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- W2364367067 abstract "In order to satisfy the high capability of modern aviation turbojet engine,a new aeroengine control system was developed with digital electronic control technique.A turbine rotate speed measure signal was used to unchain the coupling affect between the rotate speed and controlled fuel flux.A fuel flux measure signal was used to compensate the variable gain parameter of turbine rotate speed which influenced by the flight altitude,mach number and rotate speed of turbine.A variable parameters PID control algorithm was used to achieve the zero static error of turbine rotate speed and non-overshooting adjusting of controlled fuel flux.The results show that: the control precision,speed and stability can be improved obviously by using this method;the control effect of electronic adjusted system is better than the one of mechanical hydraulic adjuster.4 figs,8 refs." @default.
- W2364367067 created "2016-06-24" @default.
- W2364367067 creator A5038008601 @default.
- W2364367067 date "2009-01-01" @default.
- W2364367067 modified "2023-09-23" @default.
- W2364367067 title "Electronic adjust for turbojet engine based on variable parameters PID control" @default.
- W2364367067 hasPublicationYear "2009" @default.
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