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EP4151838
European procedure
Extract from the Register of European Patents
EP About this file: EP4151838
| EP4151838 - AIRCRAFT ENGINE ASSEMBLY COMPRISING A THRUST LOAD-RECEIVING DEVICE CONFIGURED TO BE MOUNTED TO AN AIRCRAFT [Right-click to bookmark this link] | |||
| Former [2023/12] | AIRCRAFT DRIVE UNIT COMPRISING A THRUST LOAD-RECEIVING DEVICE | ||
| [2024/12] | Status | The patent has been granted Status updated on 05.07.2024 Database last updated on 21.03.2025 | |
| Former | Grant of patent is intended Status updated on 01.04.2024 | ||
| Former | Examination is in progress Status updated on 14.12.2022 | Most recent event Tooltip | 07.02.2025 | Lapse of the patent in a contracting state New state(s): ES, HR, RS | published on 12.03.2025 [2025/11] | Applicant(s) | For all designated states AIRBUS OPERATIONS (S.A.S.) 316, route de Bayonne 31060 Toulouse / FR | [2023/12] | Inventor(s) | 01 /
BERJOT, Michael 31060 TOULOUSE / FR | 02 /
ROBIGLIO, Thomas 31060 TOULOUSE / FR | 03 /
ARELLANES MENDOZA, Karla Mariana 31060 TOULOUSE / FR | [2023/12] | Representative(s) | Jardel, Marc Henry Philippe Airbus Operations S.A.S. M0101/1 - Intellectual Property Department 316, route de Bayonne 31060 Toulouse Cedex 09 / FR | [N/P] |
| Former [2023/12] | Jardel, Marc Henry Philippe Airbus Operations S.A.S. ETRT 316, route de Bayonne 31060 Toulouse Cedex 09 / FR | Application number, filing date | 22195787.1 | 15.09.2022 | [2023/12] | Priority number, date | FR20210009869 | 20.09.2021 Original published format: FR 2109869 | [2023/12] | Filing language | FR | Procedural language | FR | Publication | Type: | A1 Application with search report | No.: | EP4151838 | Date: | 22.03.2023 | Language: | FR | [2023/12] | Type: | B1 Patent specification | No.: | EP4151838 | Date: | 07.08.2024 | Language: | FR | [2024/32] | Search report(s) | (Supplementary) European search report - dispatched on: | EP | 14.11.2022 | Classification | IPC: | B64D27/40, F01D25/24 | [2024/12] | CPC: |
B64D27/406 (EP,US);
B64D27/40 (US);
B64D27/404 (EP);
F01D25/243 (EP);
F02C7/20 (US)
|
| Former IPC [2023/12] | F01D25/24, B64D27/26 | Designated contracting states | AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LI, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR [2023/44] |
| Former [2023/12] | AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LI, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR | Title | German: | FLUGTRIEBWERKSAUFBAU MIT EINER VORRICHTUNG ZUR AUFNAHME VON SCHUBKRÄFTEN GEEIGNET ZUR AUFHÄNGUNG AN EINEM FLUGZEUG | [2024/12] | English: | AIRCRAFT ENGINE ASSEMBLY COMPRISING A THRUST LOAD-RECEIVING DEVICE CONFIGURED TO BE MOUNTED TO AN AIRCRAFT | [2024/12] | French: | ENSEMBLE DE MOTORISATION D ́AÉRONEF COMPRENANT UN DISPOSITIF DE REPRISE D'EFFORTS DE POUSSÉE CONFIGURÉ POUR ÊTRE ATTACHÉ À UN AÉRONEF | [2024/12] |
| Former [2023/12] | MOTORISIERUNGSEINHEIT FÜR EIN FLUGZEUG MIT EINER VORRICHTUNG ZUR WIEDERHERSTELLUNG VON SCHUBKRÄFTEN | ||
| Former [2023/12] | AIRCRAFT DRIVE UNIT COMPRISING A THRUST LOAD-RECEIVING DEVICE | ||
| Former [2023/12] | ENSEMBLE DE MOTORISATION D AÉRONEF COMPRENANT UN DISPOSITIF DE REPRISE D'EFFORTS DE POUSSÉE | Examination procedure | 16.09.2022 | Examination requested [2023/12] | 14.11.2022 | Date on which the examining division has become responsible | 25.11.2022 | Despatch of a communication from the examining division (Time limit: M04) | 14.12.2022 | Reply to a communication from the examining division | 02.04.2024 | Communication of intention to grant the patent | 25.06.2024 | Fee for grant paid | 25.06.2024 | Fee for publishing/printing paid | 25.06.2024 | Receipt of the translation of the claim(s) |
| Opt-out from the exclusive Tooltip competence of the Unified Patent Court | See the Register of the Unified Patent Court for opt-out data | ||
| Responsibility for the accuracy, completeness or quality of the data displayed under the link provided lies entirely with the Unified Patent Court. | Lapses during opposition Tooltip | AT | 07.08.2024 | BG | 07.08.2024 | ES | 07.08.2024 | FI | 07.08.2024 | HR | 07.08.2024 | LV | 07.08.2024 | NL | 07.08.2024 | PL | 07.08.2024 | NO | 07.11.2024 | RS | 07.11.2024 | GR | 08.11.2024 | IS | 07.12.2024 | PT | 09.12.2024 | [2025/11] |
| Former [2025/09] | AT | 07.08.2024 | |
| BG | 07.08.2024 | ||
| FI | 07.08.2024 | ||
| LV | 07.08.2024 | ||
| NL | 07.08.2024 | ||
| PL | 07.08.2024 | ||
| NO | 07.11.2024 | ||
| GR | 08.11.2024 | ||
| IS | 07.12.2024 | ||
| PT | 09.12.2024 | ||
| Former [2025/08] | FI | 07.08.2024 | |
| NL | 07.08.2024 | ||
| PL | 07.08.2024 | ||
| NO | 07.11.2024 | ||
| GR | 08.11.2024 | ||
| PT | 09.12.2024 | Documents cited: | Search | [A]JP2004352232 (SNECMA MOTEURS); | [X]US7607609 (LEVERT STEPHANE [FR]); | [X]US10597144 (FOTOUHIE HADIE [US]) | by applicant | US7607609 | EP3792182 |