Abstract: Blade for a turbomachine, comprising an airfoil part (12) and a blade root (11), the blade root (11) comprising at least one bearing surface (22) configured to cooperate with a fastening device (31) of the turbomachine (1), wherein at least the blade root (11) is made of TiAl, and wherein the bearing surface (22) is provided with an anti-wear coating, this anti-wear coating being made of a nickel-based alloy comprising at least 9.5% by mass of Co and/or at least 14% by mass of Cr.
| # | Name | Date |
|---|---|---|
| 1 | 202517059417-STATEMENT OF UNDERTAKING (FORM 3) [20-06-2025(online)].pdf | 2025-06-20 |
| 2 | 202517059417-REQUEST FOR EXAMINATION (FORM-18) [20-06-2025(online)].pdf | 2025-06-20 |
| 3 | 202517059417-PRIORITY DOCUMENTS [20-06-2025(online)].pdf | 2025-06-20 |
| 4 | 202517059417-NOTIFICATION OF INT. APPLN. NO. & FILING DATE (PCT-RO-105-PCT Pamphlet) [20-06-2025(online)].pdf | 2025-06-20 |
| 5 | 202517059417-FORM 18 [20-06-2025(online)].pdf | 2025-06-20 |
| 6 | 202517059417-FORM 1 [20-06-2025(online)].pdf | 2025-06-20 |
| 7 | 202517059417-DRAWINGS [20-06-2025(online)].pdf | 2025-06-20 |
| 8 | 202517059417-DECLARATION OF INVENTORSHIP (FORM 5) [20-06-2025(online)].pdf | 2025-06-20 |
| 9 | 202517059417-COMPLETE SPECIFICATION [20-06-2025(online)].pdf | 2025-06-20 |
| 10 | 202517059417-FORM 3 [22-08-2025(online)].pdf | 2025-08-22 |
| 11 | 202517059417-FORM-26 [01-09-2025(online)].pdf | 2025-09-01 |
| 12 | 202517059417-FORM-26 [01-09-2025(online)]-1.pdf | 2025-09-01 |