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Extract from the Register of European Patents

EP About this file: EP3990769

EP3990769 - THRUST REVERSER FOR TURBOFAN PROPULSION SYSTEM OF AN AIRCRAFT AND THRUST REVERSAL METHOD [Right-click to bookmark this link]
StatusGrant of patent is intended
Status updated on  05.05.2024
Database last updated on 11.09.2024
FormerRequest for examination was made
Status updated on  02.04.2022
FormerThe international publication has been made
Status updated on  17.12.2021
Formerunknown
Status updated on  06.07.2021
Most recent event   Tooltip25.05.2024New entry: Renewal fee paid 
Applicant(s)For all designated states
Leonardo S.p.A.
Piazza Monte Grappa 4
00195 Roma / IT
[2022/18]
Inventor(s)01 / POLI, Massimo
21057 Olgiate Olona (Varese) / IT
02 / VERCELLESI, Marco
20131 Milano / IT
 [2022/18]
Representative(s)Verdecchia, Valerio, et al
Jacobacci & Partners S.p.A.
Corso Emilia, 8
10152 Torino / IT
[2022/18]
Application number, filing date21734504.009.06.2021
[2022/18]
WO2021IB55056
Priority number, dateIT2020001384610.06.2020         Original published format: IT202000013846
[2022/18]
Filing languageIT
Procedural languageEN
PublicationType: A2 Application without search report
No.:WO2021250584
Date:16.12.2021
Language:EN
[2021/50]
Type: A2 Application without search report 
No.:EP3990769
Date:04.05.2022
Language:EN
The application published by WIPO in one of the EPO official languages on 16.12.2021 takes the place of the publication of the European patent application.
[2022/18]
Search report(s)International search report - published on:EP10.02.2022
ClassificationIPC:F02K1/72, F02K1/60
[2022/18]
CPC:
F02K1/72 (EP,US); F02K1/68 (CN,US); F02C7/20 (EP,US);
F02K1/60 (EP,US); F05D2250/411 (EP,US); 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 [2022/18]
TitleGerman:SCHUBUMKEHRVORRICHTUNG FÜR EIN ANTRIEBSSYSTEM EINES MANTELSTROMTRIEBWERKS EINES FLUGZEUGS UND SCHUBUMKEHRVERFAHREN[2022/18]
English:THRUST REVERSER FOR TURBOFAN PROPULSION SYSTEM OF AN AIRCRAFT AND THRUST REVERSAL METHOD[2022/18]
French:INVERSEUR DE POUSSÉE POUR SYSTÈME DE PROPULSION DE RÉACTEUR À DOUBLE FLUX D'UN AÉRONEF ET PROCÉDÉ D'INVERSION DE POUSSÉE ASSOCIÉ[2024/20]
Former [2022/18]INVERSEUR DE POUSSÉE POUR SYSTÈME DE PROPULSION DE RÉACTEUR À DOUBLE FLUX D'UN AÉRONEF ET SYSTÈME DE PROPULSION DE RÉACTEUR À DOUBLE FLUX ET PROCÉDÉ D'INVERSION DE POUSSÉE ASSOCIÉS
Entry into regional phase28.01.2022National basic fee paid 
28.01.2022Designation fee(s) paid 
28.01.2022Examination fee paid 
Examination procedure28.01.2022Examination requested  [2022/18]
28.01.2022Date on which the examining division has become responsible
17.06.2022Amendment by applicant (claims and/or description)
06.05.2024Communication of intention to grant the patent
Divisional application(s)EP22175600.0  / EP4071341
EP22175604.2  / EP4071342
Fees paidRenewal fee
31.03.2023Renewal fee patent year 03
24.05.2024Renewal fee patent year 04
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Cited inInternational search[X]US2933890  (MORRISON JOHN A) [X] 1,8,17,18 * figures 6,7 *;
 [A]DE1937679  (MESSERSCHMITT BOELKOW BLOHM) [A] 1-18* figures 1,2 *;
 [Y]US2014061332  (DEZEUSTRE NICOLAS [FR], et al) [Y] 15 * paragraphs [0121] - [0129]; figures 7,8a,8b,9 *;
 [Y]US2016363097  (FOUTCH DAVID W [US]) [Y] 10 * paragraphs [0022] , [0023]; figures 1,2 *;
 [X]US2017198658  (HIGGINS ROGER [US]) [X] 1,2,6,8,11-13,16-18 * paragraphs [0045] - [0048]; figures 3A,3B,4,5,7 *;
 [XY]US2019284952  (GARDES PASCAL [FR], et al) [X] 1-3,6,8,11-13,16-18 * paragraphs [0035] - [0057]; figures 2-4 * [Y] 10,15
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.