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Extract from the Register of European Patents

EP About this file: EP3707363

EP3707363 - THRUST REVERSER FOR AN AIRCRAFT TURBOJET ENGINE NACELLE AND ASSOCIATED NACELLE [Right-click to bookmark this link]
StatusThe application has been withdrawn
Status updated on  09.10.2020
Database last updated on 30.10.2024
FormerRequest for examination was made
Status updated on  14.08.2020
FormerThe international publication has been made
Status updated on  18.05.2019
Formerunknown
Status updated on  12.01.2019
Most recent event   Tooltip09.10.2020Withdrawal of applicationpublished on 11.11.2020  [2020/46]
Applicant(s)For all designated states
Safran Nacelles
route du Pont 8
76700 Gonfreville-l'Orcher / FR
[2020/38]
Inventor(s)01 / BOILEAU, Patrick
Route du Pont 8
76700 Gonfreville L'Orcher / FR
 [2020/38]
Representative(s)Delorme, Nicolas, et al
Cabinet Germain & Maureau
BP 6153
69466 Lyon Cedex 06 / FR
[2020/38]
Application number, filing date18827157.109.11.2018
[2020/38]
WO2018FR52800
Priority number, dateFR2017006058910.11.2017         Original published format: FR 1760589
[2020/38]
Filing languageFR
Procedural languageFR
PublicationType: A1 Application with search report
No.:WO2019092383
Date:16.05.2019
Language:FR
[2019/20]
Type: A1 Application with search report 
No.:EP3707363
Date:16.09.2020
Language:FR
The application published by WIPO in one of the EPO official languages on 16.05.2019 takes the place of the publication of the European patent application.
[2020/38]
Search report(s)International search report - published on:EP16.05.2019
ClassificationIPC:F02K1/72, F02K1/34, F02K1/82
[2020/38]
CPC:
F02K1/72 (EP,US); B64D29/06 (EP); F02K1/827 (EP);
F05D2220/32 (US); F05D2250/283 (EP); F05D2260/96 (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 [2020/38]
Extension statesBANot yet paid
MENot yet paid
Validation statesKHNot yet paid
MANot yet paid
MDNot yet paid
TNNot yet paid
TitleGerman:SCHUBUMKEHRVORRICHTUNG FÜR EINE FLUGZEUGTRIEBWERKSGONDEL UND ZUGEHÖRIGE GONDEL[2020/38]
English:THRUST REVERSER FOR AN AIRCRAFT TURBOJET ENGINE NACELLE AND ASSOCIATED NACELLE[2020/38]
French:INVERSEUR DE POUSSÉE POUR NACELLE DE TURBORÉACTEUR D'AÉRONEF ET NACELLE ASSOCIÉE[2020/38]
Entry into regional phase26.03.2020National basic fee paid 
26.03.2020Designation fee(s) paid 
26.03.2020Examination fee paid 
Examination procedure26.03.2020Amendment by applicant (claims and/or description)
26.03.2020Examination requested  [2020/38]
26.03.2020Date on which the examining division has become responsible
08.10.2020Application withdrawn by applicant  [2020/46]
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Cited inInternational search[A]WO9200183  (SHORT BROTHERS PLC [GB]) [A] 1-7* the whole document *;
 [XI]EP3054140  (UNITED TECHNOLOGIES CORP [US]) [X] 1,7 * figures 5a-5c * * paragraphs [0057] - [0067] * [I] 2-6;
 [X]WO2017021628  (SAFRAN NACELLES [FR]) [X] 1-7 * figures 1b, 2a, 2b * * pages 2,4,5 * * page 6, lines 15-25 *
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.