以某型渦噴發(fā)動機(jī)及其主燃油系統(tǒng)的機(jī)械液壓式調(diào)節(jié)器為研究對象,在考慮其控制規(guī)律的前提下,建立了轉(zhuǎn)速控制系統(tǒng)及其各部件的數(shù)學(xué)模型.根據(jù)所建立的數(shù)學(xué)模型,利用SIMULINK仿真工具對轉(zhuǎn)速控制系統(tǒng)進(jìn)行了仿真研究.研究結(jié)果表明該轉(zhuǎn)速控制系統(tǒng)滿足了實(shí)際要求,同時(shí)本文為主燃油系統(tǒng)的進(jìn)一步改進(jìn)提供了基礎(chǔ).
關(guān)鍵詞：渦噴發(fā)動機(jī) 主燃油系統(tǒng) 轉(zhuǎn)速控制系統(tǒng) 數(shù)學(xué)模型 仿真
The research of rotational speed control system of X aeroengine based on simulink
DUAN Chong, XIE Shou-sheng, CHEN Dun-jun (Dept of Mech Engin , The Engineering Institute , Air Force Engineering University, Xi’an 710038,China) Abstract: A turbojet engine and its main fuel control system with hydro-mechanical regulator are studied. The rotational speed control system is modeled according to the analysis of the engine control program. According to these mathematical models, the rotational speed control system is simulated with the SIMULINK in toolbox of MATLAB. The result indicates that the rotational speed control system meets practical demand. This work has important value for further research and improvement in the main fuel control system.
Key words: turbojet engine; main fuel control system; rotational speed control system; mathematical model; simulation