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Extract from the Register of European Patents

EP About this file: EP0747655

EP0747655 - Blended missile autopilot [Right-click to bookmark this link]
StatusThe application is deemed to be withdrawn
Status updated on  22.07.2005
Database last updated on 03.08.2024
Most recent event   Tooltip13.11.2009Change - representativepublished on 16.12.2009  [2009/51]
Applicant(s)For all designated states
RAYTHEON COMPANY
PO Box 902
2000 East El Segundo Blvd.
El Segundo
California 90245 / US
[N/P]
Former [1998/41]For all designated states
Raytheon Company
PO Box 902, 2000 El Segundo Blvd.
El Segundo, California 90245 / US
Former [1996/50]For all designated states
HUGHES MISSILE SYSTEMS COMPANY
7200 Hughes Terrace
Los Angeles, California 90080-0028 / US
Inventor(s)01 / Cannon, James J.
1800 Key West Avenue
Northridge, CA 91326 / US
02 / Elkanick, Mark E.
7671 E. Tanque Verde No.223
Tucson, Arizona 85715 / US
[1996/50]
Representative(s)Jackson, Richard Eric
Carpmaels & Ransford LLP
One Southampton Row
London WC1B 5HA / GB
[N/P]
Former [2009/51]Jackson, Richard Eric
Carpmaels & Ransford 43-45 Bloomsbury Square
London WC1A 2RA / GB
Former [1996/50]Jackson, Richard Eric
Carpmaels & Ransford, 43 Bloomsbury Square
London WC1A 2RA / GB
Application number, filing date96303437.615.05.1996
[1996/50]
Priority number, dateUS1995046360305.06.1995         Original published format: US 463603
[1996/50]
Filing languageEN
Procedural languageEN
PublicationType: A2 Application without search report 
No.:EP0747655
Date:11.12.1996
Language:EN
[1996/50]
Type: A3 Search report 
No.:EP0747655
Date:02.12.1998
[1998/49]
Search report(s)(Supplementary) European search report - dispatched on:EP15.10.1998
ClassificationIPC:F41G7/00, G05D1/10, F41G7/20
[1998/49]
CPC:
F42B10/64 (EP,US); F41G7/22 (EP,US); F42B10/663 (EP,US)
Former IPC [1996/50]F41G7/00
Designated contracting statesDE,   FR,   GB,   IT [1996/50]
TitleGerman:Vielseitiger Autopilot für Raketen[1996/50]
English:Blended missile autopilot[1996/50]
French:Pilote automatique de type multiple pour missile[1996/50]
Examination procedure10.05.1999Examination requested  [1999/27]
26.01.2002Observations by third parties
24.08.2004Despatch of a communication from the examining division (Time limit: M06)
27.11.2004Observations by third parties
04.03.2005Application deemed to be withdrawn, date of legal effect  [2005/36]
11.04.2005Despatch of communication that the application is deemed to be withdrawn, reason: reply to the communication from the examining division not received in time  [2005/36]
Fees paidRenewal fee
20.04.1998Renewal fee patent year 03
14.04.1999Renewal fee patent year 04
17.04.2000Renewal fee patent year 05
23.04.2001Renewal fee patent year 06
15.04.2002Renewal fee patent year 07
16.04.2003Renewal fee patent year 08
19.04.2004Renewal fee patent year 09
Penalty fee
Additional fee for renewal fee
31.05.200510   M06   Not yet paid
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Documents cited:Search[A]JPH0695737  ;
 [Y]DE3047389  (MOTOROLA INC [US]) [Y] 5 * page 5, line 8 - page 10, line 14; figures 1-5 *;
 [A]US5094406  (SHAFER DANIEL E [US]) [A] 1,3,5 * column A * * column 3, line 12 - column 8, line 2; figures 1-6 *;
 [XY]EP0489712  (BRITISH AEROSPACE [GB]) [X] 1,3 * abstract * * page 2, column 2, line 36 - page 4, column 6, line 58; figures 1-9 * [Y] 5;
 [A]US5259569  (WAYMEYER WALTER K [US], et al) [A] 1,3,5 * column A * * column 4, line 27 - column 8, line 9; figures 1-8 *;
 [A]WO9400731  (GRUSHIN PETR D [RU], et al) [A] 1,3,5 * abstract *;
 [A]JPH0695737  (JAPAN TECH RES & DEV INST, et al) [A] 1,3,5 * figures 1-5 *;
 [AP]EP0683086  (TRW INC [US]) [AP] 1,3,5 * abstract ** page 4, line 6 - page 10, line 34; figures 1-8 *
 [A]  - PATENT ABSTRACTS OF JAPAN, (19940708), vol. 018, no. 365, Database accession no. (P - 1767), & JP06095737 A 19940408 (TECH RES & DEV INST OF JAPAN DEF AGENCY;OTHERS: 01) [A] 1,3,5 * abstract *
otherJPS63290400K
 JPS63290400
 JPH04316994
 JPH07133999
    - INNOCENTI M., THUKRAL A., "Simultaneous Reaction Jet and Aerdoynamic Control of Missile Systems", AIAA, (1993), pages 347 - 354, XP002907507
    - WEIL R.D ET AL, "Blended Aero & Reaction Jet Missile Autopilot Design Using VSS Techniques", IEEE, PROCEEDINGS OF THE 30TH CONFERENCE ON DECISION AND CONTROL, BRIGHTON UK, (1991), pages 2028 - 2029, XP002907508
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.