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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Bibliographic Details
Main Authors GEORGIN, Marc J, POISSON, Richard A
Format Patent
LanguageEnglish
French
German
Published 10.04.2024
Subjects
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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Summary: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).
Bibliography:Application Number: EP20230181902