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- Power will be provided by a single turbofan engine. 电力将提供一个单一的涡扇发动机。
- For example: Number 1 engine cowling; number 3 latch is not secure. 一号发动机整流罩的三号锁扣未扣紧。
- The skin of the fuselage, stabilizers, and engine cowling was severely buckled. 机身,平衡舵以及发动机舱盖的外壳都被扭曲得很厉害。
- Dense smoke coming out of No4 engine cowling( engine nacelle), fire suspected. 第四号发动机整流罩冒浓烟,可能着火。
- 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。
- The reverser sleeve is part of the engine cowling . the actuating system is on the reverser. 反推器的外壳是发动机整流罩的要部分。作动系统在反推器上。
- The method was satisfactorily applied to the windmilling characteristics test of a turbofan engine. 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。
- Please open the engine cowling and check for leakage overheat wires electrical connectors . 请打开发动机包皮检查渗漏过热导线插头。
- The development and design features of the high bypass ratio turbofan engine in foreign are comprehensively summarized. 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。
- Please open the engine cowling and check for leakage /overheat /wires //electrical connectors . 请打开发动机包皮检查渗漏/过热/导线/插头。
- 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。
- The new starting model can be applied to other turbofan engine"s starting processes" numerical simulation and design. 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 research of this paper is useful for improving design of turbofan engine control system. 本文的研究工作对 今后涡轮风扇发动机控制系统的设计改进是有一定的意义。
- 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。
- The Cruiser incorporates other refinements as well, including an aerodynamic engine cowl with prop spinner and fully balanced controls. 巡洋舰采用其他改进,包括了空气动力学的引擎罩与道具微调,并充分平衡控制。
- In this paper,the integrated flight/propulsion control system of a new fighter and its new turbofan engine are studied. 文中采用遗传算法实现了对PID参数的最佳整定。
- FSQP algorithm based multivariable optimal control method for the acceleration process of turbofan engine is developed. 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。
- Finally one of the principia overall structure design of this kind of turbofan engine was worked out. 最后拟出了相应的发动机主体结构。
- A method for incorporating linear state inequality constraints in a Kalman filter is proposed and applied to turbofan engine health estimation. 提出了一种加入线性不等式约束的卡尔曼滤波方法,并用于涡扇发动机的健康状况估计。
- A fault diagnosis equation for the twin-spool mixed flow turbofan engine was established based on the simulation and gas path analysis. 并以此为基础运用气路分析原理,选取表征发动机性能参数变化的症兆变量和测量参数,建立了发动机故障诊断小偏差方程。