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Journal ArticleDOI

Challenges and Progress in Controlling Dynamics in Gas Turbine Combustors

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TLDR
In this article, the components of a combined analytical, experimental, and computational approach to understand and control combustion dynamics are developed for turbopropulsion engine combustors and industrial combustors.
Abstract
Combustion dynamics impact the design of both conventional diffusion e ame gas turbine combustors and lean premixed combustion systems. The occurrence of dynamics in diffusion e ame combustors can generally be eliminated through changes to the fueling system or operating characteristics driven primarily through empirical design know-how. Lean premixed combustors, such as industrial aeroderivative dry low-emissions combustors, have more persistent dynamics problems that are only partially ameliorated with application of empirical tools and controls. With continuing emphasis on reducing emissions and cost and increasing performance of turbopropulsion engine combustors, the design direction of e ight engines is approaching the lean premixed limit; thus, there is a need for improved tools and control strategies for combustion dynamics in these applications as well. The components of a combined analytical, experimental, and computational approach to understanding and controlling combustion dynamics are being developed. With successful implementation of such an analytical and control mechanism, further improvements in the emissions, stability, and durability characteristics of both e ight and industrial combustors will become possible.

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Citations
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Journal ArticleDOI

Dynamics and stability of lean-premixed swirl-stabilized combustion

TL;DR: A comprehensive review of the advances made over the past two decades in this area is provided in this article, where various swirl injector configurations and related flow characteristics, including vortex breakdown, precessing vortex core, large-scale coherent structures, and liquid fuel atomization and spray formation are discussed.
Journal ArticleDOI

Turbulent premixed combustion: Flamelet structure and its effect on turbulent burning velocities

TL;DR: In this article, the authors used direct numerical simulation (DNS) to predict the flamelet structure and the burning velocity of premixed turbulent combustion and showed that the results were valid even for highly turbulent flames.
Journal ArticleDOI

Feedback control of combustion oscillations

TL;DR: Early work and recent advances in feedback control of combustion oscillations are described in this paper, where the concept of using feedback control to interrupt these interactions is introduced, and factors affecting practical implementation of feedback control, including sensors, actuators, and controller design are described.

Unsteady Motions in Combustion Chambers for Propulsion Systems

TL;DR: The main mechanisms for combustion instabilities in liquid and solid fueled rockets, ramjets, thrust augmentors, and gas turbines are discussed in this paper, with a broad summary of the basic material required to understand the subject.
Journal ArticleDOI

Detailed characterization of the dynamics of thermoacoustic pulsations in a lean premixed swirl flame

TL;DR: In this paper, a spray configuration for premixed gas turbine flames was operated with CH4 and air at atmospheric pressure, and a flame with P = 25 ǫkW thermal power and an equivalence ratio of Φ = 0.7 was chosen as a target flame in order to analyze the dynamics and the feedback mechanism of the periodic instability in detail.
References
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Journal ArticleDOI

Modeling Premixed Combustion-Acoustic Wave Interactions: A Review

TL;DR: In this article, the mutual interaction mechanisms between the combustion process and acoustic, vorticity, and entropy waves are described and a tutorial review is provided of current understanding of these interactions.
Journal ArticleDOI

Structure and Control of Thermoacoustic Instabilities in a Gas-turbine Combustor

TL;DR: In this article, a closed loop active control system was employed to suppress the thermoacoustic pressure oscillations and to reduce NO x emissions in an experimental low-emission swirl stabilized combustor, where the acoustic boundary conditions were modified to obtain combustion instability.
Journal ArticleDOI

Development of an Aeroderivative Gas Turbine Dry Low Emissions Combustion System

TL;DR: The development status of GE's new aeroderivative premixed combustion system is given in this paper. But the development status is not discussed in this paper, nor the development of the fuel delivery system.
Proceedings ArticleDOI

Dry Low Emissions Combustor Development

TL;DR: In the dry low emissions (DLE) technology as discussed by the authors, the combustor operates on the mid dome at light-off, the inner and the outer domes are brought on progressively, as the engine is loaded.
Proceedings ArticleDOI

Development of a Fuel Air Premixer for Aero-Derivative Dry Low Emissions Combustors

TL;DR: In this paper, an experimental program was conducted to develop premixer concepts for use in GE's aero-derivative Marine and Industrial gas turbine engines such as the LM 1600, 2500 and 6000.
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