BAE is less dependent on big "platform" sales than it used to be and now sees itself as a provider of "through-life support" for complex systems, much like the aero-engine industry.
BAE已不再像过去那样依赖大的“平台”销售，它现在更将自己看作是复杂系统的“终身支持”提供商，这很像航空引擎业。
The experimental results are valuable reference for aero-engine turbine blade cooling designers.
本文的实验结果对于航空发动机涡轮叶片冷却结构设计具有参考价值。
Movable bailie pressure distortion generator is an important device in aero-engine stability assessment tests.
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。
Blisk is a new integrated structure of blades and disk actually used in the aero-engine of high thrust-weight ratio.
整体叶盘是高推比航空发动机采用的新结构。
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 mechanism and impact of aero-engine bearing's skidding damage are analyzed.
分析了航空燃气涡轮发动机主轴承产生滑蹭损伤的机理与危害。
Rotor dynamic design is one of the most important aspects of aero-engine design.
对于航空发动机的设计，转子动力学设计是一个重要的环节。
In this paper, a new method of pipe system design based on an aero-engine DMU is introduced.
本文介绍了基于数字样机的全新管路系统设计。
The principle and method of preventing siphon in aero-engine lubrication system are described.
介绍了航空发动机滑油系统防虹吸原理及方法；
Finally, two time series and aero-engine spectrometric oil analysis data were used to verify this model.
最后，利用两组实际的航空发动机油样光谱分析数据对模型进行了验证。
The research of reliable communication is always the key point on aero-engine distributed control system.
通讯的可靠性研究一直是航空发动机分布式控制系统研究的关键问题。
Using time sequence method, the starting process of some aero-engine is controlled by starting control box.
某型发动机的起动过程采用时序控制方式，由起动程序机构来实行控制。
Based on the basic equation of an certain type of aero-engine, a linear mathematic model is established in this paper.
基于某型航空发动机的基本方程，建立了其线性数学模型。
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 results of research offer evidences for MR isolator being applied to improve the vibration condition of aero-engine.
研究结果为利用金属橡胶隔振器来改善航空发动机的振动状况提供了依据。
Develop the general version management ante-type system which faces to the design process of aero-engine blade products.
开发面向设计过程的航空发动机叶片广义版本管理原型系统。
In this paper, the optimal PID control system for aero-engine was designed using LQR (Linear-Quadratic Regulator) approach.
本文采用基于LQR的PID控制算法，设计某型号涡扇发动机控制系统。
A new neural network adaptive control scheme is presented and its applications to aero-engine control system are researched.
本文研究神经网络自适应控制方法及其在航空发动机控制中应用。
The aero-engine combustion outlet temperature makes a strong impact on the life of engine and the power of the engine output.
航空发动机燃烧室出口温度的高低及出口温度场的均匀程度，直接影响到发动机的工作寿命和输出功率的大小。
Pressure probe automatic calibration and data process system was built for high precision pressure measurements on aero-engine.
压力受感器自动校准及数据处理系统是为航空发动机精确压力测试而建立的。
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 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。
Turbine starter is a very important composing part for aero-engine, its work capability directly affects the reliability of aero-engine in start.
涡轮起动机是航空发动机的重要组成部分，其工作性能直接影响发动机的起动可靠性。
The 6th stage blade in aero-engine compressor is taken as an example, the temperature effect on the blade vibration frequency blade is investigated.
以某型航空发动机压气机第六级叶片为例，研究了温度对叶片振动频率的影响。
Then, based on the plenty analysis of the fundamental aero-engine maintenance task, the breakdown structure of the aero-engine maintenance cost is put forward.
在分析民用航空发动机基本维修工作的基础上提出了发动机维修成本的组成结构。
With the increase of the turbine inlet temperature of high performance aero-engine day by day, the turbine coating blade coating technology has been widely used.
随着高性能航空发动机涡轮进口温度日益提高，涂层技术在涡轮叶片上得以广泛应用。
In view of the existing problem of general fuzzy control, by introducing the improved fuzzy control, it has met the performance need of the aero-engine basically.
基于基本模糊控制存在的问题，通过引入改进的模糊控制方法，基本满足了航空发动机控制系统的性能要求。
To satisfy the need of blade geometry inspection and deviation analysis of aero-engine, a non-rigid registration algorithm based on deformation function is proposed.
为满足航空发动机精铸涡轮叶片壁厚偏差分析需要，提出了一种基于变形函数的精铸涡轮叶片检测模型非刚体配准算法。
This paper describes the calculation methods of finite element strength for spokes frame casing, which is used in aero-engine by the actions of various complex loads.
本文阐述在航空发动机上使用的轮辐框架式承力机匣，在受各种复杂载荷作用下的有限元强度计算方法。
This paper describes the calculation methods of finite element strength for spokes frame casing, which is used in aero-engine by the actions of various complex loads.
本文阐述在航空发动机上使用的轮辐框架式承力机匣，在受各种复杂载荷作用下的有限元强度计算方法。
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