Method and device for modulation of a flame
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorsKenneth J. Wilson, Kenneth H. Yu, Timothy Parr, Klaus C. Schadow
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AssigneeThe United States of America as represented by the Secretary of the Navy
InventorsKenneth J. Wilson, Kenneth H. Yu, Timothy Parr, Klaus C. Schadow
Estimating the term…
This invention relates to air breathing engines, such as ramjets, scramjets and internal combustion, and more particularly to an active combustion control device for a combustor. In more particularity, the present invention relates to a method and apparatus that applies active combustion control technology to advanced propulsion devices and closed-loop fuel injection at sub-harmonic frequencies of the instability frequency of the combustor. The problem of limited actuator frequency response is addressed by injecting fuel pulses at sub-harmonic frequencies of the instability. The fuel may be liquid, solid or gas. To achieve this desired result, a closed loop controller is designed to determine sub-harmonic frequencies using a divider to divide the instability frequency of a combustor, yielding a fraction of the harmonic frequency. Also, this invention also combines open loop injection control with closed loop injection control to obtain enhanced engine performance, which includes extension of the stable combustion zone.
A method of active control modulation of a flame in a combustor having an instability frequency by injecting pulsed fuel via a plurality of actuators having at least one closed loop actuator and at least one open loop actuator, comprising:
An apparatus for active control modulation of a flame in a combustor having instabilities, wherein the instabilities cause natural oscillations, by injecting pulsed fuel, comprising:
Dependencies are inferred from the claim text.