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Extract from the Register of European Patents

EP About this file: EP0807574

EP0807574 - Method and apparatus for turn coordination gain as a function of flap position [Right-click to bookmark this link]
StatusNo opposition filed within time limit
Status updated on  09.05.2003
Database last updated on 15.07.2024
Most recent event   Tooltip18.07.2008Change - representativepublished on 20.08.2008  [2008/34]
Applicant(s)For all designated states
The Boeing Company
100 North Riverside Plaza
Chicago, IL 60606-1596 / US
[N/P]
Former [1997/47]For all designated states
THE BOEING COMPANY
P.O. Box 3707, M.S. 13-08
Seattle, Washington 98124-2207 / US
Inventor(s)01 / Tran, Chuong B.
4419 - 153rd Place S.W.
Lynnwood, WA 98037 / US
[1997/47]
Representative(s)Land, Addick Adrianus Gosling, et al
Arnold & Siedsma
Bezuidenhoutseweg 57
2594 AC Den Haag / NL
[N/P]
Former [2008/34]Land, Addick Adrianus Gosling, et al
Arnold & Siedsma Sweelinckplein 1
2517 GK Den Haag / NL
Former [1997/47]Land, Addick Adrianus Gosling, et al
Arnold & Siedsma, Advocaten en Octrooigemachtigden, Sweelinckplein 1
2517 GK Den Haag / NL
Application number, filing date97201290.029.04.1997
[1997/47]
Priority number, dateUS1996064561614.05.1996         Original published format: US 645616
[1997/47]
Filing languageEN
Procedural languageEN
PublicationType: A1 Application with search report 
No.:EP0807574
Date:19.11.1997
Language:EN
[1997/47]
Type: B1 Patent specification 
No.:EP0807574
Date:03.07.2002
Language:EN
[2002/27]
Search report(s)(Supplementary) European search report - dispatched on:EP13.09.1997
ClassificationIPC:B64C13/16, G05D1/08
[1997/47]
CPC:
G05D1/085 (EP,US)
Designated contracting statesDE,   FR,   GB [1997/47]
TitleGerman:Methode und Vorrichtung zur Verstärkungsanpassung eines Kurvenflugkoordinators in Abhängigkeit von der Landeklappenposition[1997/47]
English:Method and apparatus for turn coordination gain as a function of flap position[1997/47]
French:Méthode et dispositif d'adaptation du gain d'un coordinateur de virage en fonction de la position des volets[1997/47]
Examination procedure29.04.1998Examination requested  [1998/27]
20.08.2001Despatch of communication of intention to grant (Approval: Yes)
14.01.2002Communication of intention to grant the patent
07.02.2002Fee for grant paid
07.02.2002Fee for publishing/printing paid
Opposition(s)04.04.2003No opposition filed within time limit [2003/26]
Fees paidRenewal fee
06.04.1999Renewal fee patent year 03
03.04.2000Renewal fee patent year 04
02.04.2001Renewal fee patent year 05
22.04.2002Renewal fee patent year 06
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Documents cited:Search[A]FR2339920  (SPERRY RAND CORP [US]) [A] 1 * page 2, line 11 - page 5, line 11 * * page 8, line 22 - page 16, line 23 * * page 17, line 1 - page 18, line 18; figure 1 *;
 [A]EP0293018  (BOEING CO [US]) [A] 1 * abstract * * page 4, line 46 - page 5, line 53; figure 5 *;
 [A]EP0296951  (AEROSPATIALE [FR]) [A] 1 * abstract * * column 2, line 6 - column 4, line 34 * * column 8, line 61 - column 12, line 63; figures 2,5 *;
 US5072893  [ ] (CHAKRAVARTY ABHIJIT J M [US], et al);
 [A]  - PETER M. THOMPSON ET AL., "H ROBUST CONTROL SYNTHESIS FOR A FIGHTER PERFORMING A COORDINATED BANK TURN", PROCEEDINGS OF THE 29TH IEEE CONFERENCE ON DECISION AND CONTROL, HILTON HAWAIIAN VILLAGE, HONOLULU, HAWAII, (19901205), vol. 6, pages 3362 - 3366, XP000207313 [A] 1 * the whole document *
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.