DocumentCode :
3084477
Title :
Control of thermo-acoustic instabilities using pulse width modulation
Author :
McManus, K.R. ; Magill, John C.
Author_Institution :
Phys. Sci. Inc., Andover, MA, USA
fYear :
1997
fDate :
5-7 Oct. 1997
Firstpage :
824
Lastpage :
829
Abstract :
An experimental study of a closed-loop control system to suppress thermo-acoustic combustion instabilities is described. The control mechanism relies on out-of-phase heat addition by means of an auxiliary fuel injector. Pulse width modulation is used to precisely control the amplitude and phase of the auxiliary fuel pulses. The controller was successfully implemented in a numerical simulation of a dynamic combustion instability and experimentally.
Keywords :
aerospace engines; closed loop systems; combustion; feedback; pulse width modulation; turbines; auxiliary fuel injector; auxiliary fuel pulses; closed-loop control system; dynamic combustion instability; out-of-phase heat addition; pulse width modulation; thermo-acoustic instabilities; Aerodynamics; Combustion; Control systems; Engines; Fires; Fuels; Pulse width modulation; Space vector pulse width modulation; Spraying; Turbines;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications, 1997., Proceedings of the 1997 IEEE International Conference on
Conference_Location :
Hartford, CT, USA
Print_ISBN :
0-7803-3876-6
Type :
conf
DOI :
10.1109/CCA.1997.627763
Filename :
627763
Link To Document :
بازگشت