EP0485263 - System for the integrated control of pitch and thrust for an aircraft [Right-click to bookmark this link] | Status | No opposition filed within time limit Status updated on 19.08.1995 Database last updated on 09.09.2024 | Most recent event Tooltip | 19.08.1995 | No opposition filed within time limit | published on 11.10.1995 [1995/41] | Applicant(s) | For all designated states AEROSPATIALE Société Nationale Industrielle 37, Boulevard de Montmorency 75781 Paris Cédex 16 / FR | [N/P] |
Former [1995/32] | For all designated states AEROSPATIALE Société Nationale Industrielle 37, Boulevard de Montmorency F-75781 Paris Cédex 16 / FR | ||
Former [1992/20] | For all designated states AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE Société Anonyme dite: 37, Boulevard de Montmorency F-75016 Paris / FR | Inventor(s) | 01 /
Farineau, Jacques 45 rue Saint Roch F-31400 Toulouse / FR | 02 /
Larramendy, Panxika 86, rue de la Concorde F-31000 Toulouse / FR | [1992/20] | Representative(s) | Bonnetat, Christian Gevers France 41, avenue de Friedland 75008 Paris / FR | [N/P] |
Former [1992/20] | Bonnetat, Christian CABINET BONNETAT 23, Rue de St. Pétersbourg F-75008 Paris / FR | Application number, filing date | 91402936.8 | 04.11.1991 | [1992/20] | Priority number, date | FR19900013718 | 06.11.1990 Original published format: FR 9013718 | [1992/20] | Filing language | FR | Procedural language | FR | Publication | Type: | A1 Application with search report | No.: | EP0485263 | Date: | 13.05.1992 | Language: | FR | [1992/20] | Type: | B1 Patent specification | No.: | EP0485263 | Date: | 19.10.1994 | Language: | FR | [1994/42] | Search report(s) | (Supplementary) European search report - dispatched on: | EP | 13.03.1992 | Classification | IPC: | G05D1/06, B64C13/04, G05D1/00 | [1994/42] | CPC: |
B64C13/503 (EP,US);
G05D1/0061 (EP,US);
G05D1/0638 (EP,US)
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Former IPC [1992/20] | B64C13/04, G05D1/00, G05D1/06 | Designated contracting states | DE, GB, IT, NL [1992/20] | Title | German: | Vorrichtung zur integrierten Steuerung der Längseigungs- und Schubachsen eines Luftfahrzeuges | [1992/20] | English: | System for the integrated control of pitch and thrust for an aircraft | [1992/20] | French: | Système pour la commande intégrée en profondeur et en poussée d'un aéronef | [1992/20] | Examination procedure | 04.06.1992 | Examination requested [1992/31] | 27.12.1993 | Despatch of communication of intention to grant (Approval: Yes) | 14.04.1994 | Communication of intention to grant the patent | 06.05.1994 | Fee for grant paid | 06.05.1994 | Fee for publishing/printing paid | Opposition(s) | 20.07.1995 | No opposition filed within time limit [1995/41] | Fees paid | Renewal fee | 27.10.1993 | Renewal fee patent year 03 |
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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 | [A]US3512737 (PLATT WALTER A, et al); | [A]FR2245999 (BODENSEEWERK GERAETETECH [DE]); | [A]US4266743 (KELLEY WENDELL W); | [A]GB2073114 (UNITED TECHNOLOGIES CORP); | [A]EP0296951 (AEROSPATIALE [FR]) | [A] - JOURNAL OF GUIDANCE AND CONTROL AND DYNAMICS, vol. 9, no. 6, novembre 1986, pages 614-619, New York, US; R.A. HESS et al.: "Cross coupling in pilot-vehicle systems" | [A] - ELECTRONICS & WIRELESS WORLD, vol. 96, no. 1652, juin 1990, pages 473-478, Sutton, GB; AVIONICS: "Safety in numbers ?" |