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EP0091841
European procedure
Extract from the Register of European Patents
EP About this file: EP0091841
| EP0091841 - Device to be deployed for the extension of the exhaust nozzle of a rocket engine [Right-click to bookmark this link] | Status | No opposition filed within time limit Status updated on 20.02.1987 Database last updated on 09.04.2026 | Most recent event Tooltip | 20.02.1987 | No opposition filed within time limit | published on 08.04.1987 [1987/15] | Applicant(s) | For all designated states CENTRE NATIONAL D'ETUDES SPATIALES 2, Place Maurice Quentin 75001 Paris / FR | [N/P] |
| Former [1986/10] | For all designated states CENTRE NATIONAL D'ETUDES SPATIALES 2, Place Maurice Quentin F-75001 Paris / FR | ||
| Former [1983/42] | For all designated states CENTRE NATIONAL D'ETUDES SPATIALES 129, Rue de l'Université F-75007 Paris / FR | Inventor(s) | 01 /
Gauge, Paul Denis 10, Rue de Nangis F-77240 Cesson / FR | [1983/42] | Representative(s) | De Boisse, Louis CABINET de BOISSE 37, Avenue Franklin D. Roosevelt 75008 Paris / FR | [N/P] |
| Former [1983/42] | de Boisse, Louis Arnaud CABINET de BOISSE 37, Avenue Franklin D. Roosevelt F-75008 Paris / FR | Application number, filing date | 83400474.9 | 08.03.1983 | [1983/42] | Priority number, date | FR19820004508 | 17.03.1982 Original published format: FR 8204508 | [1983/42] | Filing language | FR | Procedural language | FR | Publication | Type: | A1 Application with search report | No.: | EP0091841 | Date: | 19.10.1983 | Language: | FR | [1983/42] | Type: | B1 Patent specification | No.: | EP0091841 | Date: | 23.04.1986 | Language: | FR | [1986/17] | Search report(s) | (Supplementary) European search report - dispatched on: | EP | 09.08.1983 | Classification | IPC: | F02K9/97 | [1983/42] | CPC: |
F02K9/976 (EP,US)
| Designated contracting states | BE, CH, DE, FR, GB, IT, LI, LU, NL [1986/09] |
| Former [1983/42] | AT, BE, CH, DE, FR, GB, IT, LI, LU, NL, SE | Title | German: | Zusatzvorrichtung für die Düse eines Raketenmotors | [1983/42] | English: | Device to be deployed for the extension of the exhaust nozzle of a rocket engine | [1983/42] | French: | Dispositif déployable de prolongement de tuyère de moteur fusée | [1983/42] | Examination procedure | 24.10.1983 | Examination requested [1984/02] | 13.09.1984 | Despatch of a communication from the examining division (Time limit: M04) | 20.12.1984 | Reply to a communication from the examining division | 10.07.1985 | Despatch of communication of intention to grant (Approval: ) | 24.10.1985 | Communication of intention to grant the patent | 20.12.1985 | Fee for grant paid | 20.12.1985 | Fee for publishing/printing paid | Opposition(s) | 24.01.1987 | No opposition filed within time limit [1987/15] | Fees paid | Renewal fee | 28.02.1985 | Renewal fee patent year 03 | 27.12.1985 | Renewal fee patent year 04 | Penalty fee | Additional fee for renewal fee | 31.03.1985 | 03 M06 Fee paid on 28.02.1985 |
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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 | [AD] JOURNAL OF SPACECRAFT AND ROCKETS, vol. 9, no. 7, juillet 1972, pages 485-486, New York, USA [AD] |