|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/39320 ; 60/39360 ; 60/760|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 2 인용 특허 : 3|
Unequal flow rates of dilution air about an annular combustor and the resulting hot spots and thermal stresses are avoided in a structure wherein a vane assembly (66) made up of ring (76) and integral vanes (76) is mounted to the rear turbine shroud (42) for limited movement with respect thereto sufficient to accommodate unequal thermal growth of the rear turbine shroud (42) and the vane assembly (66).
A gas turbine comprising: a rotor including a turbine wheel journaled for rotation about an axis; an annular nozzle radially outward of an surrounding said turbine wheel for directing gases inwardly at said turbine wheel; an annular shroud extending from said nozzle about the periphery of said turbine wheel to contain gases from said nozzle against said turbine wheel; an annular combustor about said axis and having an outlet connected to said nozzle; a cooling air plenum for directing cooling air about the combustor and including an annular section betwe...