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turbofan

美英 ['tɜːbəʊfæn]

n.涡轮风扇；涡轮通风器；涡轮扇发动机
网络涡轮风扇发动机；涡扇；扇涡轮

复数：turbofans

turbofan

英-汉英-英网络释义

turbofan

涡轮风扇发动机

涡轮风扇发动机（Turbofan）是飞机发动机的一种，由涡轮喷气发动机（Turbojet）发展而成。与涡轮喷气比较，主要特点是 …

涡扇

航空相关VOCA 中英文对照单词表 - 豆丁网 ... troubleshooting 排故 turbofan 涡扇 turbulence detection 紊流探测 ...

涡轮扇

744发动机属於涡轮扇(Turbofan)发动机PW4000系列 4052 4056 4060 4062GE CF6-80C2R&R RB211-524系列单颗发动机的 …

扇涡轮

英语新词汇与常用词汇的翻译... ... turbo 涡轮 turbofan 扇涡轮 turbogenerator 涡轮式发电机 ...

涡扇发动机

这是涡扇发动机(Turbofan)适合使用在商用飞机 - 比较省油,操作温度较低,制造/维护/操作花费也较低。但是没有发动机参数也 …

涡轮扇叶发动机

...轮发动机（Gas turbine），与属于内燃机的涡轮扇叶发动机（Turbofan）。

涡轮风扇式

...使飞机前进，不用螺旋桨，现已渐被淘汰，代之而起的涡轮风扇式（turbofan）如 A300 或 B747-300 即是。

例句：

This turbofan powerplant is being developed for the Flanker, and is also sometimes referred to as the WS-10A.

这种涡扇推力装置就是为侧卫研发，有时被称为 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 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 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.

这种飞行器的引擎既能在其核心机中燃烧燃油，也能在核心机关车时用电力转动涡轮风扇。

for virtually all commercial airliners today , the answer is " turbofan engines , " the latest in a decades - long evolution .

若以目前商用客机而言，答案是涡轮扇引擎，它是近数十年来最新的演化成果。

Both BA and KLM, after all , had direct experience of what flying through volcanic ash can do to a high-bypass turbofan jet engine .

毕竟，英航和荷航都有用高旁路涡轮风扇喷气式飞机引擎穿越火山灰的经验。

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 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。

In the first part, the mathematic model of a certain type of turbofan aeroengine is discussed.

第一部分是某型涡轮风扇发动机的数学模型及其计算方法的研究。

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。

MK2 fuselage and empennage structure would be re-lied and reassembled, with redesigned wings and BR710 turbofan engines .

MK2 型的机身和尾部结构将进行延寿和重新组装，包括采用重新设计的新型机翼和 BR710 涡扇发动机。

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。

Pratt & Whitney has entered early testing on the PurePower PW1524G geared turbofan, having achieved idle and full power runs.

普惠公司已开始对其洁净动力 PW1524G 齿轮传动式涡轮风扇发动机进行空车及全推力测试。

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

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