turbofan的例句大全

Design and tests of jet fuel starter-assisted airstarts for turbofan engines

涡扇发动机起动机辅助空中起动方案设计和试验

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An important concept on the phase of high performance military turbofan engine's designing, throttle ratio, is discussed in this paper.

强调论述了高性能加力涡扇发动机设计论证阶段的个重要概念节流比。

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Fault quantitative diagnosis of turbofan gas path component by BPN

涡扇发动机气路故障定量诊断的BP网络研究

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Application of BPN to quantitative diagnosis of gas path component faults in turbofan

BPN在涡扇发动机气路故障诊断中的应用

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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

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Application of SQP to Multi-Object Optimization of Turbofan Engine Acceleration Control

利用SQP控制涡扇发动机加速过程的多目标最优化研究

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Application of SQP to acceleration control of turbofan engine

SQP方法在航空发动机加速过程控制中的应用研究

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The optimal control for turbofan engine acceleration control has been investigated. The optimal method used in this paper is Sequential Quadratic Programming ( SQP), one of the most successful methods for solving nonlinear constrained problem.

本文研究了采用非线性规划方法中的序列二次规划最优化方法解决涡轮风扇发动机加速过程的最优控制问题。

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Chinese large aircraft turbofan engine must be verified through inclusive to obtain airworthiness certificate.

航空大国在民用和军用航空发动机规范中都有专门条文对包容性做出严格规定，我国自行研制的大飞机涡扇发动机，要取得适航证，就必须通过包容性验证。

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For correct and wide application of reduced thrust takeoff technique, the temperature characteristics of high bypass ratio turbofan engines and the takeoff performance of large aircrafts were analyzed.

为正确使用和推广减推力起飞技术，分析了高涵道比涡轮风扇发动机温度特性和大型民航机起飞性能。

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Design Study of a dual-cycle turbofan-ramjet engine for a hypersonic aircraft

用于高超音速飞行器的涡扇-冲压双循环发动机设计研究

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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。

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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

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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。

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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。

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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

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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

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but today's turbofan engines are so powerful and reliable that four may not be justified in future airliners.

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。

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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。

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furthermore, to resolve the difficulties of complex structure in micro-turbofan engines, a newly conceived integral fan-compressor component with both high-low blades and splitter blades is claimed.

进一步，为解决微型涡扇发动机的结构复杂性困难，提出了一种微型高矮叶片单叶轮风扇压气机的压缩系统气动布局和结构设计方案。

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