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航空发动机     
相关语句
  aeroengine
    Fatigue Reliability Analysis of Aeroengine Low Pressure Compressor Disk
    某型航空发动机低压压气机轮盘疲劳可靠性分析
短句来源
    DYNAMIC SIMULATION RESEARCH ON DIGITAL SPEED CONTROL SYSTEM OF AEROENGINE
    航空发动机转速数控系统的动态模拟研究
短句来源
    DYNAMIC FLEXIBILITY COEFFICIENT MATRIX AND ITS MEASUREMENT FOR AEROENGINE SUPPORTING SYSTEM
    航空发动机支承系统的动柔度系数矩阵及其测量
短句来源
    AEROENGINE CONDITION MONITORING AND FAULT DIAGNOSIS SYSTEM
    航空发动机状态监控和故障诊断系统
短句来源
    Application of Brazing and Diffusion Welding Honeycomb Parts in Aeroengine
    钎焊扩散焊蜂窝结构在航空发动机中的应用
短句来源
更多       
  aero-engine
    Research of BIT Technology for Aero-engine Digital Controller and Integrated System of Avionics
    航空发动机数字控制器与航空电子综合系统BIT技术研究
短句来源
    INVESTIGATION OF INTELLIGENT MEASUREMENT SYSTEM FOR AERO-ENGINE EXPERIMENTS
    航空发动机智能测试系统实验研究
短句来源
    GE Talk about Reducing Emissions and Noise of Aero-Engine
    让人类生存环境更清洁、安静、舒适——GE公司谈降低航空发动机的污染与噪声
短句来源
    Application and Development of Blisk on Aero-Engine
    整体叶盘在航空发动机上的应用和发展
短句来源
    Development of Aero-engine Materials
    航空发动机材料的发展
短句来源
更多       
  aircraft engine
    '93 Aircraft Engine Overhaul and Repair Technologies
    ’93航空发动机维修技术
短句来源
    One combustor model was designed based on theory for aircraft engine combustor, the other was on a design for a previously proved micro-engine design.
    两个模型分别是采用了航空发动机大型燃烧室设计理论及公式设计而成的燃烧室模型,和已经在实际中成功应用的国外某型微型涡喷发动机燃烧室模型。
短句来源
    The knowledge management flow and technology system for aircraft engine design are presented, with an emphasis on knowledge acquisition and sharing, implementary method and key technology for knowledge management.
    提出了航空发动机设计知识管理流程与技术体系,重点探讨了发动机设计知识获取与共享、知识管理实施方法及关键技术。
短句来源
    Aiming at the problems that BP algorithm has slow convergence rate and is likely to fall into local minimum point,presents two improved BP algorithm methods:LM(Levenberg-Marquardt)optimization algorithm and SCG(scaled conjugate gradient)algorithm,then the two algorithms were applied to fault diagnosis of aircraft engine rotor and compared with each other in research result,simulation and experiment proved that LM optimization algorithm has higher accuracy,faster convergence rate and better feasibility than the SCG algorithm.
    针对传统BP算法存在的收敛速度慢以及容易陷入局部最小点等问题,给出了两种改进BP算法:LM(Levenberg-Marquardt)优化算法和SCG(Scaled Conjugate Gradient)算法,应用这两种算法对航空发动机转子故障进行诊断研究,比较它们之间的研究结果,仿真和实验表明LM优化算法比SCG算法具有更高的准确度和较快的收敛速度,可行性更强。
短句来源
    Fibre-reinforced Metal Matrix Composites and Application on Aircraft Engine
    纤维增强金属基复合材料及其在航空发动机上的应用
短句来源
更多       
  aero engine
    Fatigue Reliability Analysis of Aeroengine Low Pressure Compressor Disk
    某型航空发动机低压压气机轮盘疲劳可靠性分析
短句来源
    DYNAMIC SIMULATION RESEARCH ON DIGITAL SPEED CONTROL SYSTEM OF AEROENGINE
    航空发动机转速数控系统的动态模拟研究
短句来源
    DYNAMIC FLEXIBILITY COEFFICIENT MATRIX AND ITS MEASUREMENT FOR AEROENGINE SUPPORTING SYSTEM
    航空发动机支承系统的动柔度系数矩阵及其测量
短句来源
    AEROENGINE CONDITION MONITORING AND FAULT DIAGNOSIS SYSTEM
    航空发动机状态监控和故障诊断系统
短句来源
    Application of Brazing and Diffusion Welding Honeycomb Parts in Aeroengine
    钎焊扩散焊蜂窝结构在航空发动机中的应用
短句来源
更多       

 

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  aeroengine
By using this method, the 3-D temperature distribution of the flame tube wall of the combustion chamber of an aeroengine has been simulated successfully.
      
An investigation setup is presented enabling the determination of the substituting drop diameter in fuel aerosol stream created by aeroengine injectors.
      
Modelling and lifing of structural materials for future aeroengine components
      
A non-contact inspection system that can automatically assess the quality of complex engineering components such as turbine blades, has been identified by the aeroengine industry as a requirement in automating the process of proof inspection.
      
The first article inspection of cast turbine blades is on the critical path of a new aeroengine.
      
更多          
  aero-engine
In the manufacture of aero-engine components, auxiliary materials are used which impair mechanical properties if they are not completely removed afterwards.
      
Thermal analysis of a high-pressure compressor rotor of an aero-engine - Venting as a means for life improvement
      
This brief note describes the thermal design of a highpressure compressor rotor of an aero-engine.
      
Two-phase titanium aluminide alloys are being considered as lightweight materials to replace nickel-based superalloys in some high-temperature aero-engine applications.
      
The approach is applied to the simulation of the flow past an installed aero-engine nacelle, at three different free stream conditions.
      
更多          
  aircraft engine
This regime made it possible to model the motion of individual charged clusters of different charge and size in aircraft engine jets.
      
A possible mechanism of formation of electric currents ("engine currents") in aircraft engine jets (with subsequent charging of the aircraft) is investigated.
      
Electric Charging of Soot Particles in Aircraft Engine Exhaust Plumes
      
Electric Diffusion Processes on a High-Temperature Turbine Blade and Its Contribution to the Aircraft Engine Current
      
Wide-band sound-absorbing structures for aircraft engine ducts
      
更多          
  aero engine
Erosion Testing of Coatings for Aero Engine Compressor Components
      
Grid-based distributed simulation of an aero engine
      
Designers and engineers may face these difficulties when designing aero engine systems that need to evolve and change rapidly.
      
Conceptual tribo-energetic analysis of cutting tool protective coating delamination in dry cutting of hard-to-cut aero engine al
      
Aluminum titanate (Al2TiO5) has tremendous application in automobile and aero engine industry due to its excellent thermal property.
      
更多          
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