FR3110126B1 - Electrical power distribution equipment for aircraft braking and taxiing system and aircraft braking and taxiing system - Google Patents

Electrical power distribution equipment for aircraft braking and taxiing system and aircraft braking and taxiing system Download PDF

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Publication number
FR3110126B1
FR3110126B1 FR2004799A FR2004799A FR3110126B1 FR 3110126 B1 FR3110126 B1 FR 3110126B1 FR 2004799 A FR2004799 A FR 2004799A FR 2004799 A FR2004799 A FR 2004799A FR 3110126 B1 FR3110126 B1 FR 3110126B1
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FR
France
Prior art keywords
aircraft braking
taxiing system
electrical power
power distribution
distribution equipment
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
FR2004799A
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French (fr)
Other versions
FR3110126A1 (en
Inventor
Brian Goyez
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 Landing Systems SAS
Original Assignee
Safran Landing Systems 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 Landing Systems SAS filed Critical Safran Landing Systems SAS
Priority to FR2004799A priority Critical patent/FR3110126B1/en
Publication of FR3110126A1 publication Critical patent/FR3110126A1/en
Application granted granted Critical
Publication of FR3110126B1 publication Critical patent/FR3110126B1/en
Active legal-status Critical Current
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
    • B60T8/17—Using electrical or electronic regulation means to control braking
    • B60T8/1701—Braking or traction control means specially adapted for particular types of vehicles
    • B60T8/1703—Braking or traction control means specially adapted for particular types of vehicles for aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T2270/00—Further aspects of brake control systems not otherwise provided for
    • B60T2270/40—Failsafe aspects of brake control systems
    • B60T2270/414—Power supply failure
    • 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

Abstract

Equipement électrique de distribution de puissance (1), agencé pour relier une pluralité de sources de puissance (50, 60, 70) à un système de freinage (80) et à un système de taxiage (90) d’un aéronef pour les alimenter électriquement, comprenant des ports d’entrée (3, 4) destinés à être reliés à une source de puissance (50, 60, 70), un premier port de sortie (6) destiné à être relié au système de freinage (80) et un deuxième port de sortie (7) destiné à être relié au système de taxiage (90) ainsi qu’ un troisième port d’entrée/sortie (5). Système (100) comprenant un tel équipement électrique de distribution de puissance. FIGURE DE L’ABREGE : Fig. 1Electrical power distribution equipment (1), arranged to connect a plurality of power sources (50, 60, 70) to a braking system (80) and to a taxiing system (90) of an aircraft in order to supply them electrically, comprising input ports (3, 4) intended to be connected to a power source (50, 60, 70), a first output port (6) intended to be connected to the braking system (80) and a second output port (7) intended to be connected to the taxiage system (90) as well as a third input/output port (5). A system (100) comprising such electrical power distribution equipment. FIGURE OF THE ABRIDGE: Fig. 1

FR2004799A 2020-05-14 2020-05-14 Electrical power distribution equipment for aircraft braking and taxiing system and aircraft braking and taxiing system Active FR3110126B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2004799A FR3110126B1 (en) 2020-05-14 2020-05-14 Electrical power distribution equipment for aircraft braking and taxiing system and aircraft braking and taxiing system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2004799A FR3110126B1 (en) 2020-05-14 2020-05-14 Electrical power distribution equipment for aircraft braking and taxiing system and aircraft braking and taxiing system
FR2004799 2020-05-14

Publications (2)

Publication Number Publication Date
FR3110126A1 FR3110126A1 (en) 2021-11-19
FR3110126B1 true FR3110126B1 (en) 2022-06-17

Family

ID=71784289

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2004799A Active FR3110126B1 (en) 2020-05-14 2020-05-14 Electrical power distribution equipment for aircraft braking and taxiing system and aircraft braking and taxiing system

Country Status (1)

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FR (1) FR3110126B1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6402259B2 (en) * 1999-07-14 2002-06-11 Goodrich Corporation Electromechanical braking system with power distribution and redundancy
FR2864024B1 (en) * 2003-12-22 2006-04-07 Messier Bugatti METHOD FOR MANAGING AN AIRCRAFT BRAKING SYSTEM ARCHITECTURE, AND BRAKING SYSTEM ARCHITECTURE USING THE SAME
US20080258548A1 (en) * 2007-04-18 2008-10-23 Bill May Aircraft brake control architecture having improved antiskid redundancy
FR3072924B1 (en) 2017-10-30 2019-10-25 Safran Landing Systems ELECTRICAL EQUIPMENT FOR CONNECTING TO AN ELECTROMECHANICAL BRAKING ACTUATOR AND A DRIVING ELECTROMECHANICAL ACTUATOR

Also Published As

Publication number Publication date
FR3110126A1 (en) 2021-11-19

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