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CPC Main Group Additional Only
F23R 2900/00

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

25 direct subcodes

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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