|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3917 ; 60/3929 ; 60/39511|
|발명자 / 주소|
|인용정보||피인용 횟수 : 89 인용 특허 : 4|
A gas turbine system with integrated high and low pressure circuits having a power transmission for extracting work from one of the circuits, the volume of air and fuel to the respective circuits being varied according to the power demand monitored by a microprocessor, wherein the turbine system has a low pressure compressor and a staged high pressure compressor with a combustion chamber and high pressure turbine associated with the high pressure compressor, and, a combustion chamber and a low pressure turbine associated with the low pressure compressor,...
A gas turbine assembly with integrated high and low pressure circuits comprising: a low pressure air compressor and a high pressure air compressor staged with the low pressure air compressor; a first high pressure combustion chamber and associated two-stage, high pressure turbine communicating with the high pressure combustion chamber, the two-stage high pressure turbine having a first stage coupled to the high pressure air compressor and a second stage coupled to the low pressure air compressor; a second low pressure combustion chamber and associated lo...