Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor

Child Classifications

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• F23R 2900/00001 Arrangements using bellows, e.g. to adjust volumes or reduce thermal stresses
• F23R 2900/00002 Gas turbine combustors adapted for fuels having low heating value [LHV]
• F23R 2900/00004 Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits
• F23R 2900/00005 Preventing fatigue failures or reducing mechanical stress in gas turbine components
• F23R 2900/00006 Using laser for starting or improving the combustion process
• F23R 2900/00008 Combustion techniques using plasma gas
• F23R 2900/00009 Using plasma torches for igniting, stabilizing, or improving the combustion process
• F23R 2900/00012 Details of sealing devices
• F23R 2900/00013 Reducing thermo-acoustic vibrations by active means
• F23R 2900/00014 Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
• F23R 2900/00015 Trapped vortex combustion chambers
• F23R 2900/00016 Retrofitting in general, e.g. to respect new regulations on pollution
• F23R 2900/00017 Assembling combustion chamber liners or subparts
• F23R 2900/00018 Manufacturing combustion chamber liners or subparts
• F23R 2900/00019 Repairing or maintaining combustion chamber liners or subparts
• F23R 2900/03041 Effusion cooled combustion chamber walls or domes
• F23R 2900/03042 Film cooled combustion chamber walls or domes
• F23R 2900/03043 Convection cooled combustion chamber walls with means for guiding the cooling air flow
• F23R 2900/03044 Impingement cooled combustion chamber walls or subassemblies
• F23R 2900/03045 Convection cooled combustion chamber walls provided with turbolators or means for creating turbulences to increase cooling
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