turbofan
美 
英 ['t??b??fæn]
- n.渦輪風扇；渦輪通風器；渦輪扇發動機
- 網絡渦輪風扇發動機；渦扇；扇渦輪
詞形變化
復數：turbofans
英漢解釋
英英解釋
例句
This turbofan powerplant is being developed for the Flanker, and is also sometimes referred to as the WS-10A.
這種渦扇推力裝置就是為側衛研發，有時被稱為WS-10A。
SIMULINK tools in MATLAB were used to simulate a turbofan engine digital control system's hydraulic mechanical backup unit in this paper.
使用MATLAB軟件中SIMULINK工具，實現對某型發動機數控系統液壓機械備份裝置的仿真。
An artificial neural network based expert system has been developed and is applied to aircraft turbofan engine fault diagnosis.
介紹了人工神經網絡專家系統在航空渦輪風扇發動機故障診斷上的應用。
This report discusses the study of detailed nonlinear real time performance simulation for a two spool turbofan engine with afterburner.
本文就雙軸加力渦扇發動機詳細非線性實時仿真模型進行了研究。
The aircraft's engines could use both fuel to burn in the engine's core, and electricity to turn the turbofan when the core is powered down.
這種飛行器的引擎既能在其核心機中燃燒燃油，也能在核心機關車時用電力轉動渦輪風扇。
for virtually all commercial airliners today , the answer is " turbofan engines , " the latest in a decades - long evolution.
若以目前商用客機而言，答案是渦輪扇引擎，它是近數十年來最新的演化成果。
The simulation accuracy can be improved by above model for the turbofan engine transient performance.
上述模型的建立將有效的提高渦扇發動機過渡過程性能模擬程序的精度。
Both BA and KLM, after all, had direct experience of what flying through volcanic ash can do to a high-bypass turbofan jet engine.
畢竟，英航和荷航都有用高旁路渦輪風扇噴氣式飛機引擎穿越火山灰的經驗。
the windmilling start ignition characteristic of a turbofan engine was analyzed in this paper.
著重對該發動機的風車起動點火特性進行了分析。
The field replacing and repairing technologies of various stages fan blades for an turbofan engine were studied.
研究了在外場更換和修理某型渦扇發動機各級風扇葉片的技術。
The content of this article for follow-up of micro-components turbofan engine research laid the foundation for design.
本文的內容為后續的微渦扇發動機部件設計研究奠定了基礎。
In the first part, the mathematic model of a certain type of turbofan aeroengine is discussed.
第一部分是某型渦輪風扇發動機的數學模型及其計算方法的研究。
Unlike a conventional turbofan, it uses a gearbox rather than a shaft between the fan and the turbine.
與傳統的渦扇發動機不同它并非使用一根軸而是用齒輪箱將風扇與渦輪連接起來。
One is the geared turbofan (GTF), a new type of jet engine from Pratt & Whitney, part of America's United Technologies group.
一種是齒輪驅動渦扇（GTF），這是來自美國的聯合科技集團旗下普惠（Pratt&Whitney）公司的一種新型噴氣式引擎。
Based on a turbofan engine, the afterburner is replaced with pulse detonation combustor to form a turbofan-pulse detonation hybrid engine.
在渦扇發動機基礎上，以脈沖爆震燃燒室代替普通加力燃燒室構成渦扇-脈沖爆震組合發動機。
MK2 fuselage and empennage structure would be re-lied and reassembled, with redesigned wings and BR710 turbofan engines.
MK2型的機身和尾部結構將進行延壽和重新組裝，包括采用重新設計的新型機翼和BR710渦扇發動機。
A mathematical model of turbofan engine with thrust vector control was established.
建立了帶推力矢量的渦扇發動機數學模型。
A small turbofan engine starting operation as an example was simulated by using this model.
并對某小型渦扇發動機起動過程進行了計算分析。
An algorithm is developed based on the N-R(Newton-Raphson) iteration method to solve the nonlinear mathematical model of turbofan engine.
