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电力将提供一个单一的涡扇发动机。Power will be provided by a single turbofan engine.

本论文建立了一个新的涡扇发动机起动过程模拟的模型。This paper build up a new model of turbofan engine's starting process.

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简要介绍了某型涡扇发动机中下垂直锥齿轮辐板断裂故障。The cone gear spoke fracture is briefly described for a typical turbofan.

发动机是一个有两个转子和不同的定子叶片的轴流式涡轮风扇发动机。The engine is an axial flow turbofan with two rotors and variable stator vanes.

将此设计方法应用于某型涡扇发动机的LTR控制，取得了良好的控制效果。Simulation results of LTR control for a turbofan engine show the effectiveness of the approach.

该方法在某型涡扇发动机风车特性试验中得到了成功应用。The method was satisfactorily applied to the windmilling characteristics test of a turbofan engine.

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。Mirage 2000 uses a SNECMA M53-P2 turbofan engine which provides 64 kN thrust and 98 kN with afterburn.

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目前还不清楚关于这架飞机的详细数据，如涡扇发动机和机载电子系统。Specific details of the aircraft, such as its turbofan engines and onboard systems, are not yet known.

基于改善涡扇发动机多任务适应性的目的，提出了两种解决方案。To improve the multi-mission adaptability of the reheat turbofan engine, two methods were brought forward.

但是现在的涡扇发动机功率很大并且很可靠，四发动机对于未来的飞机或许就不太合理了。But today's turbofan engines are so powerful and reliable that four may not be justified in future airliners.

本文基于面向对象技术建立了某型双轴涡扇航空发动机的部件级气动热力模型。A component level aerothermodymamic model of a turbofan aeroengine is created in this thesis using OO technology.

貌似你指的是双交叠喷口意味着是涡扇10A的某个升级版本。It sounds like you're referring to the double-overlap nozzle which suggests some sort of WS-10A turbofan variant.

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可以把这个起动模型应用到其它涡扇发动机的起动过程的模拟和设计中。The new starting model can be applied to other turbofan engine"s starting processes" numerical simulation and design.

提出了一种基于FSQP算法的涡扇发动机多变量最优加速控制方法。FSQP algorithm based multivariable optimal control method for the acceleration process of turbofan engine is developed.

较为系统地总结了国外大涵道比涡扇发动机的研制特点和设计特点。The development and design features of the high bypass ratio turbofan engine in foreign are comprehensively summarized.

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

综述了涡扇发动机风扇叶片的发展及各种风扇叶片的成形工艺。The development of fan blade of turbofan and the forming technology of all kinds of fan blades are summarized in the paper.

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这些经验对于我们今后设计大函道比涡扇发动机和螺浆风扇发动机试车台时，将是十分有用的。This experience will be very helpful in the design of test for high by-pass ratio turbofan engine and propeller-fan engine.

通过一个高涵道比涡扇发动机故障诊断的实例分析，验证了三层逆传播网络的可行性。The case study of a high bypass ratio turbofan engine has verified the feasibility of a three-layer back propagation network.

建立了一体化弹用小涡扇发动机系统含粘性力项的准三维欧拉流动模型。A quasi three dimensional flow Euler model with viscous force terms was constructed for integrated small turbofan engine systems.