您要查找的是不是:
- Study of real-time performance simulation of a mixed-flow two-spool augmented turbofan engine used in a flight simulator was carried out. 對飛行模擬機用的多變量控制的雙軸加力渦扇發(fā)動(dòng)機實(shí)時(shí)性能仿真模型進(jìn)行了研究。
- Simulation of the performances of an augmented turbofan engine using three-layer iterations 某型加力渦扇發(fā)動(dòng)機特性的三層迭代模擬
- Real-Time Performance Simulation of a Mixed-Flow Two-Spool Augmented Turbofan Engine 某型雙軸加力渦扇發(fā)動(dòng)機實(shí)時(shí)性能仿真模型
- Power will be provided by a single turbofan engine. 電力將提供一個(gè)單一的渦扇發(fā)動(dòng)機。
- The mathematical model of turbofan engine transient process with thrust vectoring nozzle was established. 建立帶矢量噴管的渦扇發(fā)動(dòng)機動(dòng)態(tài)數學(xué)模型。
- The method was satisfactorily applied to the windmilling characteristics test of a turbofan engine. 該方法在某型渦扇發(fā)動(dòng)機風(fēng)車(chē)特性試驗中得到了成功應用。
- The development and design features of the high bypass ratio turbofan engine in foreign are comprehensively summarized. 較為系統地總結了國外大涵道比渦扇發(fā)動(dòng)機的研制特點(diǎn)和設計特點(diǎn)。
- Simulation results of LTR control for a turbofan engine show the effectiveness of the approach. 將此設計方法應用于某型渦扇發(fā)動(dòng)機的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. 可以把這個(gè)起動(dòng)模型應用到其它渦扇發(fā)動(dòng)機的起動(dòng)過(guò)程的模擬和設計中。
- The research of this paper is useful for improving design of turbofan engine control system. 本文的研究工作對 今后渦輪風(fēng)扇發(fā)動(dòng)機控制系統的設計改進(jìn)是有一定的意義。
- The effects of thrust vectoring angle and angular velocity of vectoring on turbofan engine operation were investigated. 研究了矢量噴管偏轉角和偏轉角速度對渦扇發(fā)動(dòng)機工作的影響。
- In this paper,the integrated flight/propulsion control system of a new fighter and its new turbofan engine are studied. 文中采用遺傳算法實(shí)現了對PID參數的最佳整定。
- FSQP algorithm based multivariable optimal control method for the acceleration process of turbofan engine is developed. 提出了一種基于FSQP算法的渦扇發(fā)動(dòng)機多變量最優(yōu)加速控制方法。
- Finally one of the principia overall structure design of this kind of turbofan engine was worked out. 最后擬出了相應的發(fā)動(dòng)機主體結構。
- A method for incorporating linear state inequality constraints in a Kalman filter is proposed and applied to turbofan engine health estimation. 提出了一種加入線(xiàn)性不等式約束的卡爾曼濾波方法,并用于渦扇發(fā)動(dòng)機的健康狀況估計。
- A fault diagnosis equation for the twin-spool mixed flow turbofan engine was established based on the simulation and gas path analysis. 并以此為基礎運用氣路分析原理,選取表征發(fā)動(dòng)機性能參數變化的癥兆變量和測量參數,建立了發(fā)動(dòng)機故障診斷小偏差方程。
- In the end, a turbofan engine"s starting process with the new starting process model is simulated and the new model gives reasonable results. 最后利用建立的模型對某型渦扇發(fā)動(dòng)機的起動(dòng)過(guò)程進(jìn)行了數值模擬,得到了合理準確的結果。
- The nozzle flow is composed of the main gas stream and the secondary air stream in order to simulate the nozzle of turbofan engine. 噴管中的氣流由主流燃氣和次流空氣組成,用以模擬渦扇發(fā)動(dòng)機的噴管。
- The application of the approach to establishing the small perturbation SVM for a turbofan engine shows its effectiveness. 應用該方法建立某型渦扇發(fā)動(dòng)機的小偏差狀態(tài)變量模型,具有較高的精度,從而驗證了該方法的有效性。
- The life usage consumption of turbine operating blade of some typical missile turbofan engine was predicted by working data processing. 利用某短壽命發(fā)動(dòng)機的開(kāi)車(chē)數據,對其高壓渦輪葉片使用壽命進(jìn)行了預測。