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Extract from the Register of European Patents

EP About this file: EP4357249

EP4357249 - METHOD AND AIRCRAFT HAVING AT LEAST ONE COMBUSTION ENGINE AND A DRIVE SYSTEM HAVING AT LEAST TWO ELECTRIC MACHINES [Right-click to bookmark this link]
StatusRequest for examination was made
Status updated on  03.05.2024
Database last updated on 14.09.2024
FormerThe application has been published
Status updated on  22.03.2024
Most recent event   Tooltip13.09.2024Change - classificationpublished on 16.10.2024 [2024/42]
13.09.2024Change - classificationpublished on 16.10.2024 [2024/42]
Applicant(s)For all designated states
Airbus Helicopters
Aéroport International Marseille Provence
13725 Marignane Cedex / FR
[2024/17]
Inventor(s)01 / GAZZINO, Marc
13012 MARSEILLE / FR
 [2024/17]
Representative(s)GPI Brevets
1330, rue Guillibert de la Lauzière
EuroParc de Pichaury
Bât B2
13856 Aix en Provence Cedex 3 / FR
[2024/17]
Application number, filing date23194149.330.08.2023
[2024/17]
Priority number, dateFR2022001075018.10.2022         Original published format: FR 2210750
[2024/17]
Filing languageFR
Procedural languageFR
PublicationType: A1 Application with search report 
No.:EP4357249
Date:24.04.2024
Language:FR
[2024/17]
Search report(s)(Supplementary) European search report - dispatched on:EP12.02.2024
ClassificationIPC:B64D31/18, B64D35/023, B64D33/00, B64D27/10, B64D31/02, F02C7/262, F02C7/275, F02K5/00, // B64D27/04, B64C27/06, B64D35/08
[2024/42]
CPC:
B64D33/00 (EP); B64D27/02 (CN); F02C9/00 (US);
B64D27/10 (EP); B64D31/02 (EP); B64D31/18 (EP);
B64D35/023 (EP); F02C6/206 (US); F02C7/262 (EP);
F02C7/275 (EP); F02K5/00 (EP); H02P9/08 (US);
B64C27/06 (EP); B64D27/04 (EP); B64D35/08 (EP);
F05D2220/329 (EP); H02P2101/25 (US); H02P2101/30 (US) (-)
Former IPC [2024/17]B64D33/00, B64D27/10, B64D31/02, F02C7/268, F02C7/262, F02C7/275, F02K5/00, // B64D27/04, B64C27/06, B64D35/08, F02C6/20
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,   ME,   MK,   MT,   NL,   NO,   PL,   PT,   RO,   RS,   SE,   SI,   SK,   SM,   TR [2024/23]
Former [2024/17]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 
Extension statesBANot yet paid
Validation statesKHNot yet paid
MANot yet paid
MDNot yet paid
TNNot yet paid
TitleGerman:VERFAHREN UND FLUGZEUG MIT MINDESTENS EINEM VERBRENNUNGSMOTOR UND EINEM ANTRIEBSSYSTEM MIT MINDESTENS ZWEI ELEKTRISCHEN MASCHINEN[2024/17]
English:METHOD AND AIRCRAFT HAVING AT LEAST ONE COMBUSTION ENGINE AND A DRIVE SYSTEM HAVING AT LEAST TWO ELECTRIC MACHINES[2024/17]
French:PROCÉDÉ ET AÉRONEF MUNI D'AU MOINS UN MOTEUR À COMBUSTION ET D'UN SYSTÈME D'ENTRAINEMENT À AU MOINS DEUX MACHINES ÉLECTRIQUES[2024/17]
Examination procedure26.04.2024Examination requested  [2024/23]
26.04.2024Date on which the examining division has become responsible
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Documents cited:Search[A]EP2404775  (EUROCOPTER FRANCE [FR]);
 [A]EP3209563  (SAFRAN HELICOPTER ENGINES [FR]);
 [A]US2019264615  (HUSBAND STEPHEN M [GB], et al)
by applicantEP2404775
 FR2967133
 FR3019215
 EP3209563
 US2019264615
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.