|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-007/12 F01D-025/12 F28F-003/12|
|미국특허분류(USC)||60/730 ; 415/176 ; 165/51 ; 165/169|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 24 인용 특허 : 0|
An improved structure is provided for liquid cooling a transition member which conducts hot motive gases from a combustor to a turbine inlet in a gas turbine power plant. The liquid-cooled structure includes a transition member body having a longitudinal inlet manifold and a longitudinal collection manifold attached to opposite sides of the body. The body has a plurality of internal laterally disposed passages which communicate liquid coolant from the inlet manifold, around the body to the collection manifold. The liquid coolant transfers heat from the m...
In a gas turbine including a combustion liner and a turbine, a transition member for conducting hot combustion gas from the combustion liner to an inlet passage of the turbine, said transition member comprising: a contoured body having an inlet end of circular cross-section conforming to the shape of the exit end of the combustion liner and an exit end of generally rectangular cross-section conforming to the shape of the turbine inlet passage; an inlet manifold having an inlet adjacent the inlet of said body adapted to receive liquid coolant, said inlet ...