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Extract from the Register of European Patents

EP About this file: EP0435764

EP0435764 - System to lower the stresses applied to a wing, especially at the mast-base connection of the wings from a flying aircraft [Right-click to bookmark this link]
StatusNo opposition filed within time limit
Status updated on  08.01.1996
Database last updated on 09.09.2024
Most recent event   Tooltip08.01.1996No opposition filed within time limitpublished on 07.02.1996 [1996/06]
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 [1991/27]For all designated states
AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE Société Anonyme dite:
37, Boulevard de Montmorency
F-75016 Paris / FR
Inventor(s)01 / Fabre, Pierre
16, rue du Foyer Toulousain
F-31300 Toulouse / FR
02 / Lacoste, Philippe
2, Rue du Commissaire Philippe
F-31000 Toulouse / FR
03 / Le Tron, Xavier
41, rue de la Colombette
F-31000 Toulouse / FR
[1991/27]
Representative(s)Bonnetat, Christian
Gevers France
41, avenue de Friedland
75008 Paris / FR
[N/P]
Former [1991/27]Bonnetat, Christian
CABINET BONNETAT 23, Rue de St. Pétersbourg
F-75008 Paris / FR
Application number, filing date90403753.824.12.1990
[1991/27]
Priority number, dateFR1989001734128.12.1989         Original published format: FR 8917341
[1991/27]
Filing languageFR
Procedural languageFR
PublicationType: A1 Application with search report 
No.:EP0435764
Date:03.07.1991
Language:FR
[1991/27]
Type: B1 Patent specification 
No.:EP0435764
Date:15.02.1995
Language:FR
[1995/07]
Search report(s)(Supplementary) European search report - dispatched on:EP22.03.1991
ClassificationIPC:G05D1/00, B64C13/16, G05D1/06
[1991/27]
CPC:
B64C13/16 (EP,US); G05D1/0066 (EP,US)
Designated contracting statesDE,   ES,   GB,   IT,   NL [1991/27]
TitleGerman:Verfahren zur Verminderung der Flügelspannung, insbesondere bei Mastfussbefestigung des Flügels eines fliegenden Flugzeugs[1991/27]
English:System to lower the stresses applied to a wing, especially at the mast-base connection of the wings from a flying aircraft[1991/27]
French:Système pour diminuer les efforts appliqués à la voilure et notamment à l'emplanture des ailes d'un aéronef en vol[1991/27]
Examination procedure26.07.1991Examination requested  [1991/38]
30.09.1993Despatch of a communication from the examining division (Time limit: M04)
07.01.1994Reply to a communication from the examining division
17.05.1994Despatch of communication of intention to grant (Approval: Yes)
23.08.1994Communication of intention to grant the patent
23.09.1994Fee for grant paid
23.09.1994Fee for publishing/printing paid
Opposition(s)16.11.1995No opposition filed within time limit [1996/06]
Fees paidRenewal fee
30.11.1992Renewal fee patent year 03
03.12.1993Renewal fee patent year 04
08.12.1994Renewal fee patent year 05
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Documents cited:Search[Y]US4562546  (WYKES JOHN H [US], et al);
 [X]EP0213760  (SPERRY CORP [US]);
 [A]WO8702964  (GRUMMAN AEROSPACE CORP [US]);
 [A]US4725020  (WHITENER PHILIP C [US]);
 [Y]US4787042  (BURNS ROGER D [US], et al);
 [Y]US4796192  (LEWIS GEORGE E [US]);
 [Y]US4821982  (VAN PATTEN ROBERT E [US]);
 [A]US4821981  (GANGSAAS DAGFINN [US], et al)
 [A]  - JOURNAL OF AIRCRAFT. vol. 26, no. 4, 26 avril 1989, NEW YORK US pages 322 - 327; Y.Matsuzaki: "Gust Load Alleviation of a Transport-Type Wing:Test and Analysis"
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.