|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/777; 060/723; 431/007|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 46 인용 특허 : 70|
The present additional control strategy has been developed to allow the gas turbine to operate at lower load or at other conditions where the total fuel required by the gas turbine is not optimum for full combustion of the fuel. The present invention manages air that bypasses the catalytic combustor and air that bleeds off of the compressor discharge. The bypass system changes the fuel air ratio of the catalytic combustor without affecting the overall gas turbine power output. The bleed system also changes the fuel air ratio of the catalytic combustor bu...
1. A method of controlling a catalytic combustion system comprising an air supply, a flame burner, a fuel injector positioned downstream of the flame burner and a catalyst positioned downstream of the fuel injector, a flow path containing a valve that directs a portion of the airflow to bypass the catalyst, wherein a portion of the fuel combusts within the catalyst and a remainder of the fuel combusts in the region downstream of the catalyst, comprising:determining the adiabatic combustion temperature at the catalyst inlet;measuring a load on a turbine d...