IP Library › Granted Patent US 12,247,491
Granted Patent B2
US 12,247,491 · App. 17/630,031 · Granted Mar 11, 2025

Abradable coating

Inventors: Guillaume Fradet (Moissy-Cramayel, FR); Laurent Paul Dudon (Moissy-Cramayel, FR); Serge Georges Vladimir Selezneff (Moissy-Cramayel, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
F01D11/122C23C4/04C23C4/129F05D2230/311F05D2300/611
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Quick Facts
Patent No.
US 12,247,491
App. No.
17/630,031
Granted
Mar 11, 2025
Kind
B2
Abstract

An abradable coating for a turbomachine, as well as a turbomachine module and a turbomachine including such an abradable coating, the abradable coating including, with a content of greater than 50% by volume, an inorganic compound whose Mohs hardness is less than 6 and whose melting temperature is greater than 900° C.

Claims (32)

1. An abradable track suitable for a turbomachine, the abradable track comprising:

a substrate; and

abradable coating, provided on the substrate;

wherein the abradable coating comprises, in a content of greater than 95 vol. %, Ca 10 (PO 4 ) 6 (OH) 2 , LaPO 4 , or diatomaceous earth, and

wherein the abradable coating has a surface roughness Ra of less than 3 μm.

2. The abradable track of claim 1 , wherein the abradable coating has a porosity of less than 15%.

3. The abradable track of claim 1 , wherein the abradable coating further comprises a metal compound.

4. The abradable track of claim 3 , wherein the metal compound is based on nickel, cobalt, or iron.

5. The abradable track of claim 3 , wherein the metal compound is NiAl.

6. The abradable track of claim 3 , wherein the Ca 10 (PO 4 ) 6 (OH) 2 and the metal compound together constitute at least 99 vol. % of total abradable coating material.

7. A turbomachine module, comprising:

a rotor, provided with a plurality of moving blades;

a stator; and

the abradable track of claim 1 , provided at the interface between a portion of the rotor and a portion of the stator.

8. A turbomachine, comprising:

a module of claim 7 .

9. A process for manufacturing the abradable track of claim 1 , the process comprising:

depositing the Ca 10 (PO 4 ) 6 (OH) 2 , LaPO 4 , or diatomaceous earth by thermal spraying from a powder having a particle size in a range of from 45 to 90 μm; and

surface machining the abradable coating.

10. The abradable track of claim 1 , wherein the abradable coating further comprises NiCrAl.

11. The abradable track of claim 1 , wherein the abradable coating further comprises CoNiCrAlY.

12. The abradable track of claim 1 , wherein the abradable coating further comprises FeCrAlY.

13. The abradable track of claim 1 , wherein the abradable coating comprises the LaPO 4 .

14. The abradable track of claim 1 , wherein the abradable coating comprises the diatomaceous earth.

15. The abradable track of claim 1 , wherein the Ca 10 (PO 4 ) 6 (OH) 2 is at least 99 vol. % of the abradable coating.

16. The abradable track of claim 1 , wherein the abradable coating consists of the Ca 10 (PO 4 ) 6 (OH) 2 and possible impurities.

17. The abradable track of claim 1 , wherein the LaPO 4 is at least 99 vol. % of the abradable coating.

18. The abradable track of claim 1 , wherein the abradable coating consists of the LaPO 4 and possible impurities.

19. The abradable track of claim 1 , wherein the diatomaceous earth is at least 99 vol. % of the abradable coating.

20. The abradable track of claim 1 , wherein the abradable coating consists of the diatomaceous earth and possible impurities.

21. The abradable track of claim 1 , wherein the abradable coating has a porosity of less than 15%, and

wherein the Ca 10 (PO 4 ) 6 (OH) 2 is greater than 95 vol. % of the abradable coating.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 25, 2022
From: FRADET, GUILLAUME; DUDON, LAURENT PAUL; SELEZNEFF, SERGE GEORGES VLADIMIR
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 059809/0954 →
Priority Claims (1)
FR 19 08492 · Jul 26, 2019 · national
Continuity (1)
Related Publication 20220282633A1 · Sep 8, 2022
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