|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3953 ; 60/728|
|우선권정보||JP-0067525 (1984-04-06); JP-0067526 (1984-04-06)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 4 인용 특허 : 4|
A gas turbine is disclosed, in which a portion of compressed air from a compressor of the turbine is cooled by water and the cooled compressed air is utilized for cooling a region at or about the turbine inlet, and in which the interior of a combustor chamber into which the compressed air from the compressor is introduced is divided by a partition wall into a combustor part and a transition piece part and air cooling pipes are provided through the partition wall, each air cooling pipe being provided with nozzles through which to jet water to positively a...
A gas turbine comprising a compressor, a turbine, a turbine rotor, a plurality of combustors radially arranged around said rotor in a combustion chamber encased by a turbine casing, wherein each of said combustion chambers is internally divided along its longitudinal length by a partition wall disposed radially on a boundary between a combustor part and a transition piece part of each of said combustors so as to form a cooling air chamber axially disposed on the side of said transition piece part, said partition wall being provided therethrough with a nu...