Invention Grant
- Patent Title: Coating with property gradient for inner wall of turbomachine
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Application No.: US16770416Application Date: 2018-12-06
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Publication No.: US11111808B2Publication Date: 2021-09-07
- Inventor: Jacky Novi Mardjono , Arnaud Dubourg , Edith-Roland Fotsing , Annie Ross
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: CACA2988224 20171206,FR1761722 20171206
- International Application: PCT/FR2018/053128 WO 20181206
- International Announcement: WO2019/110934 WO 20190613
- Main IPC: F01D11/12
- IPC: F01D11/12 ; F01D25/24 ; B33Y80/00

Abstract:
A property gradient coating to be applied by additive manufacture to an inner wall of a casing mounted on the periphery of moving blades of a turbomachine rotor, the coating including in superimposed layers from an outer surface of the coating to this inner wall of the casing, on the one hand, a first layer consisting of a three-dimensional scaffolding of filaments of an abradable material forming an ordered network of channels or microchannels whose pore sizes are between 50 and 250 microns and whose porosity is greater than 85%, and, on the other hand, a second layer having a function of dissipating energy from acoustic waves striking the outer surface of the coating and consisting of a three-dimensional scaffolding of filaments of a first thermosetting material forming an ordered network of channels or microchannels whose pore sizes are between 50 and 400 microns and whose porosity is greater than 60%.
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