|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/723 ; 60/039.12 ; 431/07 ; 431/353|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 20 인용 특허 : 9|
A burner, particularly for a gas turbine, includes a catalytic combustion chamber and a performer/reformer (24). The combustion chamber has an essentially cylindrical extent in a flow direction of a fuel and a catalytically active coating (12) on a wall facing the fuel for oxidation of the fuel. A particularly low nitrogen oxide content of burner exhaust gas is achieved as a result of the catalytically induced combustion of the fuel. At the same time, in contrast to known primary measures for nitrogen oxide abatement, the flow resistance in the burner is...
[ We claim:] [1.] A burner, comprising:a catalytic preforming stage for conducting a flow of a fuel partstream therethrough and for at least partly breaking down the fuel partstream into substances igniting readily; anda catalytic, continuous combustion chamber for receiving a fuel including a main fuel stream, the preformed fuel partstream and air, the preformed fuel partstream being fed directly into said catalytic combustion chamber, said combustion chamber having a substantially cylindrical wall extending in an axial flow direction of the fuel, said ...