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Extract from the Register of European Patents

EP About this file: EP3653495

EP3653495 - METHOD FOR SECURING AN ACTUATOR FOR ROTATING AN AIRCRAFT WHEEL IN A DISENGAGED POSITION [Right-click to bookmark this link]
StatusNo opposition filed within time limit
Status updated on  03.11.2023
Database last updated on 19.07.2024
FormerThe patent has been granted
Status updated on  25.11.2022
FormerGrant of patent is intended
Status updated on  16.06.2022
FormerExamination is in progress
Status updated on  19.03.2021
FormerRequest for examination was made
Status updated on  13.11.2020
FormerThe application has been published
Status updated on  17.04.2020
Most recent event   Tooltip05.07.2024Lapse of the patent in a contracting state
New state(s): MC		published on 07.08.2024 [2024/32]
Applicant(s)For all designated states
Safran Landing Systems
7, rue Général Valérie André
Inovel Parc Sud
78140 Vélizy-Villacoublay / FR
[2020/21]
Inventor(s)01 / LIEGEOIS, Pierre-Yves
C/o Safran Landing Systems
CEPI
Site de Villaroche - Rond-point René Ravaud
77550 Moissy-Cramayel / FR
02 / THORAVAL, Bruno
C/o Safran Landing Systems
CEPI
Site de Villaroche - Rond-point René Ravaud
77550 Moissy-Cramayel / FR
 [2020/21]
Representative(s)Lavialle, Bruno François Stéphane, et al
Cabinet Boettcher
5 rue de Vienne
75008 Paris / FR
[N/P]
Former [2020/21]Lavialle, Bruno François Stéphane, et al
Cabinet Boettcher
16, rue Médéric
75017 Paris / FR
Application number, filing date19208576.912.11.2019
[2020/21]
Priority number, dateFR2018006050614.11.2018         Original published format: FR 1860506
[2020/21]
Filing languageFR
Procedural languageFR
PublicationType: A1 Application with search report 
No.:EP3653495
Date:20.05.2020
Language:FR
[2020/21]
Type: B1 Patent specification 
No.:EP3653495
Date:28.12.2022
Language:FR
[2022/52]
Search report(s)(Supplementary) European search report - dispatched on:EP14.04.2020
ClassificationIPC:B64C25/40, B64C25/34
[2020/21]
CPC:
B64C25/405 (EP); B64C25/34 (EP,CN); B64C25/26 (US);
B64C25/22 (US); F15B15/26 (US); F15B2015/268 (US);
F15B2211/72 (US); Y02T50/80 (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 [2020/51]
Former [2020/21]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:SICHERUNGSVERFAHREN EINES ANTRIEBSSTELLGLIEDS IN DER RADDREHUNG EINES LUFTFAHRZEUGS IN ENTKUPPELTER POSITION[2020/21]
English:METHOD FOR SECURING AN ACTUATOR FOR ROTATING AN AIRCRAFT WHEEL IN A DISENGAGED POSITION[2020/21]
French:PROCÉDÉ DE SÉCURISATION D'UN ACTIONNEUR D'ENTRAÎNEMENT EN ROTATION DE ROUE D'AÉRONEF DANS UNE POSITION DÉGAGÉE[2022/28]
Former [2020/21]PROCEDE DE SECURISATION D'UN ACTIONNEUR D'ENTRAINEMENT EN ROTATION DE ROUE D'AERONEF DANS UNE POSITION DEGAGEE
Examination procedure06.11.2020Amendment by applicant (claims and/or description)
06.11.2020Examination requested  [2020/51]
06.11.2020Date on which the examining division has become responsible
22.03.2021Despatch of a communication from the examining division (Time limit: M04)
20.07.2021Reply to a communication from the examining division
17.06.2022Communication of intention to grant the patent
13.10.2022Fee for grant paid
13.10.2022Fee for publishing/printing paid
13.10.2022Receipt of the translation of the claim(s)
Opposition(s)29.09.2023No opposition filed within time limit [2023/49]
Fees paidRenewal fee
18.11.2021Renewal fee patent year 03
22.11.2022Renewal fee patent year 04
