Patent · US Active

Corrosion mitigation for gearbox

US10077499B2 · kind B2 · utility

4Cited by
14References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 6, 2013
Grant dateSep 18, 2018
Priority date
Expiry dateNov 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.