| 发明名称 |
LINER STRUCTURE FOR A GAS TURBINE COMBUSTION CHAMBER |
| 摘要 |
A liner structure for use in a gas turbine combustion chamber includes two spaced liner walls (12) between which cooling air flows. The space between the liner walls is divided into a plurality of spaces (18) by a plurality of partitions (13). Each space (18) accommodates a twisted tape (14) which causes air flowing along the length of the space to swirl thereby improving in a cooling efficiency. |
| 申请公布号 |
DE3664681(D1) |
申请公布日期 |
1989.08.31 |
| 申请号 |
DE19863664681 |
申请日期 |
1986.04.16 |
| 申请人 |
ISHIKAWAJIMA-HARIMA JUKOGYO KABUSHIKI KAISHA |
发明人 |
SATO, YUKINORI;WATANABE, TAKESHI;NIKAI, ISAO 7-102 OKURAYAMA HEIM;WATANABE, KENJI |
| 分类号 |
F23R3/00;F23R3/04;F23R3/08;F23R3/44;(IPC1-7):F23R3/08 |
主分类号 |
F23R3/00 |
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