随着航空发动机技术的发展,对滚珠轴承的速度特性要求也越来越高。
With the development of aeromotor technology, more strict speed performance of ball bearing is required.
主要用于活塞式航空发动机。
涡轮叶片是航空发动机中的关键部件之一。
The turbine blade is one of the key components in aeroengine.
航空汽油用于活塞式航空发动机,使用量较少。
Aviation benzine is used at piston aviation engine, use quantity is less.
研究航空发动机的非线性动态模型的建立问题。
Modeling of nonlinearity dynamic respondence of the aero engine was studied.
在这个基础上,介绍了一种航空发动机数字转速表设计。
Based on this method, a digital tachometer design for aero engine was introduced.
讨论了某型航空发动机试车计算机辅助试验系统的开发;
The development of computer aided testing system for certain aeroengine test-run is discussed.
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, the theory and method of intelligence control are used to aeroengine multivariable control.
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。
Dynamic balance accuracy of aeroengine main shaft bearing cage is of the utmost importance to bearing performance.
空气螺旋桨是把航空发动机的动力转化为飞行器推进力的工具。
Air propeller is the tool which transforms the power of aerial engine to the thrust of aircraft.
下面你会发现信息的V -双和径向航空发动机,我设计和建造。
Below you'll find information about the V-twin and radial air engines that I designed and constructed.
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 wall thickness of the hollow aeroengine turbine blade is a critical parameter for ensuring its strength.
本文阐述一个可用于航空发动机数据检测和控制的光纤传输系统。
This paper deals with a optical fiber transmisson system being used for detecting and control of aeroengines.
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。
Low cycle multiaxial fatigue failure is the main failure mode of aeroengine compressor disk.
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。
The establishment and existing problems of metallurgy model standard for an aeroengine are introduced.
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 near deadbeat control design was applied to an aeroengine speed simulation system for flight handling simulation.
叶片内部通道冷却技术在航空发动机叶片的设计中占有重要的位置。
The cooling technique of the blade inner passage plays a significant role in the design of blades for gas turbine.
最后提供了传感器在航空发动机和压缩机动态压力测试中的测试结果。
And the results of the dynamic pressure measurement on aircraft engines and air compressors are given.
最后给出传感器标定结果,并讨论了在航空发动机燃油测量中的应用。
Finally, the application of the sensor is discussed in measuring fuel flow of an aeronautical engine.
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 fault tree of rotor uncontained top event was established combining the structure characteristics of an aeroengine.
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。
In this paper, an RBF neural network approach is applied to aeroengine gas path fault diagnosis.
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。
Design concept, function and features of the test process management system for aeroengine test were presented.
将相对关联距离熵应用于航空发动机转子—机匣系统状态识别和故障诊断。
The relative correlation distance entropy is applied to fault diagnosis and state recognition of aero engine rotor-case system.
可移动插板式压力畸变发生器是现代航空发动机稳定性评定试验中的一项关键设备。
Movable bailie pressure distortion generator is an important device in aero-engine stability assessment tests.
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。
Summarizing the whole work, Expectation the using of neural-network modeling and intelligent digital filtering technology on the aeroengine.
为模拟航空发动机主轴轴系所有重要轴承联合试验,研制了航空发动机轴系轴承试验机。
To simulate combined testing for all of the important bearings on aviation engine main shaft, a shafting bearing tester is designed.
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 blade is one of the important parts of aeroengine. Efficiency and precision are important for the blades' machining.
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。
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。
Through summarizing the laws and characteristics of aeroengine research and development, the existing major problems are analyzed.
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