Wang, ChenLi, YiguangYang, B. Y.2017-01-102017-01-102016-12-10Wang C, Li YG, Yang BY. Transient Performance Simulation of Aircraft Engine Integrated with Fuel and Control Systems. Applied Thermal Engineering, Volume 114, 5 March 2017, Pages 1029–10371359-4311http://dx.doi.org/10.1016/j.applthermaleng.2016.12.036https://dspace.lib.cranfield.ac.uk/handle/1826/11234A 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.enAttribution-NonCommercial-NoDerivatives 4.0 Internationalhttp://creativecommons.org/licenses/by-nc-nd/4.0/Gas turbineEngineControlTransient performanceFuel systemSimulationArticle15980753