EP4194675 - METHOD AND SYSTEM FOR DETERMINING AIRCRAFT ENGINE INLET TOTAL PRESSURE [Right-click to bookmark this link] | Status | The patent has been granted Status updated on 14.06.2024 Database last updated on 13.11.2024 | |
Former | Grant of patent is intended Status updated on 06.02.2024 | ||
Former | Request for examination was made Status updated on 29.09.2023 | ||
Former | The application has been published Status updated on 12.05.2023 | Most recent event Tooltip | 14.06.2024 | (Expected) grant | published on 17.07.2024 [2024/29] | Applicant(s) | For all designated states PRATT & WHITNEY CANADA CORP. 1000 Marie Victorin, (01BE5) Longueuil, Québec J4G 1A1 / CA | [2023/24] | Inventor(s) | 01 /
CLOUTIER, Yves St-Bruno-de-Montaville / US | [2023/24] | Representative(s) | Dehns 10 Old Bailey London EC4M 7NG / GB | [N/P] |
Former [2023/24] | Dehns St. Bride's House 10 Salisbury Square London EC4Y 8JD / GB | Application number, filing date | 22211920.8 | 07.12.2022 | [2023/24] | Priority number, date | US202117643072 | 07.12.2021 Original published format: US202117643072 | [2023/24] | Filing language | EN | Procedural language | EN | Publication | Type: | A1 Application with search report | No.: | EP4194675 | Date: | 14.06.2023 | Language: | EN | [2023/24] | Type: | B1 Patent specification | No.: | EP4194675 | Date: | 17.07.2024 | Language: | EN | [2024/29] | Search report(s) | (Supplementary) European search report - dispatched on: | EP | 08.05.2023 | Classification | IPC: | F02C9/00, F02C9/28 | [2023/24] | CPC: |
F02C9/00 (EP,US);
F02C9/28 (EP);
F05D2220/323 (US);
F05D2260/821 (EP);
F05D2270/3011 (EP,US)
| 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, ME, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR [2023/44] |
Former [2023/24] | 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, ME, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR | Title | German: | VERFAHREN UND SYSTEM ZUR BESTIMMUNG DES GESAMTDRUCKS EINES FLUGZEUGMOTOREINLASSES | [2023/24] | English: | METHOD AND SYSTEM FOR DETERMINING AIRCRAFT ENGINE INLET TOTAL PRESSURE | [2023/24] | French: | PROCÉDÉ ET SYSTÈME DE DÉTERMINATION DE LA PRESSION TOTALE D'ENTRÉE D'UN MOTEUR D'AÉRONEF | [2023/24] | Examination procedure | 28.09.2023 | Examination requested [2023/44] | 28.09.2023 | Date on which the examining division has become responsible | 07.02.2024 | Communication of intention to grant the patent | 07.06.2024 | Fee for grant paid | 07.06.2024 | Fee for publishing/printing paid | 07.06.2024 | Receipt of the translation of the claim(s) |
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Responsibility for the accuracy, completeness or quality of the data displayed under the link provided lies entirely with the Unified Patent Court. | Documents cited: | Search | [A]GB2355046 (HONDA MOTOR CO LTD [JP]); | [A]US2011208400 (LICKFOLD RAY D [US], et al); | [A]US2015330310 (DEGARIBODY JOHN RUSSELL [US]) |