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Extract from the Register of European Patents

EP About this file: EP1482126

EP1482126 - Rotor assembly for a gas turbine engine [Right-click to bookmark this link]
Former [2004/49]Dovetail assembly of a gas turbine engine
[2010/42]
StatusNo opposition filed within time limit
Status updated on  20.07.2012
Database last updated on 03.10.2024
Most recent event   Tooltip20.07.2012No opposition filed within time limitpublished on 22.08.2012  [2012/34]
Applicant(s)For all designated states
GENERAL ELECTRIC COMPANY
1 River Road
Schenectady, NY 12345 / US
[N/P]
Former [2004/49]For all designated states
GENERAL ELECTRIC COMPANY
1 River Road
Schenectady, NY 12345 / US
Inventor(s)01 / Dibella, Joseph John
23 Courtney Road
West Roxbury, MA 02132-1043 / US
 [2004/49]
Representative(s)Illingworth-Law, William Illingworth, et al
GPO Europe
GE International Inc. The Ark
201 Talgarth Road
Hammersmith
London W6 8BJ / GB
[N/P]
Former [2011/33]Illingworth-Law, William Illingworth, et al
Global Patent Operation - Europe GE International Inc. 15 John Adam Street
London WC2N 6LU / GB
Former [2004/49]Pedder, James Cuthbert, et al
London Patent Operation, General Electric International, Inc., 15 John Adam Street
London WC2N 6LU / GB
Application number, filing date04253139.227.05.2004
[2004/49]
Priority number, dateUS2003044781729.05.2003         Original published format: US 447817
[2004/49]
Filing languageEN
Procedural languageEN
PublicationType: A2 Application without search report 
No.:EP1482126
Date:01.12.2004
Language:EN
[2004/49]
Type: A3 Search report 
No.:EP1482126
Date:22.11.2006
[2006/47]
Type: B1 Patent specification 
No.:EP1482126
Date:14.09.2011
Language:EN
[2011/37]
Search report(s)(Supplementary) European search report - dispatched on:EP23.10.2006
ClassificationIPC:F01D5/30
[2004/49]
CPC:
F01D5/3038 (EP,US); F05D2250/70 (EP,US); F05D2250/711 (EP,US);
Y02T50/60 (EP,US)
Designated contracting statesDE,   FR,   GB [2007/30]
Former [2004/49]AT,  BE,  BG,  CH,  CY,  CZ,  DE,  DK,  EE,  ES,  FI,  FR,  GB,  GR,  HU,  IE,  IT,  LI,  LU,  MC,  NL,  PL,  PT,  RO,  SE,  SI,  SK,  TR 
TitleGerman:Rotoranordnung für eine Gasturbinentriebwerk[2010/42]
English:Rotor assembly for a gas turbine engine[2010/42]
French:Ensemble rotor pour moteur à turbine à gaz[2010/42]
Former [2004/49]Schwalbenschwanzförmige Schaufelanordnung in einer Gasturbine
Former [2004/49]Dovetail assembly of a gas turbine engine
Former [2004/49]Aubage en forme de queue d'aronde dans une turbine à gaz
Examination procedure22.05.2007Examination requested  [2007/27]
11.07.2007Despatch of a communication from the examining division (Time limit: M04)
20.11.2007Reply to a communication from the examining division
31.01.2011Communication of intention to grant the patent
10.06.2011Fee for grant paid
10.06.2011Fee for publishing/printing paid
Divisional application(s)The date of the Examining Division's first communication in respect of the earliest application for which a communication has been issued is  11.07.2007
Opposition(s)15.06.2012No opposition filed within time limit [2012/34]
Fees paidRenewal fee
31.05.2006Renewal fee patent year 03
31.05.2007Renewal fee patent year 04
02.06.2008Renewal fee patent year 05
02.06.2009Renewal fee patent year 06
31.05.2010Renewal fee patent year 07
31.05.2011Renewal fee patent year 08
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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.
Documents cited:Search[X]FR1294695  (RICHARDSONS) [X] 1-6 * page 1, column 2 * * figures 1,2 *;
 [A]US5183389  (GILCHRIST ALAN R [US], et al) [A] 1-6 * the whole document *;
 [A]US6375429  (HALILA HERBERT [US], et al) [A] 1-6* column 4, lines 17-65; figure 4 *
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.