Active control of nonlinear pressure oscillations in combustion chambers
A theoretical analysis of active control of nonlinear acoustic instabilities in combustion chambers is developed in this article. The formulation starts with a generalized wave equation that describes the dynamic behavior of second-order nonlinear oscillations with distributed feedback actions. Cont...
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Veröffentlicht in: | Journal of propulsion and power 1992-11, Vol.8 (6), p.1282-1289 |
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Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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Zusammenfassung: | A theoretical analysis of active control of nonlinear acoustic instabilities in combustion chambers is developed in this article. The formulation starts with a generalized wave equation that describes the dynamic behavior of second-order nonlinear oscillations with distributed feedback actions. Control inputs are provided by the burning of the injected secondary fuel in the chamber, with its instantaneous mass flow rate modulated by a proportional-plus-integral (PI) controller located between the pressure sensor and the fuel injection mechanism. Various nonlinear-stability characteristics, including the existence and stability of limit cycles, are studied analytically using the method of time averaging. In addition, an optimization procedure is developed for selecting controller gains. |
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ISSN: | 0748-4658 1533-3876 |
DOI: | 10.2514/3.11474 |