|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3917 ; 60/39182|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 35 인용 특허 : 3|
In a gas turbine group which consists essentially of a compressor (2), a first combustion chamber (3), a first turbine (4), a second combustion chamber (5) and a second turbine (6), the first combustion chamber (3) is configured as an annular combustion chamber. This annular combustion chamber (3) is operated by a number of premixing burners (11) which are distributed at the periphery. The first turbine (4) is designed in such a way that its exhaust gases have a temperature level which is above the self-ignition temperature of the fuel (13) used in the s...
A gas turbine group, comprising: at least one compressor unit; a first combustion chamber for generating working gas, the first combustion chamber connected to receive compressed air from the compressor unit, the first combustion chamber being an annular combustion chamber having a plurality of premixing burners; a first turbine connected to received working gas from the first combustion chamber; a second turbine; a second combustion chamber connected to receive exhausted working gas from the first turbine and deliver working gas to the second turbine, t...