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Extract from the Register of European Patents

EP About this file: EP1918203

EP1918203 - Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof [Right-click to bookmark this link]
StatusNo opposition filed within time limit
Status updated on  04.02.2011
Database last updated on 02.11.2024
Most recent event   Tooltip16.12.2011Change - lapse in a contracting state
State(s) deleted from list of lapses: IT
published on 18.01.2012  [2012/03]
Applicant(s)For all designated states
Airbus Operations S.L.
Avenida John Lennon, s/n
28906 Getafe, Madrid / ES
[2010/06]
Former [2008/19]For all designated states
Airbus España, S.L.
Avda. John Lennon, s/n
28906 Getafe (Madrid) / ES
Inventor(s)01 / Martino Gonzalez, Esteban
Avda. Pontejos, 9
39005 Santander / ES
02 / Sanz Martinez, Pablo Timoteo
Los Galgos, 14
28861 Paracuellos del Jarama / ES
03 / Alvaro Granero, David
Canchal, 44-1[deg]-A
28021 Madrid / ES
 [2008/19]
Representative(s)Ungria López, Javier, et al
Avda. Ramón y Cajal, 78
28043 Madrid / ES
[N/P]
Former [2008/19]Ungria Lopez, Javier, et al
Avda. Ramón y Cajal, 78
28043 Madrid / ES
Application number, filing date07380156.531.05.2007
[2008/19]
Priority number, dateES2006000277031.10.2006         Original published format: ES 200602770
[2008/19]
Filing languageES
Procedural languageEN
PublicationType: A1 Application with search report 
No.:EP1918203
Date:07.05.2008
Language:EN
[2008/19]
Type: B1 Patent specification 
No.:EP1918203
Date:31.03.2010
Language:EN
[2010/13]
Search report(s)(Supplementary) European search report - dispatched on:EP22.11.2007
ClassificationIPC:B64D41/00, B64C7/02
[2008/19]
CPC:
B64D29/08 (EP,US); B64C7/02 (ES); B64D29/06 (ES);
B64D41/00 (EP,ES,US); B64D2041/002 (EP,US)
Designated contracting statesDE,   ES,   FR,   GB,   IT [2009/03]
Former [2008/19]AT,  BE,  BG,  CH,  CY,  CZ,  DE,  DK,  EE,  ES,  FI,  FR,  GB,  GR,  HU,  IE,  IS,  IT,  LI,  LT,  LU,  LV,  MC,  MT,  NL,  PL,  PT,  RO,  SE,  SI,  SK,  TR 
TitleGerman:Heckkonus für ein Flugzeug mit beweglicher Verkleidung und Stützstruktur für ein Hilfstriebwerk sowie Hilfselemente dafür[2008/19]
English:Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof[2008/19]
French:Pointe arrière pour avion avec carénage mobile et structure de support pour unité de puissance auxiliaire et éléments auxiliaires correspondants[2008/19]
Examination procedure06.11.2008Examination requested  [2008/51]
08.11.2008Loss of particular rights, legal effect: designated state(s)
14.11.2008Amendment by applicant (claims and/or description)
16.12.2008Despatch of communication of loss of particular rights: designated state(s) AT, BE, BG, CH, CY, CZ, DK, EE, FI, GR, HU, IE, IS, LT, LU, LV, MC, MT, NL, PL, PT, RO, SE, SI, SK, TR
20.10.2009Communication of intention to grant the patent
17.02.2010Fee for grant paid
17.02.2010Fee for publishing/printing paid
Opposition(s)04.01.2011No opposition filed within time limit [2011/10]
Fees paidRenewal fee
13.04.2009Renewal 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  TooltipES12.07.2010
[2012/03]
Former [2011/22]IT31.05.2010
ES12.07.2010
Documents cited:Search[A]GB1375868  ;
 [A]FR2291091  (SNECMA [FR]);
 [A]EP0361901  (SHORT BROTHERS PLC [GB]);
 [XY]US6039287  (LISTON LAURENCE D N [US], et al);
 [Y]US6220546  (KLAMKA ANDREW [US], et al)
by applicantUS6039287
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.