1、Signal Acquisition and Processing of CAT System for Aeroengine Test Run
航空發(fā)動(dòng)機(jī)CAT系統(tǒng)信號(hào)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(dòng)機(jī)試車計(jì)算機(jī)輔助試驗(yàn)系統(tǒng)的開發(fā)；

3、Fault Detection of Microprcessor System in Aeroengine FADEC
發(fā)動(dòng)機(jī)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(jī)的渦扇發(fā)動(dòng)機(jī)試車故障診斷

5、Ceramic Coating of Aeroengine Turbine Blade
陶瓷涂層在航空發(fā)動(dòng)機(jī)渦輪葉片表面處理中的應(yīng)用

6、A new method measuring aeroengine T_4 temperature
一種測量航空發(fā)動(dòng)機(jī)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(dòng)機(jī)制造中的應(yīng)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(dòng)機(jī)低壓壓氣機(jī)輪盤的主要失效形式。

9、Machining Technologies for T Slots of Aeroengine Casings
航空發(fā)動(dòng)機(jī)機(jī)匣T型槽加工技術(shù)

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

11、APPLICATION OF LOW BTU GASES TO AEROENGINE MODIFIED FOR INDUSTRIAL USE
關(guān)于低熱值煤氣在航機(jī)改型中的應(yīng)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(dòng)機(jī)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(dòng)機(jī)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(dòng)機(jī)自適應(yīng)控制

15、An Identification Model of Aeroengine Starting Process Based on RBF Network
基于RBF網(wǎng)絡(luò)的發(fā)動(dòng)機(jī)起動(dòng)過程的模型辨識(shí)

16、Design of codec for FIR used in the telemetry of aeroengine rotor
航空發(fā)動(dòng)機(jī)轉(zhuǎn)子參數(shù)遙測中的FIR編解碼器設(shè)計(jì)

17、Condition Monitoring of Aeroengine Based on Wavelet Process Neural Networks
基于小波過程神經(jīng)網(wǎng)絡(luò)的飛機(jī)發(fā)動(dòng)機(jī)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(luò)的航空發(fā)動(dòng)機(jī)轉(zhuǎn)子連接件方案設(shè)計(jì)系統(tǒng)

19、Structural Reliability Analysis of an Aeroengine Compressor Disk
某型發(fā)動(dòng)機(jī)壓氣機(jī)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(dòng)機(jī)可靠性目標(biāo)值的模糊決策

21、Application of ANN Technology to Aeroengine Fault Diagnosis
人工神經(jīng)網(wǎng)絡(luò)在某型航空發(fā)動(dòng)機(jī)故障診斷中的應(yīng)用

22、AN OPTIMAL DYNAMIC DESIGN OF AEROENGINE ROTORS WITH FREQUENCY CONSTRAINTS
帶頻率禁區(qū)的發(fā)動(dòng)機(jī)轉(zhuǎn)子動(dòng)力優(yōu)化設(shè)計(jì)

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(luò)應(yīng)用到航空發(fā)動(dòng)機(jī)故障診斷中。

24、Structural reliability analysis of an aeroengine 2nd-stage compressor disk is presented.
對某型發(fā)動(dòng)機(jī)壓氣機(jī)第2級(jí)輪盤進(jìn)行了結(jié)構(gòu)可靠性分析。

aeroengine翻譯