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Extract from the Register of European Patents

EP About this file: EP4285004

EP4285004 - STATOR RING FOR AN AIRCRAFT TURBINE ENGINE AND AIRCRAFT TURBINE ENGINE FITTED WITH SAME [Right-click to bookmark this link]
StatusRequest for examination was made
Status updated on  03.11.2023
Database last updated on 26.07.2024
FormerThe international publication has been made
Status updated on  05.08.2022
Formerunknown
Status updated on  02.03.2022
Most recent event   Tooltip29.03.2024Change: Validation statespublished on 01.05.2024  [2024/18]
29.03.2024Change - extension statespublished on 01.05.2024  [2024/18]
Applicant(s)For all designated states
SAFRAN AIRCRAFT ENGINES
2 Boulevard du Général Martial Valin
75015 Paris / FR
[2023/49]
Inventor(s)01 / MERLIN, Rémi
77550 MOISSY-CRAMAYEL / FR
02 / GUILMET, Damien Gérard Marcel Jacques
77550 MOISSY-CRAMAYEL / FR
03 / GOUSPY, Romain Mikel Erwan
77550 MOISSY-CRAMAYEL / FR
 [2023/49]
Representative(s)Gevers & Orès
Immeuble le Palatin 2
3 Cours du Triangle
CS 80165
92939 Paris La Défense Cedex / FR
[2023/49]
Application number, filing date22705435.024.01.2022
[2023/49]
WO2022FR50126
Priority number, dateFR2021000076427.01.2021         Original published format: FR 2100764
[2023/49]
Filing languageFR
Procedural languageFR
PublicationType: A1 Application with search report
No.:WO2022162299
Date:04.08.2022
Language:FR
[2022/31]
Type: A1 Application with search report 
No.:EP4285004
Date:06.12.2023
Language:FR
The application published by WIPO in one of the EPO official languages on 04.08.2022 takes the place of the publication of the European patent application.
[2023/49]
Search report(s)International search report - published on:EP04.08.2022
ClassificationIPC:F01D9/04, F04D29/54
[2023/49]
CPC:
F04D29/542 (EP); F01D9/041 (EP); F05D2230/53 (EP);
F05D2240/80 (EP); F05D2250/294 (EP); F05D2250/72 (EP);
F05D2250/75 (EP); Y02T50/60 (EP) (-)
Designated contracting statesAL,   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 [2023/49]
TitleGerman:STATORRING FÜR EIN FLUGZEUGTURBINENTRIEBWERK UND DAMIT AUSGESTATTETES FLUGZEUGTURBINENTRIEBWERK[2023/49]
English:STATOR RING FOR AN AIRCRAFT TURBINE ENGINE AND AIRCRAFT TURBINE ENGINE FITTED WITH SAME[2023/49]
French:REDRESSEUR POUR UNE TURBOMACHINE D'AÉRONEF, UNE TURBOMACHINE D'AÉRONEF EQUIPÉE D'UN TEL REDRESSEUR[2023/49]
Entry into regional phase10.08.2023National basic fee paid 
10.08.2023Designation fee(s) paid 
10.08.2023Examination fee paid 
Examination procedure10.08.2023Amendment by applicant (claims and/or description)
10.08.2023Examination requested  [2023/49]
10.08.2023Date on which the examining division has become responsible
Fees paidRenewal fee
23.01.2024Renewal fee patent year 03
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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.
Cited inInternational search[AD]FR2948737  (SNECMA [FR]) [AD] 1-9 * page 9, line 27 - page 11, line 22 * * figures 2, 3, 6d *;
 [AD]WO2011157956  (SNECMA [FR], et al) [AD] 1-9 * claims 1-15 * * figures 1-6 *;
 [AD]FR3085416  (SAFRAN AIRCRAFT ENGINES [FR]) [AD] 1-9 * page 6, line 22 - page 9, line 31 ** figures 2-4 *
by applicantFR2948737
 WO2011157956
 FR3085416
The EPO accepts no responsibility for the accuracy of data originating from other authorities; in particular, it does not guarantee that it is complete, up to date or fit for specific purposes.