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Extract from the Register of European Patents

EP About this file: EP1775553

EP1775553 - Hybrid centered head-down aircraft attitude display and method for calculating displayed drift angle limit [Right-click to bookmark this link]
StatusNo opposition filed within time limit
Status updated on  15.02.2013
Database last updated on 05.10.2024
Most recent event   Tooltip15.02.2013No opposition filed within time limitpublished on 20.03.2013  [2013/12]
Applicant(s)For all designated states
Honeywell International Inc.
101 Columbia Road
Morristown, NJ 07960 / US
[2012/15]
Former [2008/38]For all designated states
Honeywell International Inc.
101 Columbia Avenue P.O. Box 2245
Morristown NJ 07960 / US
Former [2007/16]For all designated states
Honeywell International Inc.
P O Box 2245
Morristown, NJ 07962 / US
Inventor(s)01 / He, Gang
/ 1 Pletcher Place
Morristown, NJ 07960 / US
 [2012/15]
Former [2007/16]01 / He, Gang
1 Pletcher Place
Morristown, NJ 07960 / US
Representative(s)Buckley, Guy Julian, et al
Patent Outsourcing Limited
1 King Street
Bakewell
Derbyshire DE45 1DZ / GB
[N/P]
Former [2010/42]Buckley, Guy Julian, et al
Patent Outsourcing Limited Cornerhourse 1 King Street Bakewell
Derbyshire DE45 1EW / GB
Former [2007/16]Haley, Stephen
Gill Jennings & Every LLP Broadgate House 7 Eldon Street
London EC2M 7LH / GB
Application number, filing date06121880.606.10.2006
[2007/16]
Priority number, dateUS2005024923712.10.2005         Original published format: US 249237
[2007/16]
Filing languageEN
Procedural languageEN
PublicationType: A1 Application with search report 
No.:EP1775553
Date:18.04.2007
Language:EN
[2007/16]
Type: B1 Patent specification 
No.:EP1775553
Date:11.04.2012
Language:EN
[2012/15]
Search report(s)(Supplementary) European search report - dispatched on:EP20.02.2007
ClassificationIPC:G01C23/00
[2007/16]
CPC:
G01C23/005 (EP,US)
Designated contracting statesDE,   FR,   GB [2007/52]
Former [2007/16]AT,  BE,  BG,  CH,  CY,  CZ,  DE,  DK,  EE,  ES,  FI,  FR,  GB,  GR,  HU,  IE,  IS,  IT,  LI,  LT,  LU,  LV,  MC,  NL,  PL,  PT,  RO,  SE,  SI,  SK,  TR 
TitleGerman:Hybride zentrierte Fluglagenanzeige mit Blickrichtung nach unten und Verfahren zur Berechnung des angezeigten Abdriftwinkellimits[2007/16]
English:Hybrid centered head-down aircraft attitude display and method for calculating displayed drift angle limit[2007/16]
French:Viseur d'attitude d'aéronef tête basse centré hybride et procédé de calcul de la limite d'angle de dérive affichée[2007/16]
Examination procedure10.10.2007Examination requested  [2007/47]
27.12.2011Communication of intention to grant the patent
29.02.2012Fee for grant paid
29.02.2012Fee for publishing/printing paid
Divisional application(s)The date of the Examining Division's first communication in respect of the earliest application for which a communication has been issued is  27.12.2011
Opposition(s)14.01.2013No opposition filed within time limit [2013/12]
Fees paidRenewal fee
27.03.2008Renewal fee patent year 03
07.10.2009Renewal fee patent year 04
23.09.2010Renewal fee patent year 05
10.10.2011Renewal fee patent year 06
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Documents cited:Search[A]GB1209922  (KAISER AEROSPACE & ELECTRONICS [US]) [A] 1,5,8* the whole document *;
 [A]US5745054  (WILKENS DEAN RICHARD [US]) [A] 1,5,8 * the whole document *;
 [A]US2003132860  (FEYEREISEN THEA L [US], et al) [A] 1-10 * paragraphs [0019] , [0043] , [0068] , [0166] - [0186]; figure 3 *;
 [A]US2004160341  (FEYEREISEN THEA L [US], et al) [A] 1-10 * paragraphs [0029] - [0032] - [0083]; figures 2-4 *
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.