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Extract from the Register of European Patents

EP About this file: EP1884852

EP1884852 - Tuning procedure for aircraft fault detection [Right-click to bookmark this link]
StatusNo opposition filed within time limit
Status updated on  11.06.2010
Database last updated on 16.09.2024
Most recent event   Tooltip11.06.2010No opposition filed within time limitpublished on 14.07.2010  [2010/28]
Applicant(s)For all designated states
HONEYWELL INC.
101 Columbia Road P.O. Box 2245
Morristown NJ 07960 / US
[2008/38]
Former [2008/06]For all designated states
HONEYWELL INC.
P.O. Box 2245
Morristown, NJ 07962 / US
Inventor(s)01 / Ganguli, Subhabrata
12415 44th Place North
Plymouth, MN 55442 / US
02 / Papageorgiou, George
2572 Kenzie Terrace Apt. 205
Minneapolis, MN 55418 / US
03 / Glavaski-Radovanovic, Sonja
11435 50th Place North
Plymouth, MN 55442 / US
 [2008/06]
Representative(s)Haley, Stephen
Gill Jennings & Every LLP The Broadgate Tower
20 Primrose Street
London EC2A 2ES / GB
[N/P]
Former [2008/06]Haley, Stephen
Gill Jennings & Every LLP Broadgate House 7 Eldon Street
London EC2M 7LH / GB
Application number, filing date07107505.504.05.2007
[2008/06]
Priority number, dateUS2006046248104.08.2006         Original published format: US 462481
[2008/06]
Filing languageEN
Procedural languageEN
PublicationType: A1 Application with search report 
No.:EP1884852
Date:06.02.2008
Language:EN
[2008/06]
Type: B1 Patent specification 
No.:EP1884852
Date:05.08.2009
Language:EN
[2009/32]
Search report(s)(Supplementary) European search report - dispatched on:EP09.10.2007
ClassificationIPC:G05D1/00, B64D43/00, G01C23/00, // G08G5/00, G06F11/00
[2008/06]
CPC:
G08G5/0052 (EP,US); G05B23/0254 (EP,US); G08G5/0021 (EP,US)
Designated contracting statesDE,   FR,   GB [2008/42]
Former [2008/06]AT,  BE,  BG,  CH,  CY,  CZ,  DE,  DK,  EE,  ES,  FI,  FR,  GB,  GR,  HU,  IE,  IS,  IT,  LI,  LT,  LU,  LV,  MC,  MT,  NL,  PL,  PT,  RO,  SE,  SI,  SK,  TR 
TitleGerman:Einstellverfahren für die Fehlererkennung bei Flugzeugen[2008/06]
English:Tuning procedure for aircraft fault detection[2008/06]
French:Procédure de réglage pour la détection des défaillances d'un avion[2008/06]
Examination procedure24.07.2008Examination requested  [2008/36]
07.08.2008Loss of particular rights, legal effect: designated state(s)
25.08.2008Despatch of a communication from the examining division (Time limit: M06)
10.09.2008Despatch of communication of loss of particular rights: designated state(s) AT, BE, BG, CH, CY, CZ, DK, EE, ES, FI, GR, HU, IE, IS, IT, LT, LU, LV, MC, MT, NL, PL, PT, RO, SE, SI, SK, TR
26.01.2009Reply to a communication from the examining division
09.03.2009Communication of intention to grant the patent
22.06.2009Fee for grant paid
22.06.2009Fee for publishing/printing paid
Opposition(s)07.05.2010No opposition filed within time limit [2010/28]
Fees paidRenewal fee
07.05.2009Renewal fee patent year 03
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Documents cited:Search[YA]DE4022954  (BODENSEEWERK GERAETETECH [DE]) [Y] 1 * abstract * * page 2, line 7 - line 28 * * page 2, line 59 - page 3, line 4; figure 1 *[A] 8;
 [YA]WO9800334  (SUNDSTRAND CORP [US]) [Y] 1,2,7,8 * page 4, paragraph L - page 5, paragraph 2 * * page 6, paragraph 2 * * page 13, paragraph 4 - page 15, paragraph 2; figure 3 * [A] 3,4;
 [YA]EP1122694  (GEN ELECTRIC [US]) [Y] 1,2,7,8 * page 3, line 42 - page 4, line 7; figure 1 * * page 4, line 43 - line 49; figure 3 * * page 5, line 47 - line 53 * * page 8, line 12 - line 29; figure 6 * * page 8, line 44 - line 57; figure 8 * [A] 3,4;
 [YA]US6298286  (YING SIDNEY S [US]) [Y] 1,2,7,8 * abstract * * column 1, line 14 - line 32 * * column 2, line 51 - column 3, line 16 * * column 3, line 52 - column 5, line 7; figure 1 * * column 8, line 49 - column 10, line 31; figure 2 * [A] 3-6
by applicantUS6298286
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.