Process for complete cladding of metal parts of aircraft turbojets, and complete protection tool for implementing the process
US10610967B2 · kind B2 · utility
1Cited by
2References
15Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | May 23, 2013 |
| Grant date | Apr 7, 2020 |
| Priority date | — |
| Expiry date | May 23, 2033 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2230/234
- WIPO fieldMachine tools
- WIPO sectorMechanical engineering
Abstract
A process for cladding a metal part of an aircraft turbojet, including a plurality of metal portions, using a nozzle for emitting a laser beam, the process including positioning the metal part to be cladded on a turntable; positioning a cover on the turntable; positioning the nozzle in an aperture present in the cover; introducing an inert gas under the cover; and cladding a first portion of the metal part by carrying out operations of: spraying metal powders; emitting the laser beam; and moving the nozzle relative to the first metal portion.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.