Abstract: There is provided a nozzle ring for a turbine of a turbocharger. The nozzle ring comprises: a nozzle dividing wall, at least on nozzle vane, and a circumferentially extending outer rim. The nozzle dividing wall extends generally perpendicular to a longitudinal axis of the nozzle ring. The at least one nozzle vane extends from the nozzle dividing wall and has a leading edge defining a first radius relative to the longitudinal axis. The circumferentially extending outer rim defines a second radius relative to the longitudinal axis. The ratio of the second radius to the first radius is at least around 1.05.
| # | Name | Date |
|---|---|---|
| 1 | 202417039988-TRANSLATIOIN OF PRIOIRTY DOCUMENTS ETC. [22-05-2024(online)].pdf | 2024-05-22 |
| 2 | 202417039988-STATEMENT OF UNDERTAKING (FORM 3) [22-05-2024(online)].pdf | 2024-05-22 |
| 3 | 202417039988-NOTIFICATION OF INT. APPLN. NO. & FILING DATE (PCT-RO-105-PCT Pamphlet) [22-05-2024(online)].pdf | 2024-05-22 |
| 4 | 202417039988-FORM 1 [22-05-2024(online)].pdf | 2024-05-22 |
| 5 | 202417039988-DRAWINGS [22-05-2024(online)].pdf | 2024-05-22 |
| 6 | 202417039988-DECLARATION OF INVENTORSHIP (FORM 5) [22-05-2024(online)].pdf | 2024-05-22 |
| 7 | 202417039988-COMPLETE SPECIFICATION [22-05-2024(online)].pdf | 2024-05-22 |
| 8 | 202417039988-FORM-26 [06-06-2024(online)].pdf | 2024-06-06 |
| 9 | 202417039988-FORM 18 [13-06-2024(online)].pdf | 2024-06-13 |
| 10 | 202417039988-Proof of Right [26-07-2024(online)].pdf | 2024-07-26 |
| 11 | 202417039988-FORM 3 [18-11-2024(online)].pdf | 2024-11-18 |
| 12 | 202417039988-Response to office action [26-07-2025(online)].pdf | 2025-07-26 |