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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  TooltipAL28.12.2022
AT28.12.2022
CZ28.12.2022
DK28.12.2022
EE28.12.2022
FI28.12.2022
HR28.12.2022
IT28.12.2022
LT28.12.2022
LV28.12.2022
MC28.12.2022
NL28.12.2022
PL28.12.2022
RO28.12.2022
RS28.12.2022
SE28.12.2022
SI28.12.2022
SK28.12.2022
SM28.12.2022
NO28.03.2023
GR29.03.2023
IS28.04.2023
PT28.04.2023
[2024/32]
Former [2024/26]AL28.12.2022
AT28.12.2022
CZ28.12.2022
DK28.12.2022
EE28.12.2022
FI28.12.2022
HR28.12.2022
IT28.12.2022
LT28.12.2022
LV28.12.2022
NL28.12.2022
PL28.12.2022
RO28.12.2022
RS28.12.2022
SE28.12.2022
SI28.12.2022
SK28.12.2022
SM28.12.2022
NO28.03.2023
GR29.03.2023
IS28.04.2023
PT28.04.2023
Former [2024/11]AL28.12.2022
AT28.12.2022
CZ28.12.2022
DK28.12.2022
EE28.12.2022
FI28.12.2022
HR28.12.2022
LT28.12.2022
LV28.12.2022
NL28.12.2022
PL28.12.2022
RO28.12.2022
RS28.12.2022
SE28.12.2022
SI28.12.2022
SK28.12.2022
SM28.12.2022
NO28.03.2023
GR29.03.2023
IS28.04.2023
PT28.04.2023
Former [2023/46]AL28.12.2022
AT28.12.2022
CZ28.12.2022
DK28.12.2022
EE28.12.2022
FI28.12.2022
HR28.12.2022
LT28.12.2022
LV28.12.2022
NL28.12.2022
PL28.12.2022
RO28.12.2022
RS28.12.2022
SE28.12.2022
SK28.12.2022
SM28.12.2022
NO28.03.2023
GR29.03.2023
IS28.04.2023
PT28.04.2023
Former [2023/39]AL28.12.2022
AT28.12.2022
CZ28.12.2022
EE28.12.2022
FI28.12.2022
HR28.12.2022
LT28.12.2022
LV28.12.2022
NL28.12.2022
PL28.12.2022
RO28.12.2022
RS28.12.2022
SE28.12.2022
SK28.12.2022
SM28.12.2022
NO28.03.2023
GR29.03.2023
IS28.04.2023
PT28.04.2023
Former [2023/38]AL28.12.2022
AT28.12.2022
CZ28.12.2022
EE28.12.2022
FI28.12.2022
HR28.12.2022
LT28.12.2022
LV28.12.2022
NL28.12.2022
PL28.12.2022
RO28.12.2022
RS28.12.2022
SE28.12.2022
SK28.12.2022
SM28.12.2022
NO28.03.2023
GR29.03.2023
PT28.04.2023
Former [2023/37]AL28.12.2022
AT28.12.2022
CZ28.12.2022
EE28.12.2022
FI28.12.2022
HR28.12.2022
LT28.12.2022
LV28.12.2022
NL28.12.2022
RO28.12.2022
RS28.12.2022
SE28.12.2022
SM28.12.2022
NO28.03.2023
GR29.03.2023
PT28.04.2023
Former [2023/35]AT28.12.2022
CZ28.12.2022
EE28.12.2022
FI28.12.2022
HR28.12.2022
LT28.12.2022
LV28.12.2022
NL28.12.2022
RO28.12.2022
RS28.12.2022
SE28.12.2022
SM28.12.2022
NO28.03.2023
GR29.03.2023
PT28.04.2023
Former [2023/34]EE28.12.2022
FI28.12.2022
HR28.12.2022
LT28.12.2022
LV28.12.2022
NL28.12.2022
RS28.12.2022
SE28.12.2022
SM28.12.2022
NO28.03.2023
GR29.03.2023
PT28.04.2023
Former [2023/33]FI28.12.2022
HR28.12.2022
LT28.12.2022
LV28.12.2022
NL28.12.2022
RS28.12.2022
SE28.12.2022
SM28.12.2022
NO28.03.2023
GR29.03.2023
Former [2023/29]FI28.12.2022
HR28.12.2022
LT28.12.2022
LV28.12.2022
NL28.12.2022
RS28.12.2022
SE28.12.2022
NO28.03.2023
GR29.03.2023
Former [2023/25]FI28.12.2022
HR28.12.2022
LT28.12.2022
LV28.12.2022
RS28.12.2022
SE28.12.2022
NO28.03.2023
GR29.03.2023
Former [2023/23]FI28.12.2022
LT28.12.2022
LV28.12.2022
SE28.12.2022
NO28.03.2023
GR29.03.2023
Former [2023/22]FI28.12.2022
LT28.12.2022
SE28.12.2022
NO28.03.2023
Former [2023/20]LT28.12.2022
NO28.03.2023
Documents cited:Search[A]US3762670  (CHILLSON C) [A] 2-5* column 7, line 39 - column 11, line 14; figure 5 *;
 [A]WO2015040364  (AIRBUS OPERATIONS LTD [GB]) [A] 1 * page 11, line 29 - page 15, line 9 *;
 [A]US2015151833  (COX ISAIAH [US]) [A] 1 * paragraph [[0035]]; figures 2a-2b *;
 [XAI]EP2982603  (AIRBUS OPERATIONS LTD [GB]) [X] 1 * paragraph [[0059]] - paragraph [[0064]]; figure 10 * [A] 5 [I] 2-4;
 [A]EP3222521  (SAFRAN LANDING SYSTEMS [FR]) [A] 1 * the whole document *
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.