Liner cooling construction for gas turbine combustor or the like
US4790140A · kind A · utility
10Cited by
6References
1Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Oct 29, 1987 |
| Grant date | Dec 13, 1988 |
| Priority date | — |
| Expiry date | Oct 29, 2007 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R3/002
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A liner cooling construction for a gas turbine combustor or the like in which twisted or helical tapes in the spaces defined between the liner walls and the partition walls cause the cooling air to swirl so that the efficient cooling of the liner walls can be ensured.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.