1、Signal Acquisition and Processing of CAT System for Aeroengine Test Run
航空發(fā)動機CAT系統(tǒng)信號采集與處理

2、The development of computer aided testing system for certain aeroengine test-run is discussed.
討論了某型航空發(fā)動機試車計算機輔助試驗系統(tǒng)的開發(fā)；

3、Fault Detection of Microprcessor System in Aeroengine FADEC
發(fā)動機FADEC中微處理系統(tǒng)故障檢測

4、Application of Support Vector Machine in Fault Diagnosis of Aeroengine Test
支持向量機的渦扇發(fā)動機試車故障診斷

5、Ceramic Coating of Aeroengine Turbine Blade
陶瓷涂層在航空發(fā)動機渦輪葉片表面處理中的應用

6、A new method measuring aeroengine T_4 temperature
一種測量航空發(fā)動機T_4溫度的新方法

7、Application of ISCAR Tool in Aeroengine Manufacturing
ISCAR刀具在航空發(fā)動機制造中的應用

8、Low cycle multiaxial fatigue failure is the main failure mode of aeroengine compressor disk.
低循環(huán)多軸疲勞失效是航空發(fā)動機低壓壓氣機輪盤的主要失效形式。

9、Machining Technologies for T Slots of Aeroengine Casings
航空發(fā)動機機匣T型槽加工技術

10、Fault Detection of Measuring Channel in Aeroengine FADEC System
航空發(fā)動機量測系統(tǒng)的故障檢測

11、APPLICATION OF LOW BTU GASES TO AEROENGINE MODIFIED FOR INDUSTRIAL USE
關于低熱值煤氣在航機改型中的應用問題

12、The optimal control of aeroengine acceleration and deceleration processes is deeply investigated.
深入研究了航空發(fā)動機加速過程和減速過程的最優(yōu)控制問題。

13、High Energy X - Ray Instrumentation System for Aeroengine Test
航空發(fā)動機高能X射線測試系統(tǒng)

14、Aeroengine adaptive control based on adaline network
基于Adaline網(wǎng)的航空發(fā)動機自適應控制

15、An Identification Model of Aeroengine Starting Process Based on RBF Network
基于RBF網(wǎng)絡的發(fā)動機起動過程的模型辨識

16、Design of codec for FIR used in the telemetry of aeroengine rotor
航空發(fā)動機轉(zhuǎn)子參數(shù)遙測中的FIR編解碼器設計

17、Condition Monitoring of Aeroengine Based on Wavelet Process Neural Networks
基于小波過程神經(jīng)網(wǎng)絡的飛機發(fā)動機狀態(tài)監(jiān)視

18、System of Scheme Design of Aeroengine Rotor Coupling Based on BP Network
基于BP網(wǎng)絡的航空發(fā)動機轉(zhuǎn)子連接件方案設計系統(tǒng)

19、Structural Reliability Analysis of an Aeroengine Compressor Disk
某型發(fā)動機壓氣機輪盤結(jié)構(gòu)可靠性分析

20、Fuzzy Decision for Design Values of Aeroengine Reliability
航空發(fā)動機可靠性目標值的模糊決策

21、Application of ANN Technology to Aeroengine Fault Diagnosis
人工神經(jīng)網(wǎng)絡在某型航空發(fā)動機故障診斷中的應用

22、AN OPTIMAL DYNAMIC DESIGN OF AEROENGINE ROTORS WITH FREQUENCY CONSTRAINTS
帶頻率禁區(qū)的發(fā)動機轉(zhuǎn)子動力優(yōu)化設計

23、In this paper, an RBF neural network approach is applied to aeroengine gas path fault diagnosis.
本文將徑向基函數(shù)(RBF)神經(jīng)網(wǎng)絡應用到航空發(fā)動機故障診斷中。

24、Structural reliability analysis of an aeroengine 2nd-stage compressor disk is presented.
對某型發(fā)動機壓氣機第2級輪盤進行了結(jié)構(gòu)可靠性分析。

aeroengine翻譯