|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/392 ; 60/3925 ; 415/160|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 1 인용 특허 : 1|
Thermal degradation of variable nozzle components in a gas turbine power plant is minimized by a construction including a radial outflow compressor 16 on a shaft 10 with a radial inflow turbine 18, combustion gas delivery path 78 which is generally concentric about the shaft 10, a compressed gas delivery path 40 from the compressor 16 to the turbine 18 which is parallel to the axial combustion gas path 78 and rotatably mounted guide vanes 80 located in the axial combustion path 78 which are provided with control elements 82 that extend through the compre...
A gas turbine power plant having in combination: a radial outflow compressor means and a radial inflow turbine means coupled for simultaneous rotation about an axis of rotation; means to deliver combustion gas from a combustor to said radial inflow turbine along an axial combustion gas path concentric to said axis of rotation; means to deliver compressed gas from said radial outflow compressor means to said combustor along with a compressed gas path parrallel to said axial combustion gas path; and rotatably mounted guide vane means positioned in said axi...