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Part Load Operation of a Piloted FLOXآ® Combustion System
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A large operational envelope is a key requirement for modern gas turbines. Fuel staging is used here to improve the part load performance of an enhanced FLOXآ® type combustor. A swirlstabilized pilot stage is integrated ...
Generative Design of a Gas Turbine Combustor Using Invertible Neural Networks
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The need to burn 100% H2 in high efficient gas turbines featuring low NOx combustion in premix mode requires the complete redesign of the combustion system to ensure stable operation without any flashback. Since all engine ...
Comparison of Nonlinear to Linear Thermoacoustic Stability Analysis of a Gas Turbine Combustion System
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Gas turbines offer a high operational flexibility and a good turn down ratio to meet future requirements of power production. In this context, stable operation over a wide range and for different blends of fuel is requested. ...
Assessment of a Gas Turbine NOx Reduction Potential Based on a Spatiotemporal Unmixedness Parameter
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The paper presents a onedimensional approach to assess the reduction potential of NOx emissions for lean premixed gas turbine combustion systems. NOx emissions from these systems are known to be mainly caused by high ...