Invention Grant
- Patent Title: Method for compacting an anti-corrosive paint of a turbine engine part
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Application No.: US17771738Application Date: 2020-10-27
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Publication No.: US12083555B2Publication Date: 2024-09-10
- Inventor: Anthony Cyrille Grunenwald , Romaric Jean-Marie Piette
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: CHRISTENSEN O'CONNOR JOHNSON KINDNESS PLLC
- Priority: FR 12298 2019.10.31
- International Application: PCT/FR2020/051943 2020.10.27
- International Announcement: WO2021/084202A 2021.05.06
- Date entered country: 2022-04-25
- Main IPC: B05D3/06
- IPC: B05D3/06 ; B05D1/02 ; B05D5/12 ; B05D7/14 ; F02C7/36

Abstract:
A method compacts an anti-corrosive paint having metal particles of a mechanical part such as a turbine engine part. The mechanical part extends along a longitudinal axis X and has a radially outer surface covered with a first layer of anti-corrosive paint. The method includes at least one step of generating a laser beam on the first layer of anti-corrosive paint to bring the metal particles into contact and to render the anti-corrosive paint electrically conductive.
Public/Granted literature
- US20220410208A1 METHOD FOR COMPACTING AN ANTI-CORROSIVE PAINT OF A TURBINE ENGINE PART Public/Granted day:2022-12-29
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