Patent · US Active

Corrosion mitigation for gearbox

US10883178B2 · kind B2 · utility

0Cited by
16References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 17, 2018
Grant dateJan 5, 2021
Priority date
Expiry dateJan 1, 2039

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.