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Extract from the Register of European Patents

EP About this file: EP0485263

EP0485263 - System for the integrated control of pitch and thrust for an aircraft [Right-click to bookmark this link]
StatusNo opposition filed within time limit
Status updated on  19.08.1995
Database last updated on 09.09.2024
Most recent event   Tooltip19.08.1995No opposition filed within time limitpublished 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 date91402936.804.11.1991
[1992/20]
Priority number, dateFR1990001371806.11.1990         Original published format: FR 9013718
[1992/20]
Filing languageFR
Procedural languageFR
PublicationType: 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:EP13.03.1992
ClassificationIPC:G05D1/06, B64C13/04, G05D1/00
[1994/42]
CPC:
B64C13/503 (EP,US); G05D1/0061 (EP,US); G05D1/0638 (EP,US)
Former IPC [1992/20]B64C13/04, G05D1/00, G05D1/06
Designated contracting statesDE,   GB,   IT,   NL [1992/20]
TitleGerman: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 procedure04.06.1992Examination requested  [1992/31]
27.12.1993Despatch of communication of intention to grant (Approval: Yes)
14.04.1994Communication of intention to grant the patent
06.05.1994Fee for grant paid
06.05.1994Fee for publishing/printing paid
Opposition(s)20.07.1995No opposition filed within time limit [1995/41]
Fees paidRenewal fee
27.10.1993Renewal fee patent year 03
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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 ?"
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.