دانلود مقاله ISI انگلیسی شماره 96036
ترجمه فارسی عنوان مقاله

شبیه سازی عملکرد گذرا موتور هواپیما با سیستم های سوخت و کنترل

عنوان انگلیسی
Transient performance simulation of aircraft engine integrated with fuel and control systems
کد مقاله سال انتشار تعداد صفحات مقاله انگلیسی
96036 2017 9 صفحه PDF
منبع

Publisher : Elsevier - Science Direct (الزویر - ساینس دایرکت)

Journal : Applied Thermal Engineering, Volume 114, 5 March 2017, Pages 1029-1037

ترجمه کلمات کلیدی
توربین گازی، موتور، کنترل، عملکرد گذرا، سیستم سوخت، شبیه سازی،
کلمات کلیدی انگلیسی
Gas turbine; Engine; Control; Transient performance; Fuel system; Simulation;
پیش نمایش مقاله
پیش نمایش مقاله  شبیه سازی عملکرد گذرا موتور هواپیما با سیستم های سوخت و کنترل

چکیده انگلیسی

A new method for the simulation of gas turbine fuel systems based on an inter-component volume method has been developed. It is able to simulate the performance of each of the hydraulic components of a fuel system using physics-based models, which potentially offers more accurate results compared with those using transfer functions. A transient performance simulation system has been set up for gas turbine engines based on an inter-component volume (ICV) method. A proportional-integral (PI) control strategy is used for the simulation of engine controller. An integrated engine and its control and hydraulic fuel systems has been set up to investigate their coupling effect during engine transient processes. The developed simulation system has been applied to a model aero engine. The results show that the delay of the engine transient response due to the inclusion of the fuel system model is noticeable although relatively small. The developed method is generic and can be applied to any other gas turbines and their control and fuel systems.