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EP0529917
European procedure
Extract from the Register of European Patents
EP About this file: EP0529917
| EP0529917 - Fusion bonded thermoplastic leading edge for aircraft aerodynamic surfaces [Right-click to bookmark this link] | Status | No opposition filed within time limit Status updated on 23.09.1995 Database last updated on 03.06.2024 | Most recent event Tooltip | 17.02.2006 | Change - lapse in a contracting state Updated state(s): FR | published on 05.04.2006 [2006/14] | Applicant(s) | For all designated states BRITISH AEROSPACE PUBLIC LIMITED COMPANY Warwick House, P.O. Box 87, Farnborough Aerospace Centre Farnborough Hants. GU14 6YU / GB | [N/P] |
| Former [1993/09] | For all designated states BRITISH AEROSPACE PUBLIC LIMITED COMPANY Warwick House, P.O. Box 87, Farnborough Aerospace Centre Farnborough, Hants. GU14 6YU / GB | Inventor(s) | 01 /
Dominé, Christophe, British Aerospace Airbus Ltd. PO Box 77, Filton House Bristol BS99 7AR / GB | [1993/09] | Application number, filing date | 92307536.0 | 18.08.1992 | [1993/09] | Priority number, date | GB19910018186 | 23.08.1991 Original published format: GB 9118186 | [1993/09] | Filing language | EN | Procedural language | EN | Publication | Type: | A1 Application with search report | No.: | EP0529917 | Date: | 03.03.1993 | Language: | EN | [1993/09] | Type: | B1 Patent specification | No.: | EP0529917 | Date: | 23.11.1994 | Language: | EN | [1994/47] | Search report(s) | (Supplementary) European search report - dispatched on: | EP | 14.12.1992 | Classification | IPC: | B64C3/28, B29C65/00 | [1993/09] | CPC: |
B64C3/28 (EP,US);
B29C65/02 (EP,US);
B29C65/1412 (EP,US);
B29C66/72 (EP,US);
B29C66/7392 (EP,US);
B29C66/742 (EP,US);
B29K2105/06 (EP,US);
B29L2031/3085 (EP,US);
Y10S264/64 (EP,US);
Y10T156/1028 (EP,US);
Y10T156/1031 (EP,US);
Y10T156/1089 (EP,US);
Y10T156/109 (EP,US)
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| Designated contracting states | DE, ES, FR, GB, IT, NL, SE [1993/09] | Title | German: | Thermoplastische, schmelzverbundene Vorderkante für die aerodynamischen Flächen eines Flugzeuges | [1993/09] | English: | Fusion bonded thermoplastic leading edge for aircraft aerodynamic surfaces | [1993/09] | French: | Bord d'attaque pour surfaces aérodynamiques d'avion en matériel thermoplastique collé par fusion | [1993/09] | Examination procedure | 27.08.1992 | Examination requested [1993/09] | 06.05.1994 | Despatch of communication of intention to grant (Approval: Yes) | 27.05.1994 | Communication of intention to grant the patent | 21.06.1994 | Fee for grant paid | 21.06.1994 | Fee for publishing/printing paid | Opposition(s) | 24.08.1995 | No opposition filed within time limit [1995/46] | Fees paid | Renewal fee | 12.08.1994 | Renewal fee patent year 03 |
| Opt-out from the exclusive Tooltip competence of the Unified Patent Court | See the Register of the Unified Patent Court for opt-out data | ||
| 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 Tooltip | FR | 23.11.1994 | ES | 19.08.1995 | SE | 19.08.1995 | [2006/14] |
| Former [2004/37] | FR | 21.04.1995 | |
| ES | 19.08.1995 | ||
| SE | 19.08.1995 | ||
| Former [1996/23] | FR | 21.04.1995 | |
| SE | 19.08.1995 | ||
| Former [1995/41] | FR | 21.04.1995 | Documents cited: | Search | [A]US4657615 (BRAUN RUDOLF [CA], et al); | [A]EP0296283 (HONDA MOTOR CO LTD [JP]); | [A]NL8501678 (POLS ERIK BERNARD VAN DER) | [A] - NAVY TECHNICAL DISCLOSURE BULLETIN vol. 9, no. 2, December 1983, ARLINGTON US pages 93 - 98 W. J. WALLACE 'COMPOSITE AIR FOIL, NAVY TECH. CAT. NO.0164, NAVY CASE NO.66779' | Examination | - pages 93 - 98 W. J. WALLACE 'COMPOSITE AIR FOIL, NAVY TECH. CAT. NO.0164, NAVYCASE NO.66779' |