Surfacing of additively manufactured components and corresponding manufactured components of a turbomachine
US9862059B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Sep 1, 2015 |
| Grant date | Jan 9, 2018 |
| Priority date | — |
| Expiry date | Sep 1, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldMaterials, metallurgy
- WIPO sectorChemistry
Abstract
The present invention relates to a method for manufacturing components, in particular components of turbomachines, such as aircraft engines, wherein an additive method is used at least partially for the manufacture of the component (1), wherein at least one surface region (3) of the additively manufactured portion of the component (1) is provided with a smoothing layer (2), which is deposited by vapor deposition. In addition, the invention relates to a correspondingly manufactured component of a turbomachine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.