A brake system for an aircraft is provided according to various embodiments. The system may include a left pedal arrangement comprising a left pedal (22), a first left sensor (30) to generate a first left signal in response to translation of the left pedal. The system also includes a right pedal arrangement comprising a right pedal (24), a first right sensor (30) to generate a first right signal in response to translation of the right pedal. Normal brake control logic (52) controls the brake system in response to a normal condition being set. The normal brake control logic commands a left brake based on the left signal, and a right brake based on the first right signal. Emergency brake control logic (54) controls the brake system in response to an emergency condition being set. The emergency brake control logic commands a same force to the left and right brakes based the left and right signals.
SYSTEMS AND METHODS FOR EMERGENCY AIRCRAFT BRAKE OPERATION
SYSTEME UND VERFAHREN ZUR NOTFALLFLUGZEUGBREMSENBETÄTIGUNG
SYSTÈMES ET PROCÉDÉS DE FONCTIONNEMENT D'UN FREIN D'URGENCE D'AÉRONEF
01.12.2021
Patent
Elektronische Ressource
Englisch
IPC: | B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF |
SYSTEMS AND METHODS FOR EMERGENCY AIRCRAFT BRAKE OPERATION
Europäisches Patentamt | 2018
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