F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 9/18 (2006.01) F02C 9/52 (2006.01) F23R 3/04 (2006.01) F23R 3/26 (2006.01)
Patent
CA 2451049
A method of operating a combustor (10) in a gas turbine that receives combustion air from a compressor (12) includes a) controlling combustion temperature as a function of compressor discharge air bled from the compressor (12) by determining a minimum amount of compressor discharge air required for maintaining a predetermined minimum combustion temperature; and b) bleeding compressor discharge air in excess of the minimum amount from the compressor via a control valve (30).
Méthode d'opération d'une chambre de combustion (10) de turbine à gaz qui reçoit de l'air de combustion d'un compresseur (12). Cela comprend : a) réguler la température de combustion en fonction de l'air de décharge prélevé du compresseur (12) en établissant la quantité minimale d'air de décharge du compresseur nécessaire pour conserver une température de combustion minimale prédéterminée et, b) prélever de l'air de décharge compresseur, au-delà de la quantité minimale, au moyen d'une vanne de commande (30).
Boettner Robert Edward
Elward Kevin Michael
Nichols Richard Lee
Norman Bruce G.
Pavri Roointon Erach
Company General Electric
Craig Wilson And Company
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