Turbine airfoils with micro cooling features
US10876413B2 · kind B2 · utility
1Cited by
21References
19Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | May 21, 2019 |
| Grant date | Dec 29, 2020 |
| Priority date | — |
| Expiry date | May 21, 2039 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A blade used in a gas turbine engine includes a pair of pedestals and an airfoil coupled between the pedestals. The airfoil includes cooling features to cool the airfoil.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.