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Extract from the Register of European Patents

EP About this file: EP1108958

EP1108958 - Fuel nozzle for gas turbine engine and method of assembling [Right-click to bookmark this link]
StatusNo opposition filed within time limit
Status updated on  27.10.2006
Database last updated on 19.10.2024
Most recent event   Tooltip17.11.2017Lapse of the patent in a contracting statepublished on 20.12.2017  [2017/51]
Applicant(s)For all designated states
GENERAL ELECTRIC COMPANY
1 River Road
Schenectady, NY 12345 / US
[N/P]
Former [2001/25]For all designated states
GENERAL ELECTRIC COMPANY
1 River Road
Schenectady, NY 12345 / US
Inventor(s)01 / Chauvette, Claude Henry
6579 Kenview Drive
Cincinnati, Ohio 45243 / US
02 / Joshi, Narendra Digamber
12169 Village Woods Drive
Cincinnati, Ohio 45241 / US
 [2001/25]
Representative(s)Goode, Ian Roy, et al
London Patent Operation
General Electric International, Inc.
15 John Adam Street
London
WC2N 6LU / GB
[N/P]
Former [2009/31]Goode, Ian Roy, et al
London Patent Operation General Electric International, Inc. 15 John Adam Street London
WC2N 6LU / GB
Former [2001/25]Goode, Ian Roy, et al
GE LONDON PATENT OPERATION, Essex House, 12/13 Essex Street
London WC2R 3AA / GB
Application number, filing date00311263.815.12.2000
[2001/25]
Priority number, dateUS1999046655717.12.1999         Original published format: US 466557
[2001/25]
Filing languageEN
Procedural languageEN
PublicationType: A1 Application with search report 
No.:EP1108958
Date:20.06.2001
Language:EN
[2001/25]
Type: B1 Patent specification 
No.:EP1108958
Date:21.12.2005
Language:EN
[2005/51]
Search report(s)(Supplementary) European search report - dispatched on:EP28.02.2001
ClassificationIPC:F23R3/28, F23D11/38, F23D14/48, B05B15/06
[2001/25]
CPC:
F23R3/283 (EP,US); B05B15/65 (EP,US); F23D11/38 (EP,US);
F23D14/48 (EP,US); Y10T29/49348 (EP,US)
Designated contracting statesDE,   FR,   GB,   IT [2002/11]
Former [2001/25]AT,  BE,  CH,  CY,  DE,  DK,  ES,  FI,  FR,  GB,  GR,  IE,  IT,  LI,  LU,  MC,  NL,  PT,  SE,  TR 
TitleGerman:Gasturbinenbrennstoffeinspritzdüse und Montageverfahren[2001/25]
English:Fuel nozzle for gas turbine engine and method of assembling[2001/25]
French:Injecteur de carburant de turbine à gaz et méthode de montage[2001/25]
Examination procedure20.12.2001Examination requested  [2002/09]
28.10.2004Despatch of a communication from the examining division (Time limit: M06)
21.04.2005Reply to a communication from the examining division
10.06.2005Communication of intention to grant the patent
20.10.2005Fee for grant paid
20.10.2005Fee for publishing/printing paid
Opposition(s)22.09.2006No opposition filed within time limit [2006/48]
Fees paidRenewal fee
02.01.2003Renewal fee patent year 03
02.01.2004Renewal fee patent year 04
03.01.2005Renewal fee patent year 05
02.01.2006Renewal fee patent year 06
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Former [2010/20]deleted
Former [2007/35]IT21.12.2005
Documents cited:Search[XA]FR985652  (ROLLS ROYCE) [X] 1 * page 2, line 37 - line 50 * * figures 1,2 *[A] 10;
 [X]GB2328386  (SPRAYING SYSTEMS CO [US]) [X] 1-3,5-7,10 * page 6, line 3 - line 34 * * page 7, line 17 - page 8, line 35 * * figures 1,4,5 *
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.