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Extract from the Register of European Patents

EP About this file: EP1661780

EP1661780 - Aircraft brake actuation system including anti-hysteresis control [Right-click to bookmark this link]
StatusNo opposition filed within time limit
Status updated on  11.11.2011
Database last updated on 07.10.2024
Most recent event   Tooltip11.11.2011No opposition filed within time limitpublished on 14.12.2011  [2011/50]
Applicant(s)For all designated states
Honeywell International Inc.
101 Columbia Road
Morristown, NJ 07960 / US
[2011/01]
Former [2008/38]For all designated states
Honeywell International Inc.
101 Columbia Avenue P.O. Box 2245
Morristown NJ 07960 / US
Former [2006/22]For all designated states
Honeywell International, Inc.
101 Columbia Avenue P.O. Box 2245
Morristown, New Jersey 07960 / US
Inventor(s)01 / Evans, Paul S.
4284 E Reins Road
Gilbert, AZ 85297 / US
02 / Quitmeyer, James N.
3871 S Barberry Place
Chandler, AZ 85248 / US
 [2006/22]
Representative(s)Buckley, Guy Julian, et al
Patent Outsourcing Limited
1 King Street
Bakewell
Derbyshire DE45 1DZ / GB
[N/P]
Former [2010/45]Buckley, Guy Julian, et al
Patent Outsourcing Limited 1 King Street Bakewell
Derbyshire DE45 1DZ / GB
Former [2006/22]Haley, Stephen
Gill Jennings & Every LLP Broadgate House 7 Eldon Street
London EC2M 7LH / GB
Application number, filing date05257129.618.11.2005
[2006/22]
Priority number, dateUS2004099360819.11.2004         Original published format: US 993608
[2006/22]
Filing languageEN
Procedural languageEN
PublicationType: A1 Application with search report 
No.:EP1661780
Date:31.05.2006
Language:EN
[2006/22]
Type: B1 Patent specification 
No.:EP1661780
Date:05.01.2011
Language:EN
[2011/01]
Search report(s)(Supplementary) European search report - dispatched on:EP01.03.2006
ClassificationIPC:B60T8/17, B60T13/74, B60T8/32
[2006/22]
CPC:
B60T8/1703 (EP,US)
Designated contracting statesDE,   FR,   GB [2007/06]
Former [2006/22]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:Hysteresisfreies Bremssteuerungsystem für ein Flugzeug[2006/22]
English:Aircraft brake actuation system including anti-hysteresis control[2006/22]
French:Systèm de commande de freinage sans hystérésis pour aéronef[2006/22]
Examination procedure20.11.2006Examination requested  [2007/01]
27.12.2006Despatch of a communication from the examining division (Time limit: M04)
23.04.2007Reply to a communication from the examining division
18.08.2010Communication of intention to grant the patent
18.11.2010Fee for grant paid
18.11.2010Fee for publishing/printing paid
Divisional application(s)EP10177791.0  / EP2263924
Opposition(s)06.10.2011No opposition filed within time limit [2011/50]
Fees paidRenewal fee
06.11.2007Renewal fee patent year 03
27.03.2008Renewal fee patent year 04
06.11.2009Renewal fee patent year 05
22.10.2010Renewal fee patent year 06
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Documents cited:Search[XA]US6480130  (HANSON MARK B [US], et al) [X] 1 * column 3, line 8 - line 57 * * claim 1 * * figures 1,4 * [A] 2,7;
 [A]US4078845  (AMBERG ROBERT LEO, et al) [A] 1 * claim 28 *
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.