|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/39182 ; 60/3959 ; 60/3983|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 46 인용 특허 : 3|
A gas turbine is provided in which the quantity of cooling air required to cool the turbine is reduced by the evaporative cooling of air bled from the compressor discharge for cooling purposes. The evaporative cooling is accomplished by spraying pressurized water into a bleed pipe which diverts the cooling air from the compressor discharge to the turbine.
A gas turbine system comprising: (a) a compressor section for compressing air, (b) a combustion section connected to receive air from said compressor section and to produce hot compressed gas by burning fuel in said received compressed air, (c) a turbine section connected to receive gas from said combustion section and for expanding said heated compressed gas, (d) a chamber between said compressor section and said combustor section for collecting said compressed air, (e) communicating means for diverting some of said air in said chamber to said turbine, ...