ARCHITECTURE OF AN AIRCRAFT BRAKING SYSTEM

ARCHITECTURE OF AN AIRCRAFT BRAKING SYSTEM

Architecture of an aircraft braking system having a brake (20) comprising a plurality of electromechanical actuators (25), with each electromechanical actuator (25) comprising a power module and a digital communication module (26). The brake digital communication modules are interconnected to form a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: GOYEZ, Brian, COUSTENOBLE, Steve, EVENOR, Eric, ONFROY, Dominique
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL
AVIATION
BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES
TRANSPORTING
VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF
VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:Architecture of an aircraft braking system having a brake (20) comprising a plurality of electromechanical actuators (25), with each electromechanical actuator (25) comprising a power module and a digital communication module (26). The brake digital communication modules are interconnected to form a digital network (30). The system also has two control units (22a, 22b) adapted for generating digital signals for controlling electric motors and one network interconnection member (23) connected to two control units and incorporated in the digital network for distributing the digital control signals to the digital communication modules via the digital network.