Abstract: Disclosed is a hybrid turbomachine (10), in particular for a rotary-wing aircraft, comprising a gas generator (13) having a first shaft (16), at least one electric machine (11) having a second shaft (17), and a rotating equipment (15) coupled to a third mechanical shaft (18). The hybrid turbomachine (10) further comprises a switching coupling means (20) configured to couple the third mechanical shaft (18) to the first mechanical shaft (16) or the second mechanical shaft (17), depending on the operating phases of the gas generator (13) and the electric machine (11).
| # | Name | Date |
|---|---|---|
| 1 | 202517128241-STATEMENT OF UNDERTAKING (FORM 3) [17-12-2025(online)].pdf | 2025-12-17 |
| 2 | 202517128241-REQUEST FOR EXAMINATION (FORM-18) [17-12-2025(online)].pdf | 2025-12-17 |
| 3 | 202517128241-PRIORITY DOCUMENTS [17-12-2025(online)].pdf | 2025-12-17 |
| 4 | 202517128241-POWER OF AUTHORITY [17-12-2025(online)].pdf | 2025-12-17 |
| 5 | 202517128241-NOTIFICATION OF INT. APPLN. NO. & FILING DATE (PCT-RO-105-PCT Pamphlet) [17-12-2025(online)].pdf | 2025-12-17 |
| 6 | 202517128241-FORM 18 [17-12-2025(online)].pdf | 2025-12-17 |
| 7 | 202517128241-FORM 1 [17-12-2025(online)].pdf | 2025-12-17 |
| 8 | 202517128241-DRAWINGS [17-12-2025(online)].pdf | 2025-12-17 |
| 9 | 202517128241-DECLARATION OF INVENTORSHIP (FORM 5) [17-12-2025(online)].pdf | 2025-12-17 |
| 10 | 202517128241-COMPLETE SPECIFICATION [17-12-2025(online)].pdf | 2025-12-17 |