Dead ended bulbed rib geometry for a gas turbine engine
US8562286B2 · kind B2 · utility
8Cited by
24References
17Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Apr 6, 2010 |
| Grant date | Oct 22, 2013 |
| Priority date | — |
| Expiry date | Feb 25, 2032 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2250/185
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A component within a gas turbine engine includes a dead ended rib which at least partially defines an internal cooling circuit flow path, the dead ended rib defines a bulbed rib profile.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.