turbofan

Simulation results of LTR control for a turbofan engine show the effectiveness of the approach.

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.

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The mathematical model of turbofan engine transient process with thrust vectoring nozzle was established.

建立带矢量喷管的涡扇发动机动态数学模型.

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The effects 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.

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Intermediate case is an important part of the turbofan engine components.

中介机匣是涡轮风扇发动机的重要承力部件.

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Abnormal vibration has been found on rear installation plane in a turbofan engine durability test.

在某民用涡轮风扇发动机的持久试车过程中,出现了发动机后安装面振动异常的现象.

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The cone gear spoke fracture is briefly described for a typical turbofan.

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.

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The method is applied to a turbofan engine control system, and is demonstrated to be feasibility.

应用于某型航空涡扇发动机控制系统设计, 仿真结果表明了其可行性.

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