|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-009/28 F02C-003/20 F02C-003/22 F23C-099/00 F23R-003/26 F23R-003/28|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 241|
A mixture of air and fuel is received into a reaction chamber of a gas turbine system. The fuel is oxidized in the reaction chamber, and a maximum temperature of the mixture in the reaction chamber is controlled to be substantially at or below an inlet temperature of a turbine of the gas turbine system. The oxidation of the fuel is initiated by raising the temperature of the mixture to or above an auto-ignition temperature of the fuel. In some cases, the reaction chamber may be provided without a fuel oxidation catalyst material.
1. A method of operating a gas turbine system, comprising: oxidizing a fuel of an air and fuel mixture in a reaction chamber, wherein a fuel oxidation catalyst material is not used during the oxidizing; andcontrolling a maximum temperature of the air and fuel mixture to be between an auto-ignition temperature of the fuel and 1300° C. by receiving a control flow comprising supplemental fuel through a plurality of ports located at a plurality of locations along a reaction chamber flow path in the reaction chamber, each of the plurality of ports being conne...