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Extract from the Register of European Patents

EP About this file: EP1086801

EP1086801 - Method for manufacturing a composite sandwich panel and panel obtained thereby [Right-click to bookmark this link]
StatusNo opposition filed within time limit
Status updated on  24.10.2003
Database last updated on 22.11.2024
Most recent event   Tooltip23.10.2009Change - representativepublished on 25.11.2009  [2009/48]
Applicant(s)For all designated states
AIRBUS France
316 Route de Bayonne
31060 Toulouse / FR
[N/P]
Former [2003/14]For all designated states
AIRBUS France
316, Route de Bayonne
31060 Toulouse / FR
Former [2001/13]For all designated states
Aerospatiale Matra Airbus S.A.
37, Boulevard de Montmorency
75781 Paris Cedex 16 / FR
Inventor(s)01 / Fournier, Alain
Le Parayre, Sainte Foy de Peyrolières
31470 Saint Lys / FR
02 / Duret, Nathalie
31, rue des Bûches
31700 Blagnac / FR
 [2002/34]
Former [2001/13]01 / Fournier, Alain
Le Parayre, Saintes Foy de Peyrolières
31470 Saint-Lys / FR
02 / Duret, Nathalie
31, rue des Bûches
31700 Blagnac / FR
Representative(s)Poulin, Gérard, et al
BREVALEX
95, rue d'Amsterdam
75378 Paris Cedex 8 / FR
[N/P]
Former [2009/48]Poulin, Gérard, et al
Brevalex 3, rue du Docteur Lancereaux
75008 Paris / FR
Former [2001/13]Poulin, Gérard, et al
Société de Protection des Inventions 3, rue du Docteur Lancereaux
75008 Paris / FR
Application number, filing date00402567.218.09.2000
[2001/13]
Priority number, dateFR1999001176621.09.1999         Original published format: FR 9911766
[2001/13]
Filing languageFR
Procedural languageFR
PublicationType: A1 Application with search report 
No.:EP1086801
Date:28.03.2001
Language:FR
[2001/13]
Type: B1 Patent specification 
No.:EP1086801
Date:18.12.2002
Language:FR
[2002/51]
Search report(s)(Supplementary) European search report - dispatched on:EP05.01.2001
ClassificationIPC:B29C70/48, B29C70/08, B29D24/00
[2001/13]
CPC:
B29C70/088 (EP,US); B29C70/48 (EP,US); B29D24/005 (EP,US);
Y10T428/233 (EP,US); Y10T428/236 (EP,US); Y10T428/24157 (EP,US)
Designated contracting statesDE,   ES,   GB,   IT,   SE [2001/51]
Former [2001/13]AT,  BE,  CH,  CY,  DE,  DK,  ES,  FI,  FR,  GB,  GR,  IE,  IT,  LI,  LU,  MC,  NL,  PT,  SE 
TitleGerman:Verfahren zur Herstellung einer Sandwichverbundplatte und dadurch hergestellte Platte[2001/13]
English:Method for manufacturing a composite sandwich panel and panel obtained thereby[2001/13]
French:Procédé de fabrication d'un panneau sandwich en matériau composite, et panneau ainsi obtenu[2002/34]
Former [2001/13]Procédé de fabrication d'un panneau sandwich en matériau composite, et panneau ainsi obtenu.
Examination procedure10.08.2001Examination requested  [2001/41]
29.09.2001Loss of particular rights, legal effect: designated state(s)
19.12.2001Despatch of a communication from the examining division (Time limit: M04)
24.01.2002Despatch of communication of loss of particular rights: designated state(s) AT, BE, CH, CY, DK, FI, FR, GR, IE, LU, MC, NL, PT
28.03.2002Reply to a communication from the examining division
15.07.2002Communication of intention to grant the patent
05.10.2002Fee for grant paid
05.10.2002Fee for publishing/printing paid
Opposition(s)19.09.2003No opposition filed within time limit [2003/50]
Fees paidRenewal fee
20.09.2002Renewal fee patent year 03
Penalty fee
Penalty fee Rule 85a EPC 1973
09.11.2001AT   M01   Not yet paid
09.11.2001BE   M01   Not yet paid
09.11.2001CH   M01   Not yet paid
09.11.2001CY   M01   Not yet paid
09.11.2001DK   M01   Not yet paid
09.11.2001FI   M01   Not yet paid
09.11.2001FR   M01   Not yet paid
09.11.2001GR   M01   Not yet paid
09.11.2001IE   M01   Not yet paid
09.11.2001LU   M01   Not yet paid
09.11.2001MC   M01   Not yet paid
09.11.2001NL   M01   Not yet paid
09.11.2001PT   M01   Not yet paid
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Documents cited:Search[X]EP0722826  (BOEING CO [US]) [X] 1-7 * column 11, line 44 - column 12, line 22; claim 6 *
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.