|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3923 ; 60/748 ; 60/757|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 15 인용 특허 : 9|
A variable geometry combustor for use in a gas turbine propulsion engine.
Variable geometry combustor apparatus comprising: (a) a housing; (b) a combustion liner at least partially enveloped by said housing and defining therewith a plenum in said housing for receiving pressurized air from a source thereof, said liner having: (1) an upstream end wall positioned within said housing plenum, (2) an interior wall positioned downstream from said end wall, (3) a sidewall portion extending downstream from said end wall within said housing, said sidewall portion defining with said interior wall and said end wall an inlet plenum within ...