aero-engine
美 
英
例句
Two numerical examples and a practical example of an aero engine disk were presented herein to validate stochastic response surface method.
兩個數值例子和一個發動機輪盤實例來驗證這一方法的有效性。
The concept of regulation and control for the aero engine service life is developed to improve its reliability.
從提高發動機使用可靠性角度，研究了某型發動機使用壽命調控方案。
An intelligent PMA for flaw detection of aero engine is presented, which can be used for data analysis and decision.
針對發動機探傷數據分析、判斷手段落后等問題，研制了一種智能PMA。
The computation methods and code referred could be applied to estimating the infrared radiation of practical aero engine exhaust system.
所開發的計算方法與程序可用于排氣系統紅外輻射特性的數值計算與分析，基本滿足工程設計的需要。
Through the analysis of a system identification example of X aero-engine EEC (engine electronic controller) , the result shows this.
經對某航空發動機電子綜合調節器燃油通道動態過程參數模型辨識的實例，驗證了該算法精確快速。
Three threshold-lines evaluation was used to analyze direct reading ferrograph data of lubricating oil from aero-engine.
利用線閾法分析某型航空發動機潤滑油樣的直讀鐵譜數據，提出油液直讀鐵譜分析診斷標準。
Full Authority Digital Electronic Control and advanced control strategy are the dominant directions in the current aero-engine control.
全權限數字電子控制以及先進控制策略是當今航空發動機控制的主流方向。
A new neural network algorithm with fuzzy logic compensation was proposed and applied to an aero- engine rotating speed control system.
提出了一種帶模糊補償的神經網絡辨識器，并應用在某型渦扇發動機轉速控制系統中。
Health assessment of aero-engine is an important technical measure for ensuring engine safe working and prolonging engine operating life.
航空發動機健康狀況評估是保證發動機安全工作、延長發動機使用壽命的一種重要技術措施。
The contra-rotating turbine disks of an aero-engine were simplified as a counter-rotating plan disk system.
將反向旋轉的高低壓渦輪盤簡化成了幾何形狀相對簡單的反轉盤系統。
The dynamic characteristics of three types of aero engine have been analyzed with this program and the results are satisfactory.
目前該程序已實際應用于三種型號的發動機上，獲得了滿意效果。
Fuel pump and lube pump used in present aero-engine and space-engine are oriented to smaller volume, bigger flux and higher pressure.
目前，航空航天發動機控制系統中的燃油供油泵、滑油增壓泵都在向著小體積、高轉速、大流量、高壓力的方向發展。
The method was applied to diagnosis the aero engine wear fault. Example shows the validity of the method proposed.
將該方法用于某型航空發動機的磨損故障診斷專家系統中，實驗證明了該方法的有效性。
GTE persists in seeking for an advanced position in aero-engine design, test and instrumentation technologies.
中國燃氣渦輪研究院以追求航空發動機設計、試驗、測試技術研究能力和水平在行業內領先為理念；
Honeycomb segment was an important sealing structure of the aero engine.
蜂窩篦齒是航空發動機中的重要封嚴結構。
Moreover, the acquired fault symptom was applied to fuzzy cluster analysis to obtain aero engine fault sources.
在此基礎上，應用模糊聚類分析方法，依據最大隸屬度原則得到發動機早期故障源。
In this case, it is a key technique to determine the operating life of aero engine main bearing.
在這種情況下，如何科學地確定主軸軸承壽命就是個難度很大的技術問題。
The system has been actually tested on our aero-engine test bed and appraised by the Aero -Industry Ministry.
本系統在發動機試車臺上進行了試驗，并通過了航空工業部部級鑒定。
Critical technologies for aero engine prognostics and health management systems development were summarized.
總結歸納了航空發動機預測健康管理系統設計的關鍵技術。
Finally, a case of aero-engine blade and blisk, the algorithm solving process was presented.
最后，以航空發動機某型葉片與輪轂為例，給出了算法求解過程。
The safety lives of parts in an aero engine are determined by use of the confidence limits of three parameter Weibull distribution.
用三參數威布爾分布的置信限，確定某發動機零件的安全壽命。
To realize the Aero- engine digital control simulation, it is necessary to create a real - time Aero- engine model.
建立航空發動機實時數學模型對于實現航空發動機數字控制是必不可少的。
The vibration test and failure diagnostics are important safeguarding measures during aero-engine tests and component tests.
振動測試與故障診斷是航空發動機整機和部件試驗中的一項重要安全保障工作。
The turbine disk is a key component of the aero engine and its work condition is severe.
渦輪盤是航空發動機關鍵件，其工作載荷復雜。
Simulation results show that the given mathematic model for aero engine starting system is feasible.
最后以典型發動機起動系統作為仿真實例驗證了此方法的可行性。
Based on collaborative working platform, full lifecycle management for aero-engine developing projects can be provided.
基于協同工作平臺提供對航空發動機研制項目的全生命周期管理。
The model provides theoretical way for the research of the thermoacoustic oscillation in the aero-engine afterburner.
該模型的建立為預測航空發動機加力燃燒室振蕩燃燒特性及控制規律提供了一種理論探索途徑。
The operation performance of an aero engine fuel nozzle was tested and investigated.
本文對某型航空發動機燃油噴嘴的工作特性和霧化質量進行了試驗研究。
Results Aero engine linear model within flight envelope designed point and active fault-tolerant controller.
結果得到在飛行包線設計點發動機線性模型和主動容錯控制器。
The flow-thermal coupling calculation of aero engine air system includes fluid network and thermal network.
發動機空氣系統可分別建立流體網絡與熱網絡進行耦合計算。
V-shaped flame holder has been widely applied in aero-engine afterburner since the third generation aero-engine.
傳統發動機加力燃燒室都采用V型火焰穩定器組織燃燒，自加力出現到第三代發動機，該方案一直得到了廣泛應用。
Pretreatment and Time-domain analysis were studied to the vibration signal of aero-engine in this paper.
本文研究了發動機振動信號的預處理和對信號的時域、幅域分析。
It provided the sustain to deal with the vibration signal of Aero-engine.
為發動機振動信號的處理提供了理論依據。
This approach is applied to aero-engine control under transient conditions. As a result, the process is perfect.
將這種方法應用于某型航空發動機的過渡態控制中，得到了理想的控制結果。
Idea of Aero-engine Development by "Core-engines in Series and Derivation"
“系列核心機及派生發展”的航空發動機發展思路
The author believes that adopting appropriate control strategy based on neural network in aero-engine control has obvious advantage.
作者認為，對于航空發動機這種嚴重非線性被控對象，選擇合適的神經網絡控制方案有著明顯的優勢。
A new general approach for aero-engine and other complex mechanical system performance monitoring was put forward.
本文的研究為航空發動機及其它復雜機械系統的性能監控提出了一種新的普適性方法。
Because of its unique features, aero engine power generation can provide quality and clean distributed power.
航改燃機發電因其獨有的特點，可以提供優質、清潔的新型分布式電能。
The CAT system can fulfill the technologic demands for aero engine test-run entirely.
系統工作穩定可靠，操作簡單，維護方便，能夠完全滿足發動機的試車技術要求。
Believed the earth sphere said, thought may reach East's India and China from the European Xi'an Aero-Engine.
相信大地球形說，認為從歐洲西航可達東方的印度和中國。
