SYSTEM AND METHOD FOR AIRCRAFT ELECTRIC TAXI BRAKE OPTIMIZATION

Systems and methods for aircraft electric taxi brake optimization are provided. The system may comprise an aircraft having a landing gear comprising a wheel, a friction brake having a brake material coupled to the wheel, a regenerative brake comprising a reversible taxi motor coupled to the wheel, a...

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Bibliographische Detailangaben
Hauptverfasser:	Keller, Steven T, Kipp, Richard A
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL AVIATION BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	Systems and methods for aircraft electric taxi brake optimization are provided. The system may comprise an aircraft having a landing gear comprising a wheel, a friction brake having a brake material coupled to the wheel, a regenerative brake comprising a reversible taxi motor coupled to the wheel, a sensor configured to measure a wheel parameter of the wheel and a temperature of the friction brake, a tangible, non-transitory memory configured to communicate with a controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising: receiving, by the controller, a command signal and the friction brake temperature and calculating, by the controller, a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal.