise engenders environment pollution largely during aeroengine test.
由于航空发动机转速高，空气流量大，排气温度高，试车时产生的强烈噪声形成大范围的环境污染；
2·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。
3·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。
4·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。
5·The methods of the shell oilway design, check, assembly application and the design specification of aeroengine Hydraulic System Actuator by using UG were introduced.
介绍了用UG软件进行航空发动机液压系统执行机构壳体油路设计、油路检查、装配应用和设计说明等的方法。