DE69412366T2 - Operating system for an aerodynamic rudder and aircraft guidance system - Google Patents

Operating system for an aerodynamic rudder and aircraft guidance system

Info

Publication number
DE69412366T2
DE69412366T2 DE1994612366 DE69412366T DE69412366T2 DE 69412366 T2 DE69412366 T2 DE 69412366T2 DE 1994612366 DE1994612366 DE 1994612366 DE 69412366 T DE69412366 T DE 69412366T DE 69412366 T2 DE69412366 T2 DE 69412366T2
Authority
DE
Germany
Prior art keywords
aircraft guidance
operating system
aerodynamic rudder
guidance system
rudder
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE1994612366
Other languages
German (de)
Other versions
DE69412366T3 (en
DE69412366D1 (en
Inventor
Jean-Baptiste Ansaldi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aerospatiale Matra
Original Assignee
Airbus Group SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=9447817&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE69412366(T2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Publication of DE69412366D1 publication Critical patent/DE69412366D1/en
Application granted granted Critical
Publication of DE69412366T2 publication Critical patent/DE69412366T2/en
Publication of DE69412366T3 publication Critical patent/DE69412366T3/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Details Of Aerials (AREA)
  • Train Traffic Observation, Control, And Security (AREA)
  • Braking Arrangements (AREA)
DE1994612366 1993-06-07 1994-05-18 Operating system for an aerodynamic rudder and aircraft guidance system Expired - Lifetime DE69412366T3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9306779 1993-06-07
FR9306779A FR2706200B1 (en) 1993-06-07 1993-06-07 Actuation system for aerodynamic control surfaces and systems for piloting aircraft, comprising at least one such actuation system.

Publications (3)

Publication Number Publication Date
DE69412366D1 DE69412366D1 (en) 1998-09-17
DE69412366T2 true DE69412366T2 (en) 1999-03-04
DE69412366T3 DE69412366T3 (en) 2004-03-25

Family

ID=9447817

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1994612366 Expired - Lifetime DE69412366T3 (en) 1993-06-07 1994-05-18 Operating system for an aerodynamic rudder and aircraft guidance system

Country Status (5)

Country Link
EP (1) EP0628783B2 (en)
DE (1) DE69412366T3 (en)
ES (1) ES2120584T5 (en)
FR (1) FR2706200B1 (en)
NO (1) NO307434B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010005350A1 (en) 2008-07-07 2010-01-14 Saab Ab Rudder machinery

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3204894A (en) * 1962-06-29 1965-09-07 Bofors Ab Roll stabilizing system for an airborne device
DE1298912B (en) * 1965-12-10 1969-07-03 Messerschmitt Boelkow Blohm Thrust vector control for a rocket propelled missile with at least one beam deflector
SE408323B (en) * 1976-06-08 1979-06-05 Bofors Ab CONTROL DEVICE FOR A BALLISTIC UNIT
US4274610A (en) * 1978-07-14 1981-06-23 General Dynamics, Pomona Division Jet tab control mechanism for thrust vector control
DE3606835C2 (en) * 1986-03-03 1997-03-27 Diehl Gmbh & Co Steering device for projectiles

Also Published As

Publication number Publication date
EP0628783A1 (en) 1994-12-14
NO942092L (en) 1994-12-08
ES2120584T5 (en) 2004-04-16
FR2706200B1 (en) 1995-08-11
NO307434B1 (en) 2000-04-03
NO942092D0 (en) 1994-06-06
EP0628783B2 (en) 2003-08-27
ES2120584T3 (en) 1998-11-01
DE69412366T3 (en) 2004-03-25
DE69412366D1 (en) 1998-09-17
EP0628783B1 (en) 1998-08-12
FR2706200A1 (en) 1994-12-16

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8327 Change in the person/name/address of the patent owner

Owner name: AEROSPATIALE MATRA, PARIS, FR

8366 Restricted maintained after opposition proceedings