FR3026718B1 - Systeme de roulage d'un aeronef. - Google Patents

Systeme de roulage d'un aeronef. Download PDF

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Publication number
FR3026718B1
FR3026718B1 FR1459459A FR1459459A FR3026718B1 FR 3026718 B1 FR3026718 B1 FR 3026718B1 FR 1459459 A FR1459459 A FR 1459459A FR 1459459 A FR1459459 A FR 1459459A FR 3026718 B1 FR3026718 B1 FR 3026718B1
Authority
FR
France
Prior art keywords
aircraft
running
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
FR1459459A
Other languages
English (en)
Other versions
FR3026718A1 (fr
Inventor
Philippe TATRY
Yann Nicolas
Matthieu Bradier
Nicolas Sanz
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 Operations SAS
Airbus SAS
Original Assignee
Airbus Operations SAS
Airbus 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 Operations SAS, Airbus SAS filed Critical Airbus Operations SAS
Priority to FR1459459A priority Critical patent/FR3026718B1/fr
Priority to US14/865,924 priority patent/US9815550B2/en
Publication of FR3026718A1 publication Critical patent/FR3026718A1/fr
Application granted granted Critical
Publication of FR3026718B1 publication Critical patent/FR3026718B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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 
    • B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface  wheeled type, e.g. multi-wheeled bogies
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P3/00—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters
    • H02P3/06—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters for stopping or slowing an individual dynamo-electric motor or dynamo-electric converter
    • H02P3/08—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters for stopping or slowing an individual dynamo-electric motor or dynamo-electric converter for stopping or slowing a dc motor
    • H02P3/12—Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters for stopping or slowing an individual dynamo-electric motor or dynamo-electric converter for stopping or slowing a dc motor by short-circuit or resistive braking
    • 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 
    • B64C25/42—Arrangement or adaptation of brakes
    • 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)
  • Power Engineering (AREA)
  • Fluid-Damping Devices (AREA)
  • Laminated Bodies (AREA)
FR1459459A 2014-10-03 2014-10-03 Systeme de roulage d'un aeronef. Active FR3026718B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1459459A FR3026718B1 (fr) 2014-10-03 2014-10-03 Systeme de roulage d'un aeronef.
US14/865,924 US9815550B2 (en) 2014-10-03 2015-09-25 Aircraft taxiing system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1459459 2014-10-03
FR1459459A FR3026718B1 (fr) 2014-10-03 2014-10-03 Systeme de roulage d'un aeronef.

Publications (2)

Publication Number Publication Date
FR3026718A1 FR3026718A1 (fr) 2016-04-08
FR3026718B1 true FR3026718B1 (fr) 2018-03-02

Family

ID=51866278

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1459459A Active FR3026718B1 (fr) 2014-10-03 2014-10-03 Systeme de roulage d'un aeronef.

Country Status (2)

Country Link
US (1) US9815550B2 (fr)
FR (1) FR3026718B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10940941B2 (en) * 2014-12-04 2021-03-09 Borealis Technical Limited Method for increasing aircraft effective value

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7237748B2 (en) * 2003-12-15 2007-07-03 Delos Aerospace, Llc Landing gear method and apparatus for braking and maneuvering
TW200532422A (en) * 2004-03-16 2005-10-01 Ind Tech Res Inst Thermal module with heat reservoir and method of applying the same on electronic products
US20070284939A1 (en) * 2006-06-12 2007-12-13 Honeywell International Aircraft electric brake and generator therefor
KR101058102B1 (ko) * 2009-12-18 2011-08-24 에스비리모티브 주식회사 배터리 팩
FR2975376B1 (fr) * 2011-05-20 2018-03-30 Safran Landing Systems Procede pour alimenter des moteurs de deplacement autonome d'un aeronef.
FR2997172A1 (fr) * 2012-10-23 2014-04-25 Airbus Operations Sas Convertisseur thermo-electrique
FR3003235B1 (fr) * 2013-03-12 2015-04-10 Messier Bugatti Dowty Dispositif multifonctions pour atterriseurs.

Also Published As

Publication number Publication date
US9815550B2 (en) 2017-11-14
FR3026718A1 (fr) 2016-04-08
US20160096618A1 (en) 2016-04-07

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