1. Control of Lean Blowout in a Swirl-Stabilized Dump Combustor at Different Levels of Premixing Based on Flame Colour.
- Author
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De, Somnath, Bhattacharya, Arijit, Mukhopadhyay, Achintya, and Sen, Swarnendu
- Subjects
ROCKET engines ,AIRPLANE motors ,COMBUSTION ,SOLENOIDS ,FURNACES ,LEAN combustion - Abstract
Presently, the use of lean combustion has been growing in industrial furnaces, aero-engine, and rocket engine applications due to their low $$N{O_X}$$ N O X emission and minimum maintenance requirements. On the other hand, due to the excessively low combustion reaction rate, the operation at a low fuel–air ratio leads to the sudden shutdown of the engines, which is termed lean blowout (LBO). Therefore, to operate land-based and aircraft engines at an extremely lean fuel–air mixture, control of LBO has become indispensable. In the present work, we develop several feedback in-loop control strategies using a pixel-averaged intensity ratio between the red and blue components of the flame emission. During a lean operation, based on the quantification of the proximity of the combustion dynamics to the LBO limits using this color ratio, the control strategies make the solenoid valves active to inject a secondary pilot fuel and energize the flame base. We notice that a proper choice of the color ratio as a threshold enhances the stability of both premixed and partially premixed combustion using a low pilot fuel. Besides, we test $$N{O_X}$$ N O X emission for unpiloted and piloted operations and find that the emission is only marginally affected during a pilot injection. [ABSTRACT FROM AUTHOR]
- Published
- 2024
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