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Extract from the Register of European Patents

EP About this file: EP4107062

EP4107062 - COMPOSITE BLADE FOR A TURBINE ENGINE ROTOR [Right-click to bookmark this link]
StatusExamination is in progress
Status updated on  12.04.2024
Database last updated on 22.01.2025
FormerRequest for examination was made
Status updated on  25.11.2022
FormerThe international publication has been made
Status updated on  27.08.2021
Formerunknown
Status updated on  05.03.2021
Most recent event   Tooltip28.05.2024New entry: Reply to examination report 
Applicant(s)For all designated states
SAFRAN AIRCRAFT ENGINES
2 boulevard du Général Martial Valin
75015 Paris / FR
[2022/52]
Inventor(s)01 / COURTIER, Vivien Mickaël
Safran c/o Centre d'Excellence de la Propriété
Intellectuelle Rond-point René Ravaud, Réau
77550 MOISSY-CRAMAYEL / FR
02 / BINDER, Anthony
Safran c/o Centre d'Excellence Propriété
Intellectuelle Rond-point René Ravaud, Réau
77550 MOISSY-CRAMAYEL / FR
 [2022/52]
Representative(s)Gevers & Orès
Immeuble le Palatin 2
3 Cours du Triangle
CS 80165
92939 Paris La Défense Cedex / FR
[2022/52]
Application number, filing date21708061.312.02.2021
[2022/52]
WO2021FR50258
Priority number, dateFR2020000159318.02.2020         Original published format: FR 2001593
[2022/52]
Filing languageFR
Procedural languageFR
PublicationType: A1 Application with search report
No.:WO2021165604
Date:26.08.2021
Language:FR
[2021/34]
Type: A1 Application with search report 
No.:EP4107062
Date:28.12.2022
Language:FR
The application published by WIPO in one of the EPO official languages on 26.08.2021 takes the place of the publication of the European patent application.
[2022/52]
Search report(s)International search report - published on:EP26.08.2021
ClassificationIPC:B64C11/26, B64C27/473, B29D99/00, F01D5/28, F01D5/30
[2022/52]
CPC:
B64C11/26 (EP,US); B29C70/86 (EP); B29D99/0025 (EP);
B64C27/473 (EP,US); F01D5/282 (EP,US); F01D5/30 (US);
B64C2027/4736 (EP,US); F05D2220/323 (US); F05D2220/36 (EP);
F05D2230/20 (US); F05D2240/30 (US); F05D2300/6034 (US);
F05D2300/612 (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 [2022/52]
TitleGerman:VERBUNDSCHAUFEL FÜR EINEN TURBINENMOTORROTOR[2022/52]
English:COMPOSITE BLADE FOR A TURBINE ENGINE ROTOR[2022/52]
French:PALE COMPOSITE POUR ROTOR DE TURBOMACHINE[2022/52]
Entry into regional phase06.09.2022National basic fee paid 
06.09.2022Designation fee(s) paid 
06.09.2022Examination fee paid 
Examination procedure06.09.2022Amendment by applicant (claims and/or description)
06.09.2022Examination requested  [2022/52]
06.09.2022Date on which the examining division has become responsible
11.04.2024Despatch of a communication from the examining division (Time limit: M04)
28.05.2024Reply to a communication from the examining division
Fees paidRenewal fee
22.02.2023Renewal fee patent year 03
20.02.2024Renewal fee patent year 04
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Cited inInternational search[A]US3923421  (CARTER DONALD RICHARD, et al);
 [XI]EP0610273  (UNITED TECHNOLOGIES CORP [US]);
 [A]FR2954271  (SNECMA [FR]);
 [XI]EP2679487  (HAMILTON SUNDSTRAND CORP [US]);
ExaminationEP0610273
 EP2679487
by applicantUS3923421
 EP0610273
 FR2954271
 EP2679487
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.