aero-engine
美 
英
例句
Two numerical examples and a practical example of an aero engine disk were presented herein to validate stochastic response surface method.
两个数值例子和一个发动机轮盘实例来验证这一方法的有效性。
The concept of regulation and control for the aero engine service life is developed to improve its reliability.
从提高发动机使用可靠性角度，研究了某型发动机使用寿命调控方案。
An intelligent PMA for flaw detection of aero engine is presented, which can be used for data analysis and decision.
针对发动机探伤数据分析、判断手段落后等问题，研制了一种智能PMA。
The computation methods and code referred could be applied to estimating the infrared radiation of practical aero engine exhaust system.
所开发的计算方法与程序可用于排气系统红外辐射特性的数值计算与分析，基本满足工程设计的需要。
Through the analysis of a system identification example of X aero-engine EEC (engine electronic controller) , the result shows this.
经对某航空发动机电子综合调节器燃油通道动态过程参数模型辨识的实例，验证了该算法精确快速。
Three threshold-lines evaluation was used to analyze direct reading ferrograph data of lubricating oil from aero-engine.
利用线阈法分析某型航空发动机润滑油样的直读铁谱数据，提出油液直读铁谱分析诊断标准。
Full Authority Digital Electronic Control and advanced control strategy are the dominant directions in the current aero-engine control.
全权限数字电子控制以及先进控制策略是当今航空发动机控制的主流方向。
A new neural network algorithm with fuzzy logic compensation was proposed and applied to an aero- engine rotating speed control system.
提出了一种带模糊补偿的神经网络辨识器，并应用在某型涡扇发动机转速控制系统中。
Health assessment of aero-engine is an important technical measure for ensuring engine safe working and prolonging engine operating life.
航空发动机健康状况评估是保证发动机安全工作、延长发动机使用寿命的一种重要技术措施。
The contra-rotating turbine disks of an aero-engine were simplified as a counter-rotating plan disk system.
将反向旋转的高低压涡轮盘简化成了几何形状相对简单的反转盘系统。
The dynamic characteristics of three types of aero engine have been analyzed with this program and the results are satisfactory.
目前该程序已实际应用于三种型号的发动机上，获得了满意效果。
Fuel pump and lube pump used in present aero-engine and space-engine are oriented to smaller volume, bigger flux and higher pressure.
目前，航空航天发动机控制系统中的燃油供油泵、滑油增压泵都在向着小体积、高转速、大流量、高压力的方向发展。
The method was applied to diagnosis the aero engine wear fault. Example shows the validity of the method proposed.
将该方法用于某型航空发动机的磨损故障诊断专家系统中，实验证明了该方法的有效性。
GTE persists in seeking for an advanced position in aero-engine design, test and instrumentation technologies.
中国燃气涡轮研究院以追求航空发动机设计、试验、测试技术研究能力和水平在行业内领先为理念；
Honeycomb segment was an important sealing structure of the aero engine.
蜂窝篦齿是航空发动机中的重要封严结构。
Moreover, the acquired fault symptom was applied to fuzzy cluster analysis to obtain aero engine fault sources.
在此基础上，应用模糊聚类分析方法，依据最大隶属度原则得到发动机早期故障源。
In this case, it is a key technique to determine the operating life of aero engine main bearing.
在这种情况下，如何科学地确定主轴轴承寿命就是个难度很大的技术问题。
The system has been actually tested on our aero-engine test bed and appraised by the Aero -Industry Ministry.
本系统在发动机试车台上进行了试验，并通过了航空工业部部级鉴定。
Critical technologies for aero engine prognostics and health management systems development were summarized.
总结归纳了航空发动机预测健康管理系统设计的关键技术。
Finally, a case of aero-engine blade and blisk, the algorithm solving process was presented.
最后，以航空发动机某型叶片与轮毂为例，给出了算法求解过程。
The safety lives of parts in an aero engine are determined by use of the confidence limits of three parameter Weibull distribution.
用三参数威布尔分布的置信限，确定某发动机零件的安全寿命。
To realize the Aero- engine digital control simulation, it is necessary to create a real - time Aero- engine model.
建立航空发动机实时数学模型对于实现航空发动机数字控制是必不可少的。
The vibration test and failure diagnostics are important safeguarding measures during aero-engine tests and component tests.
振动测试与故障诊断是航空发动机整机和部件试验中的一项重要安全保障工作。
The turbine disk is a key component of the aero engine and its work condition is severe.
涡轮盘是航空发动机关键件，其工作载荷复杂。
Simulation results show that the given mathematic model for aero engine starting system is feasible.
最后以典型发动机起动系统作为仿真实例验证了此方法的可行性。
Based on collaborative working platform, full lifecycle management for aero-engine developing projects can be provided.
基于协同工作平台提供对航空发动机研制项目的全生命周期管理。
The model provides theoretical way for the research of the thermoacoustic oscillation in the aero-engine afterburner.
该模型的建立为预测航空发动机加力燃烧室振荡燃烧特性及控制规律提供了一种理论探索途径。
The operation performance of an aero engine fuel nozzle was tested and investigated.
本文对某型航空发动机燃油喷嘴的工作特性和雾化质量进行了试验研究。
Results Aero engine linear model within flight envelope designed point and active fault-tolerant controller.
结果得到在飞行包线设计点发动机线性模型和主动容错控制器。
The flow-thermal coupling calculation of aero engine air system includes fluid network and thermal network.
发动机空气系统可分别建立流体网络与热网络进行耦合计算。
V-shaped flame holder has been widely applied in aero-engine afterburner since the third generation aero-engine.
传统发动机加力燃烧室都采用V型火焰稳定器组织燃烧，自加力出现到第三代发动机，该方案一直得到了广泛应用。
Pretreatment and Time-domain analysis were studied to the vibration signal of aero-engine in this paper.
本文研究了发动机振动信号的预处理和对信号的时域、幅域分析。
It provided the sustain to deal with the vibration signal of Aero-engine.
为发动机振动信号的处理提供了理论依据。
This approach is applied to aero-engine control under transient conditions. As a result, the process is perfect.
将这种方法应用于某型航空发动机的过渡态控制中，得到了理想的控制结果。
Idea of Aero-engine Development by "Core-engines in Series and Derivation"
“系列核心机及派生发展”的航空发动机发展思路
The author believes that adopting appropriate control strategy based on neural network in aero-engine control has obvious advantage.
作者认为，对于航空发动机这种严重非线性被控对象，选择合适的神经网络控制方案有着明显的优势。
A new general approach for aero-engine and other complex mechanical system performance monitoring was put forward.
本文的研究为航空发动机及其它复杂机械系统的性能监控提出了一种新的普适性方法。
Because of its unique features, aero engine power generation can provide quality and clean distributed power.
航改燃机发电因其独有的特点，可以提供优质、清洁的新型分布式电能。
The CAT system can fulfill the technologic demands for aero engine test-run entirely.
系统工作稳定可靠，操作简单，维护方便，能够完全满足发动机的试车技术要求。
Believed the earth sphere said, thought may reach East's India and China from the European Xi'an Aero-Engine.
相信大地球形说，认为从欧洲西航可达东方的印度和中国。