提出一種基于N-R迭代方法的有限域優化搜索法，用于求解渦扇發動機數學模型。
A turbofan engine model is developed to illustrate the real time performance and the precision on the hardware platform.
結合實際的硬件平臺，對所建模型的實時性和精度進行了驗證。
The nozzle flow is composed of the main gas stream and the secondary air stream in order to simulate the nozzle of turbofan engine.
噴管中的氣流由主流燃氣和次流空氣組成，用以模擬渦扇發動機的噴管。
Pratt & Whitney has entered early testing on the PurePower PW1524G geared turbofan, having achieved idle and full power runs.
普惠公司已開始對其潔凈動力PW1524G齒輪傳動式渦輪風扇發動機進行空車及全推力測試。
But the geared turbofan and the open rotor are so different from each other that they will need different airframes.
但是齒輪傳動渦扇發動機以及開放轉子發動機之間如此巨大的差異使得他們將需要不同的飛機構型。
Power will be provided by a single turbofan engine.
電力將提供一個單一的渦扇發動機。
Eventually given a 40 kg thrust class, low-pressurized than 3. 0 single-turbofan engine micro-impeller rich data and characteristic curves.
最終給出了一臺40公斤推力級、低增壓比為3.0的單葉輪微渦扇發動機的豐富數據和特性曲線。
The solution devised by Pratt &Whitney (P&W), a division of United Technologies, is a "geared turbofan" engine called the PurePower PW1000G.
由普拉特·惠特尼簡稱普惠提出的解決方案是名為“純凈動力PW1000G”的齒輪傳動渦扇發動機。普惠是美國聯合科技集團的一個分公司。
Mirage 2000 uses a SNECMA M53-P2 turbofan engine which provides 64 kN thrust and 98 kN with after burn.
幻影2000的動力裝置為一個SNECMA公司的M53-P2渦扇發動機，推力64千牛，加力推力98千牛。
A Study of Object-Oriented Detailed Nonlinear Real-Time Performance Simulation for a Mixed-Flow Two-Spool Turbofan Engine with Afterburner
面向對象的雙軸混排加力渦扇發動機詳細非線性實時仿真模型研究
Comparative investigation of the infrared characteristics for two exhaust systems of a turbofan engine
兩種渦扇發動機排氣系統紅外輻射特性的比較
Method and Experimental Facility for Assessing Pressure Distortion of a Certain Turbofan Engine
某渦扇發動機壓力畸變評定技術
Impact of Guide Vane Used for Wave Absorber on Turbofan Engine Performance
吸波導流體對某型渦扇發動機性能的影響
Stability Assessment Test Technology of a Turbofan Engine Inlet Temperature Distortion
某型渦扇發動機進口溫度畸變的穩定性評定試驗技術研究
System identification of a turbofan engine and design of its controller
渦扇發動機模型辨識及其控制器設計
The Dynamic Pressure Turbulence Calculation of a Turbofan Engine Total Pressure Distortion Test
渦扇發動機進氣總壓畸變試驗動態總壓紊流度計算分析
Study of the Application of Turbofan Engine to the Infra-red Stealthy Technology of Aircraft
渦輪風扇發動機在飛機紅外隱身技術中的應用研究
A Study of Enlarging Surge Margin and Optimization of Variable Geometry for Afterburning Turbofan Engines
某型加力渦扇發動機變幾何擴穩優化模擬
Simulation of the performances of an augmented turbofan engine using three-layer iterations
某型加力渦扇發動機特性的三層迭代模擬
Effect of Inlet Total Pressure Distortion on the Performance of a Certain-type Turbofan Engine
進氣總壓畸變對某型渦扇發動機性能的影響
Analysis of Windmilling Start Characteristics for a Typical Turbofan Engine
渦扇發動機空中風車起動特性分析
Numerical Simulation of the Influence of Nozzle Area Control Accuracy on Turbofan Afterburning Performance
噴管面積調節精度對某型渦扇發動機加力性能影響的數值仿真
