|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/39161 ; 60/39163 ; 415/2141 ; 416/241B|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 6 인용 특허 : 4|
In a gas generator of a gas turbine, the turbine is provided with more stages than aerodynamically necessary for reducing the turbine rotational speed. As a result thereof, the stresses of the turbine rotor are reduced, the latter can be made of ceramic material, and the turbine inlet temperature can be increased. In order to permit the compressor to continue to operate at optimum rotational speed, the compressor is coupled with the turbine by way of a transmission providing a speed-up. Owing to this arrangement, the thermal efficiency and therewith the ...
A gas turbine power plant, comprising a gas generator unit and power output means, said gas generator unit including: gas generator compressor means, combustion chamber means, gas generator turbine means drivingly coupled with the gas generator compressor means, said gas generator turbine means including at least two turbine stages with ceramic turbine blade parts, and gas generator transmission means drivingly connecting the gas generator turbine means to the compressor means independently of said power output means, said gas generator means exhibiting ...