ALTERNATE-SECONDARY SYSTEM IN PRESSURE CONTROL MODE FOR MINIMAL BRAKING DISRUPTION IN A PRIMARY-ALTERATE BRAKING SYSTEM

A method (300) of controlling an aircraft braking system (200) includes initiating (302) the aircraft braking system (200) by receiving (304) a first brake command at a primary system (320) to actuate braking via the primary system (320), receiving the first brake command at an alternate system (330...

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Bibliographische Detailangaben
Hauptverfasser:	GEORGIN, Marc J, POISSON, Richard A
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL 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:	A method (300) of controlling an aircraft braking system (200) includes initiating (302) the aircraft braking system (200) by receiving (304) a first brake command at a primary system (320) to actuate braking via the primary system (320), receiving the first brake command at an alternate system (330), and in response to the primary system (320) losing an ability to control a brake (240), controlling the braking of the brake (240) via the alternate system (330).