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Extract from the Register of European Patents

EP About this file: EP3995682

EP3995682 - METHOD FOR CONTROLLING A DRIVE SYSTEM OF A ROTORCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINES [Right-click to bookmark this link]
StatusThe patent has been granted
Status updated on  27.10.2023
Database last updated on 02.07.2024
FormerGrant of patent is intended
Status updated on  12.07.2023
FormerRequest for examination was made
Status updated on  27.05.2022
FormerThe application has been published
Status updated on  08.04.2022
Most recent event   Tooltip31.05.2024Lapse of the patent in a contracting state
New state(s): ES, HR, LV, NL, NO, PL, RS, SE
published on 03.07.2024  [2024/27]
Applicant(s)For all designated states
Airbus Helicopters
Aéroport International Marseille Provence
13725 Marignane Cedex / FR
[2022/19]
Inventor(s)01 / COSSETTI, Luca
13980 ALLEINS / FR
02 / MALBURET, François
13111 COUDOUX / FR
 [2022/19]
Representative(s)GPI Brevets
1330, rue Guillibert de la Lauzière
EuroParc de Pichaury
Bât B2
13856 Aix en Provence Cedex 3 / FR
[2022/19]
Application number, filing date21204841.726.10.2021
[2022/19]
Priority number, dateFR2020001129904.11.2020         Original published format: FR 2011299
[2022/19]
Filing languageFR
Procedural languageFR
PublicationType: A1 Application with search report 
No.:EP3995682
Date:11.05.2022
Language:FR
[2022/19]
Type: B1 Patent specification 
No.:EP3995682
Date:29.11.2023
Language:FR
[2023/48]
Search report(s)(Supplementary) European search report - dispatched on:EP30.03.2022
ClassificationIPC:F02C9/42, F02K5/00, F02C6/02
[2022/19]
CPC:
F02C9/42 (EP); B64D31/00 (US); B64C27/00 (US);
B64D27/10 (US); B64D27/24 (US); B64D37/005 (US);
F02C6/02 (EP); F02C7/22 (US); F02K5/00 (EP);
F05D2220/329 (EP,US); F05D2220/76 (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 [2022/26]
Former [2022/19]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 
TitleGerman:VERFAHREN ZUR STEUERUNG EINER TRIEBWERKSANLAGE EINES DREHFLÜGELFLUGZEUGS, DIE MINDESTENS ZWEI TURBOTRIEBWERKE UMFASST[2022/19]
English:METHOD FOR CONTROLLING A DRIVE SYSTEM OF A ROTORCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINES[2022/19]
French:PROCÉDÉ DE PILOTAGE D'UNE INSTALLATION MOTRICE D'UN GIRAVION COMPRENANT AU MOINS DEUX TURBOMOTEURS[2023/30]
Former [2022/19]PROCEDE DE PILOTAGE D'UNE INSTALLATION MOTRICE D'UN GIRAVION COMPRENANT AU MOINS DEUX TURBOMOTEURS
Examination procedure23.05.2022Amendment by applicant (claims and/or description)
23.05.2022Examination requested  [2022/26]
23.05.2022Date on which the examining division has become responsible
13.07.2023Communication of intention to grant the patent
05.10.2023Fee for grant paid
05.10.2023Fee for publishing/printing paid
05.10.2023Receipt of the translation of the claim(s)
Fees paidRenewal fee
25.10.2023Renewal 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.
Lapses during opposition  TooltipES29.11.2023
HR29.11.2023
LT29.11.2023
LV29.11.2023
NL29.11.2023
PL29.11.2023
RS29.11.2023
SE29.11.2023
BG29.02.2024
NO29.02.2024
GR01.03.2024
IS29.03.2024
[2024/27]
Former [2024/21]LT29.11.2023
BG29.02.2024
GR01.03.2024
IS29.03.2024
Former [2024/20]GR01.03.2024
IS29.03.2024
Documents cited:Search[AD]EP1990519  (PRATT & WHITNEY CANADA [CA]) [AD] 1 * figure 1 *;
 [XDAI]EP2602458  (PRATT & WHITNEY CANADA [CA]) [XD] 1-3,6,7,9 * figure 2 * * paragraph [0018] * [A] 5 [I] 4,8;
 [AD]WO2015145036  (TURBOMECA [FR]) [AD] 1* figure 1 *;
 [AD]EP3415436  (GEN ELECTRIC [US]) [AD] 1 * figure 6 *
by applicantEP1990519
 EP2602458
 WO2015052413
 WO2015145036
 FR3024707
 US2016333782
 EP3415436
 EP3783211
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.