turbofan engine

turbofan engine

美 　英

• un.渦輪風扇發動機
• 網絡機用渦扇引擎；渦扇發動機；渦輪扇葉發動機

英漢解釋

un.	1. 渦輪風扇發動機

例句

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 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。

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。

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。

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。

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

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

Application of after-burning between high and low turbines to improve performance of two-spool turbofan engine

用高低壓渦輪間補燃提高雙軸渦扇發動機性能

Numerical Simulation for the Dynamic Influence of the Change of Gas Pumping Coefficient on the Turbofan Engine

引氣系數變化對渦扇發動機動態性能影響的數值模擬

Real-Time Performance Simulation of a Mixed-Flow Two-Spool Augmented Turbofan Engine

某型雙軸加力渦扇發動機實時性能仿真模型

Numerically Assessing Aerodynamic Stability of Compression Component Running in Turbofan Engine

渦扇發動機整機環境下壓縮部件穩定工作邊界計算方法

An Investigation on Performance of Variable Vane Control Channel for a Turbofan Engine LPC

某渦扇發動機低壓壓氣機葉片角度控制通道性能研究

Start Ignition Characteristic Analysis of a Turbofan Engine Test

某型發動機起動試驗點火特性分析

Aerodynamic stability assessment for compression component running in turbofan engine with distorted flow

畸變進氣時渦扇發動機整機環境下壓縮部件氣動穩定性評定

Extrapolating component maps into the low speed and simulation of windmilling performance of turbofan engine

渦扇發動機低轉速部件特性擴展和風車狀態性能模擬

Simulation Research of Artificial Neural Network Methodology applied for Turbofan Engine Fault Diagnosis

民航渦扇發動機故障診斷的人工神經網絡方法仿真研究

A Realtime Simulation Model of a Typical Turbofan Engine in Full Flight Envelope

某型渦扇發動機全包線實時仿真模型

A New Method of Optimization of Variable Geometry for Enlarging Surge Margin of a Turbofan Engine

渦扇發動機組合變幾何調節優化方法研究

Object-oriented simulation platform for turbofan engine and its control system

面向對象的渦扇發動機及控制系統仿真平臺