A New Model Reference Adaptive Control for Aeroengine 新的参考模型自适应控制方法在航空发动机中的应用
Manufacturability evaluation method for aeroengine blade 面向航空发动机叶片的可制造性评价方法
In this paper, Auto Regressive model of metal content for specially monitored metals in lubricating oil monitoring system of aeroengine is built by the method of Time Series Analysis. 利用神经网络方法对某型航空发动机滑油监控系统中需重点监控的金属元素含量建立了网络,并根据该模型对其含量变化趋势进行了预测分析。
The fuel supply regulator was the major execution module of the comprehensive control system for an aeroengine. 供油调节器是航空发动机综合控制系统的主要执行机构。
Application of Image Superelement Technology for Strength Analysis of Aeroengine Stator Blade 影像超单元技术在航空发动机静子叶片强度分析中的应用
Demonstration test and flight test have proven the blades made of DD402 alloy in the small aeroengine working properly. 通过考核试车和试飞证明,用该合金制造的小型航空发动机涡轮工作叶片工作正常。
Application of Microcomputer in Aeroengine Combustor Test 微机在航空发动机燃烧室试验中的应用
Aeroengine online optimization methods are studied in this article. 研究了航空发动机在线优化算法问题。
It is introduced several evaluating methods of high temperature oxidative stability of aeroengine lubricating oil. 介绍了几种评定航空发动机润滑油高温氧化安定性的方法。
Method of Fault Diagnosis and Fault-Tolerant Control for Actuator Loop in Aeroengine Digital Control System 航空发动机数控系统执行机构回路故障诊断和容错控制方法
Research on Web-based Aeroengine Maintenance Decision System 基于Web的航空发动机维修决策系统研究
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。
A dynamic strain gage is developed for dynamic stress test at900 ℃ of turbine rotor blades of an aeroengine. 为了对某型航空发动机涡轮转子叶片在900℃温下进行动应力测试,研制了900℃态应变计。
A Certain Type of Aeroengine Control System Simulation Based on dSPACE 某型航空发动机控制系统dSPACE仿真
Numerical Calculation of Infrared Characteristics for Aeroengine Exhaust System 航空发动机排气系统红外辐射特征数值计算研究
All experiments have showed that the design meets the requirements of distributed aeroengine control system. 实验表明设计的通信方案可以满足航空发动机分布式控制系统要求。
A general simulation framework for aeroengine performance is constructed by the use of object-oriented technique and layered design method. 根据航空发动机性能仿真的需要,采用面向对象技术和分层设计思想,构造了航空发动机性能的通用仿真系统框架。
Advanced aeroengine alloys such as titanium and nickel-based alloys are widely used for casing and compressor blades. 航空发动机重要零件如机匣、压气机风扇叶片等广泛采用钛、镍基合金等先进结构材料。
Simulation of Pressure and Flux of Oil Supply System for an Aeroengine 某型航空发动机滑油供油系统压力和流量仿真
Aeroengine airstart assisted by the starter was presented to enlarge the turbofan airstart envelop based on the analysis of domestic development and application of correlation investigation. 在分析国外相关研究工作发展和应用情况的基础上,提出了以起动机辅助航空发动机空中起动来扩大涡扇发动机空中起动包线的措施;
Application of CBR and Neural Network for Steady-State Model of Aeroengine 案例推理和神经网络在航空发动机稳态模型中的应用
Design concept, function and features of the test process management system for aeroengine test were presented. 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 of Aeroengine Life Monitor System Based on Flight Data 基于飞行数据的航空发动机寿命监视系统设计
Summarize of Investigation and Method for Blade Fatigue Fracture of Aeroengine 航空发动机叶片疲劳断裂研究领域与方法概述
Temperature limit equipment detector for aeroengine was used to detect the performance of temperature limit equipment for aeroengine. 航空发动机限温装置检测仪用来检测发动机限温装置的性能。
In the aeroengine measurement field, the development of varied laser diagnostics was briefly introduced. 简要介绍了多种激光诊断技术在航空发动机测试领域的发展现状。
Development of Information Fusion Methods for Aeroengine Fault Diagnosis 航空发动机故障诊断信息融合方法研究现状
The fault tree of rotor uncontained top event was established combining the structure characteristics of an aeroengine. 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。
This research can accumulate experiences and properties data for manufacturing aeroengine components with EBW. 研究旨在为航空发动机构件的电子束焊接加工制造积累经验和性能数据。
Abstract: The foundation and simulation of aeroengine starter for flight simulator is discussed in this paper. 文摘:在飞行模拟训练器的研制中,发动机的起动过程是需要重点研究和模拟的过程之一。