ES2120584T3 - DRIVING SYSTEM FOR AERODYNAMIC RUDDER AND SYSTEMS FOR PILOTING AIRCRAFT. - Google Patents

DRIVING SYSTEM FOR AERODYNAMIC RUDDER AND SYSTEMS FOR PILOTING AIRCRAFT.

Info

Publication number
ES2120584T3
ES2120584T3 ES94401101T ES94401101T ES2120584T3 ES 2120584 T3 ES2120584 T3 ES 2120584T3 ES 94401101 T ES94401101 T ES 94401101T ES 94401101 T ES94401101 T ES 94401101T ES 2120584 T3 ES2120584 T3 ES 2120584T3
Authority
ES
Spain
Prior art keywords
systems
aerodynamic
driving system
coils
aerodynamic 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
ES94401101T
Other languages
Spanish (es)
Other versions
ES2120584T5 (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.)
Airbus Group SAS
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=ES2120584(T3) "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
Application granted granted Critical
Publication of ES2120584T3 publication Critical patent/ES2120584T3/en
Publication of ES2120584T5 publication Critical patent/ES2120584T5/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)

Abstract

LA PRESENTE INVENCION SE REFIERE A UN SISTEMA DE ACCIONAMIENTO (1) PARA TRAER UN TIMON AERODINAMICO (G) EN UNA U OTRA DE LAS DOS POSICIONES ACTIVAS, ESTABLES Y OPUESTAS UNA DE LA OTRA RESPECTO DE UNA POSICION NEUTRA. SEGUN LA INVENCION, ESTE SISTEMA DE ACCIONAMIENTO COMPRENDE: , DOS BOBINAS ELECTROMAGNETICAS (A,B) DISPUESTAS SOBRE UN SOPORTE FIJO (2), UNA ENFRENTE DE LA OTRA; . UNA PALETA MOVIL (P) UNO DE CUYOS EXTREMOS (4) ESTA FIJADO ELASTICAMENTE A DICHO SOPORTE FIJO (2), Y EL OTRO EXTREMO (6) ESTA DISPUESTO ENTRE DICHAS BOBINAS (A,B) Y ES SUSCEPTIBLE DE SER ATRAIDO POR CADA UNA DE DICHAS BOBINAS; Y . UN ELEMENTO MOVIL (7) SOLIDARIO DE DICHA PALETA (P) Y QUE LLEVA DICHO TIMON AERODINAMICO (G). - PILOTAJE DE AERONAVES.THE PRESENT INVENTION REFERS TO A DRIVE SYSTEM (1) TO BRING AN AERODYNAMIC RUDDER (G) IN ONE OR OTHER OF THE TWO ACTIVE, STABLE AND OPPOSITE POSITIONS ONE OF THE OTHER WITH RESPECT TO A NEUTRAL POSITION. ACCORDING TO THE INVENTION, THIS DRIVE SYSTEM INCLUDES: TWO ELECTROMAGNETIC COILS (A, B) ARRANGED ON A FIXED SUPPORT (2), ONE IN FRONT OF THE OTHER; . A MOBILE PALLET (P) ONE OF WHOSE EXTREMS (4) IS ELASTICALLY FIXED TO SUCH FIXED SUPPORT (2), AND THE OTHER END (6) IS ARRANGED BETWEEN SUCH COILS (A, B) AND IS SUSCEPTIBLE TO BE ATTRACTED BY EACH OF SUCH COILS; Y . A MOBILE ELEMENT (7) SOLIDARITY OF SUCH PALETTE (P) AND THAT CARRIES SAID AERODYNAMIC TIMON (G). - AIRCRAFT PILOTING.

ES94401101T 1993-06-07 1994-05-18 DRIVE SYSTEM FOR AERODYNAMIC TIMON AND SYSTEMS FOR AIRCRAFT PILOTING. Expired - Lifetime ES2120584T5 (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 (2)

Publication Number Publication Date
ES2120584T3 true ES2120584T3 (en) 1998-11-01
ES2120584T5 ES2120584T5 (en) 2004-04-16

Family

ID=9447817

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94401101T Expired - Lifetime ES2120584T5 (en) 1993-06-07 1994-05-18 DRIVE SYSTEM FOR AERODYNAMIC TIMON AND SYSTEMS FOR AIRCRAFT PILOTING.

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
DE69412366T3 (en) 2004-03-25
DE69412366D1 (en) 1998-09-17
DE69412366T2 (en) 1999-03-04
EP0628783B1 (en) 1998-08-12
FR2706200A1 (en) 1994-12-16

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