Combustor liner for gas turbine engine
US4132066A · kind A · utility
39Cited by
4References
8Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Sep 23, 1977 |
| Grant date | Jan 2, 1979 |
| Priority date | — |
| Expiry date | Sep 23, 1997 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R3/06
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
This invention relates to an improvement of the cooling air flow distribution in proximity to the combustion and dilution air holes of a combustor liner fabricated from Finwall.RTM. material for a turbine type power plant.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.