Three dimensional airfoil micro-core cooling chamber
US10280761B2 · kind B2 · utility
0Cited by
11References
15Claims
0Family size
Assignee
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Key dates
| Filing date | Oct 1, 2015 |
| Grant date | May 7, 2019 |
| Priority date | — |
| Expiry date | Jan 16, 2038 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A component for use in a gas turbine engine comprises a body and a micro-core cooling circuit embedded within the body. The micro-core circuit has a variation in either the thickness or contoured surface, away from a generally planar shape to a non-planar shape.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.