|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3936 ; 60/760|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 9 인용 특허 : 0|
The expense of fabricating an annular combustor (10) for a gas turbine is minimized by providing a combustor housing (12) including a generally axially extending sleeve (14) and an annular liner (18) disposed within the housing (12) and about the sleeve (14). The annular liner (18) has concentric inner and outer axially extending walls (20, 22) spaced from the sleeve (14 ) and the housing (12), respectively, and also has a radially extending wall (24) spaced from the housing (12 ) and interconnecting the inner and outer walls (20, 22) at one end to defin...
An annular combustor for a gas turbine, comprising: a combustor housing including a generally axially extending sleeve having an axis; an annular liner disposed within said housing and about said sleeve and having generally concentric inner and outer axially elongated walls, said inner and outer walls of said liner being spaced from said sleeve and said housing, respectively, said liner also having a generally radially extending wall spaced from said housing and interconnecting said inner and outer walls at one end to define a combustion chamber; said li...