Corrosion mitigation for gearbox
US10077499B2 · kind B2 · utility
4Cited by
14References
12Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 6, 2013 |
| Grant date | Sep 18, 2018 |
| Priority date | — |
| Expiry date | Nov 14, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T428/24479
- WIPO fieldSurface technology, coating
- WIPO sectorChemistry
Abstract
A magnesium component of a rotary wing aircraft is provided including a groove including a first sidewall and a second sidewall arranged on opposing sides of a recessed opening. The first sidewall includes a deposit positioned adjacent the recessed opening. The deposit is formed by cold spraying one or more layers or powdered material within an area of the first sidewall from which material was removed.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.