turbofan engine
美 
英
- un.涡轮风扇发动机
- 网络机用涡扇引擎；涡扇发动机；涡轮扇叶发动机
英汉解释
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软件中SIMULINK工具，实现对某型发动机数控系统液压机械备份装置的仿真。
An artificial neural network based expert system has been developed and is applied to aircraft turbofan engine fault diagnosis.
介绍了人工神经网络专家系统在航空涡轮风扇发动机故障诊断上的应用。
This report discusses the study of detailed nonlinear real time performance simulation for a two spool turbofan engine with afterburner.
本文就双轴加力涡扇发动机详细非线性实时仿真模型进行了研究。
The simulation accuracy can be improved by above model for the turbofan engine transient performance.
上述模型的建立将有效的提高涡扇发动机过渡过程性能模拟程序的精度。
the windmilling start ignition characteristic of a turbofan engine was analyzed in this paper.
着重对该发动机的风车起动点火特性进行了分析。
The field replacing and repairing technologies of various stages fan blades for an turbofan engine were studied.
研究了在外场更换和修理某型涡扇发动机各级风扇叶片的技术。
The content of this article for follow-up of micro-components turbofan engine research laid the foundation for design.
本文的内容为后续的微涡扇发动机部件设计研究奠定了基础。
Based on a turbofan engine, the afterburner is replaced with pulse detonation combustor to form a turbofan-pulse detonation hybrid engine.
在涡扇发动机基础上，以脉冲爆震燃烧室代替普通加力燃烧室构成涡扇-脉冲爆震组合发动机。
A mathematical model of turbofan engine with thrust vector control was established.
建立了带推力矢量的涡扇发动机数学模型。
A small turbofan engine starting operation as an example was simulated by using this model.
并对某小型涡扇发动机起动过程进行了计算分析。
An algorithm is developed based on the N-R(Newton-Raphson) iteration method to solve the nonlinear mathematical model of turbofan engine.
提出一种基于N-R迭代方法的有限域优化搜索法，用于求解涡扇发动机数学模型。
A turbofan engine model is developed to illustrate the real time performance and the precision on the hardware platform.
结合实际的硬件平台，对所建模型的实时性和精度进行了验证。
The nozzle flow is composed of the main gas stream and the secondary air stream in order to simulate the nozzle of turbofan engine.
喷管中的气流由主流燃气和次流空气组成，用以模拟涡扇发动机的喷管。
Power will be provided by a single turbofan engine.
电力将提供一个单一的涡扇发动机。
Eventually given a 40 kg thrust class, low-pressurized than 3. 0 single-turbofan engine micro-impeller rich data and characteristic curves.
最终给出了一台40公斤推力级、低增压比为3.0的单叶轮微涡扇发动机的丰富数据和特性曲线。
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·惠特尼简称普惠提出的解决方案是名为“纯净动力PW1000G”的齿轮传动涡扇发动机。普惠是美国联合科技集团的一个分公司。
Mirage 2000 uses a SNECMA M53-P2 turbofan engine which provides 64 kN thrust and 98 kN with after burn.
幻影2000的动力装置为一个SNECMA公司的M53-P2涡扇发动机，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
面向对象的双轴混排加力涡扇发动机详细非线性实时仿真模型研究
Comparative investigation of the infrared characteristics for two exhaust systems of a turbofan engine
两种涡扇发动机排气系统红外辐射特性的比较
Method and Experimental Facility for Assessing Pressure Distortion of a Certain Turbofan Engine
某涡扇发动机压力畸变评定技术
Impact of Guide Vane Used for Wave Absorber on Turbofan Engine Performance
吸波导流体对某型涡扇发动机性能的影响
Stability Assessment Test Technology of a Turbofan Engine Inlet Temperature Distortion
某型涡扇发动机进口温度畸变的稳定性评定试验技术研究
System identification of a turbofan engine and design of its controller
涡扇发动机模型辨识及其控制器设计
The Dynamic Pressure Turbulence Calculation of a Turbofan Engine Total Pressure Distortion Test
涡扇发动机进气总压畸变试验动态总压紊流度计算分析
Study of the Application of Turbofan Engine to the Infra-red Stealthy Technology of Aircraft
涡轮风扇发动机在飞机红外隐身技术中的应用研究
Simulation of the performances of an augmented turbofan engine using three-layer iterations
某型加力涡扇发动机特性的三层迭代模拟
Effect of Inlet Total Pressure Distortion on the Performance of a Certain-type Turbofan Engine
进气总压畸变对某型涡扇发动机性能的影响
Analysis of Windmilling Start Characteristics for a Typical Turbofan Engine
涡扇发动机空中风车起动特性分析
Application of after-burning between high and low turbines to improve performance of two-spool turbofan engine
用高低压涡轮间补燃提高双轴涡扇发动机性能
Numerical Simulation for the Dynamic Influence of the Change of Gas Pumping Coefficient on the Turbofan Engine
引气系数变化对涡扇发动机动态性能影响的数值模拟
Real-Time Performance Simulation of a Mixed-Flow Two-Spool Augmented Turbofan Engine
某型双轴加力涡扇发动机实时性能仿真模型
Numerically Assessing Aerodynamic Stability of Compression Component Running in Turbofan Engine
涡扇发动机整机环境下压缩部件稳定工作边界计算方法
An Investigation on Performance of Variable Vane Control Channel for a Turbofan Engine LPC
某涡扇发动机低压压气机叶片角度控制通道性能研究
Start Ignition Characteristic Analysis of a Turbofan Engine Test
某型发动机起动试验点火特性分析
Aerodynamic stability assessment for compression component running in turbofan engine with distorted flow
畸变进气时涡扇发动机整机环境下压缩部件气动稳定性评定
Extrapolating component maps into the low speed and simulation of windmilling performance of turbofan engine
涡扇发动机低转速部件特性扩展和风车状态性能模拟
Simulation Research of Artificial Neural Network Methodology applied for Turbofan Engine Fault Diagnosis
民航涡扇发动机故障诊断的人工神经网络方法仿真研究
A Realtime Simulation Model of a Typical Turbofan Engine in Full Flight Envelope
某型涡扇发动机全包线实时仿真模型
A New Method of Optimization of Variable Geometry for Enlarging Surge Margin of a Turbofan Engine
涡扇发动机组合变几何调节优化方法研究
Object-oriented simulation platform for turbofan engine and its control system
面向对象的涡扇发动机及控制系统仿真平台
