|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3902 ; 60/3906 ; 60/737 ; 60/740|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 29 인용 특허 : 0|
A fixed geometry combustor for a gas turbine comprising at least one combustion chamber, a dilution chamber disposed downstream of said combustion chamber and in communication with said combustion chamber, at least one primary inspirator for introducing a fuel/air mixture into said combustion chamber in communication with said combustion chamber, and means for introducing dilution air into the dilution chamber.
A process for combustion of a fuel in a gas turbine combustor comprising: mixing a fuel and combustion air, forming a fuel/air mixture whereby the amount of combustion air is adjusted in response to a load on said gas turbine without employing any moving parts external to said gas turbine so as to maintain about a constant total amount of air flowing into said combustor; introducing said fuel/air mixture into at least one combustion chamber of a fixed geometry combustor; introducing a dilution air into a dilution chamber of said fixed geometry combustor ...