ES548100A0 - Dispositivo para el mando automatico de un compensador aero-dinamico unido a una superficie aerodinamica de mando de un aeronave - Google Patents

Dispositivo para el mando automatico de un compensador aero-dinamico unido a una superficie aerodinamica de mando de un aeronave

Info

Publication number
ES548100A0
ES548100A0 ES548100A ES548100A ES548100A0 ES 548100 A0 ES548100 A0 ES 548100A0 ES 548100 A ES548100 A ES 548100A ES 548100 A ES548100 A ES 548100A ES 548100 A0 ES548100 A0 ES 548100A0
Authority
ES
Spain
Prior art keywords
aerodynamic
aircraft
control
compensator attached
automatic control
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.)
Granted
Application number
ES548100A
Other languages
English (en)
Other versions
ES8703373A1 (es
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
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Publication of ES8703373A1 publication Critical patent/ES8703373A1/es
Publication of ES548100A0 publication Critical patent/ES548100A0/es
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Retarders (AREA)
  • Toys (AREA)
ES548100A 1984-10-02 1985-09-30 Dispositivo para el mando automatico de un compensador aero-dinamico unido a una superficie aerodinamica de mando de un aeronave Expired ES8703373A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8415123A FR2571021B1 (fr) 1984-10-02 1984-10-02 Dispositif pour la commande automatique d'un compensateur aerodynamique associe a une surface aerodynamique de commande d'un aeronef

Publications (2)

Publication Number Publication Date
ES8703373A1 ES8703373A1 (es) 1987-02-16
ES548100A0 true ES548100A0 (es) 1987-02-16

Family

ID=9308273

Family Applications (1)

Application Number Title Priority Date Filing Date
ES548100A Expired ES8703373A1 (es) 1984-10-02 1985-09-30 Dispositivo para el mando automatico de un compensador aero-dinamico unido a una superficie aerodinamica de mando de un aeronave

Country Status (4)

Country Link
DE (1) DE3534611A1 (es)
ES (1) ES8703373A1 (es)
FR (1) FR2571021B1 (es)
GB (1) GB2164905B (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2069498B1 (es) * 1993-09-24 1995-12-16 Alfranca Isidro Sierra Nuevo alimento para rumiantes a base de elementos fibrosos y pienso compuesto y procedimiento para su correspondiente instalacion para su reparacion.
FR2737698B1 (fr) * 1995-08-08 1997-10-24 Aerospatiale Systeme pour commander une gouverne articulee sur une structure d'un vehicule
US6257528B1 (en) 1999-07-20 2001-07-10 The Boeing Company Vehicle control system and method employing control surface and geared tab
EP2805879B1 (en) * 2013-05-22 2017-07-05 Airbus Operations GmbH Flap arrangement for a wing of an aircraft and an aircraft with a wing comprising such a flap arrangement
CN109515737B (zh) * 2018-03-16 2022-04-19 陕西飞机工业（集团）有限公司 一种飞机翼面配平装置
US11760472B2 (en) * 2020-12-01 2023-09-19 Textron Innovations Inc. Rudders for rotorcraft yaw control systems

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2174422A (en) * 1936-11-18 1939-09-26 Cons Aircraft Corp Flap control mechanism
US4431149A (en) * 1982-02-11 1984-02-14 The United States Of America As Represented By The Secretary Of The Air Force Geared tab
DE3371493D1 (en) * 1982-11-23 1987-06-19 British Aerospace Aircraft flying control systems

Also Published As

Publication number Publication date
FR2571021A1 (fr) 1986-04-04
ES8703373A1 (es) 1987-02-16
FR2571021B1 (fr) 1986-12-05
GB2164905A (en) 1986-04-03
GB8523633D0 (en) 1985-10-30
GB2164905B (en) 1987-10-21
DE3534611A1 (de) 1986-04-10

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19960603