FR3060528B1 - DEVICE FOR CONTROLLING MOBILE SURFACES AND A WHEEL DIRECTOR OF AN AIRCRAFT - Google Patents

DEVICE FOR CONTROLLING MOBILE SURFACES AND A WHEEL DIRECTOR OF AN AIRCRAFT Download PDF

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Publication number
FR3060528B1
FR3060528B1 FR1662695A FR1662695A FR3060528B1 FR 3060528 B1 FR3060528 B1 FR 3060528B1 FR 1662695 A FR1662695 A FR 1662695A FR 1662695 A FR1662695 A FR 1662695A FR 3060528 B1 FR3060528 B1 FR 3060528B1
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FR
France
Prior art keywords
aircraft
actuator
controlling mobile
control
mobile surfaces
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.)
Active
Application number
FR1662695A
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French (fr)
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FR3060528A1 (en
Inventor
Pascal Coppee
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.)
Safran Electronics and Defense SAS
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Safran Electronics and Defense 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 Safran Electronics and Defense SAS filed Critical Safran Electronics and Defense SAS
Priority to FR1662695A priority Critical patent/FR3060528B1/en
Publication of FR3060528A1 publication Critical patent/FR3060528A1/en
Application granted granted Critical
Publication of FR3060528B1 publication Critical patent/FR3060528B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50—Steerable undercarriages; Shimmy-damping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/405—Powered wheels, e.g. for taxing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

Dispositif de commande (1) d'un aéronef (100) pourvu de surfaces mobiles de vol (103, 104, 111, 112) et une roue directrice (121), comprenant : - un manche de pilotage (2) ; - un calculateur de commande (3) pourvu des moyens de sa liaison (4) à un actionneur (105, 106, 113, 114) d'au moins une des surfaces mobiles de vol (103, 104, 111, 112) et à au moins un actionneur d'orientation (122) de la roue directrice (121), le calculateur de commande (3) étant agencé pour : - piloter l'actionneur d'orientation (122) de la roue directrice (121) lors de la phase de roulage ; - piloter l'actionneur (105, 106, 113, 114) de la au moins une surface mobile de vol (103, 104, 111, 112) lors de la phase de vol. Aéronef (100) comportant un tel dispositif de commandeControl device (1) of an aircraft (100) provided with movable flight surfaces (103, 104, 111, 112) and a steering wheel (121), comprising: - a control stick (2); - a control computer (3) provided with the means for its connection (4) to an actuator (105, 106, 113, 114) of at least one of the mobile flight surfaces (103, 104, 111, 112) and to at least one orientation actuator (122) of the steered wheel (121), the control computer (3) being arranged to: - control the orientation actuator (122) of the steered wheel (121) during the taxiing phase; - Controlling the actuator (105, 106, 113, 114) of the at least one mobile flight surface (103, 104, 111, 112) during the flight phase. Aircraft (100) comprising such a control device

FR1662695A 2016-12-16 2016-12-16 DEVICE FOR CONTROLLING MOBILE SURFACES AND A WHEEL DIRECTOR OF AN AIRCRAFT Active FR3060528B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1662695A FR3060528B1 (en) 2016-12-16 2016-12-16 DEVICE FOR CONTROLLING MOBILE SURFACES AND A WHEEL DIRECTOR OF AN AIRCRAFT

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1662695 2016-12-16
FR1662695A FR3060528B1 (en) 2016-12-16 2016-12-16 DEVICE FOR CONTROLLING MOBILE SURFACES AND A WHEEL DIRECTOR OF AN AIRCRAFT

Publications (2)

Publication Number Publication Date
FR3060528A1 FR3060528A1 (en) 2018-06-22
FR3060528B1 true FR3060528B1 (en) 2018-12-07

Family

ID=58010066

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1662695A Active FR3060528B1 (en) 2016-12-16 2016-12-16 DEVICE FOR CONTROLLING MOBILE SURFACES AND A WHEEL DIRECTOR OF AN AIRCRAFT

Country Status (1)

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FR (1) FR3060528B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2596290C (en) * 2020-06-22 2023-09-20 L Univ Ta Malta A method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1158219A (en) * 1980-04-01 1983-12-06 Edmond D. Diamond Multi-axis force stick, self-trimmed aircraft flight control system
US6671588B2 (en) * 2001-12-27 2003-12-30 Toyota Jidosha Kabushiki Kaisha System and method for controlling traveling direction of aircraft
FR2903658B1 (en) * 2006-07-12 2008-09-26 Airbus France Sas FLY CONTROL AND FLY CONTROL SYSTEM FOR AIRCRAFT.
DE102008011791B4 (en) * 2008-02-29 2013-09-19 Airbus Operations Gmbh Integrated multifunctional wheel drive system for aircraft

Also Published As

Publication number Publication date
FR3060528A1 (en) 2018-06-22

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