查询词典 turbofan

The aircraft is said to be powered by two DV-2F or AI-222K-25F turbofan engines with afterburner.

飞机采用二台DV-2F型或采用加力燃烧室的AI-222K-25F型涡扇发动机提供动力。

The 30,000 lbf (130 kN)-class afterburning turbofan engine had enough thrust to lift the weight of the 20,000 lb (9,072 kg) aircraft.

在30，000磅（130千牛）级加力涡扇发动机有足够的推力，以解除对的20000磅飞机的重量。

F-15E Strike EagleThis jet, with its two huge afterburning turbofan engines, shakes the ground as it flashes by, just above the runway and just below the speed of sound.

的F - 15 E罢工eaglethis射流，与它的两个巨大的加力涡扇发动机，摇了摇地面，因为它闪烁，刚刚超过跑道和仅低于音速。

The effects of thrust vectoring angle and angular velocity of vectoring on turbofan engine operation were investigated.

研究了矢量喷管偏转角和偏转角速度对涡扇发动机工作的影响。

Surge announciator of a turbofan engine is one of the major components of EEC.

1引言某型涡扇发动机喘振信号器是发动机的重要附件之一，也是综合电子调节器系统的关键外部传感器之一。

The dynamic process of the aero engine was described by using the Volterra progression model. And identification arithmetic of the Volterra progression model for aero engines was proposed. It was applied to a certain turbofan engine by imitating the dynamic respondence.

利用Volterra级数对航空发动机的动态过程进行描述，建立非线性模型，提出了模型的辨识算法利用某型涡扇发动机的动态仿真，进行了发动机Volterra模型辨识及验证。

Turbofan engine ; Ramjet engine ; Compound engine ; Aerospace plane ; Design ; Research

涡轮风扇发动机；冲压式喷气发动机；混合式发动机；航空航天飞机；设计；研究

The same technology can used to develop a suitable turbofan engine for the cruise missile.

相同的技术能用于为巡航导弹发展一种适当的涡扇发动机。

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。

Firstly,based on the WR Sexton method,the method and mathematic models of supplementing the sub-idle rotating component characteristics is presented.Secondly,the turbofan windmilling high-low pressure rotor co-working equations and the whole engine co-working equations are established.lastly,a turbofan engine windmilling characteristics under various windmilling conditions are simulated and analyzed.

首先，基于不可压流理论，附以可压缩效应修正的指数法发展了补充慢车转速以下部件特性的计算模型和计算程序；其次，根据流量连续、压力平衡、功率平衡、燃烧室进出口总温相等及转速相等等约束条件建立了风车状态时涡扇发动机高低压转子及整机的共同工作方程；最后发展了具有一定计算精度的涡扇发动机风车状态特性计算模型和程序，并以某型涡扇发动机为例，计算分析了不同飞行条件下发动机的风车特性，从计算结果看，其趋势是合理的。

The split between the two groups can hardly be papered over.

这两个团体间的分歧难以掩饰。

This approach not only encourages a greater number of responses, but minimizes the likelihood of stale groupthink.

这种做法不仅鼓励了更多的反应，而且减少跟风的可能性。