Systems and methods for aircraft electric taxi brake optimization are provided. The system may comprise an aircraft (10) having a landing gear (12, 14, 16) comprising a wheel (13A, 13B, 15A, 15B, 17A, 17B), a friction brake having a brake material coupled to the wheel (13A, 13B, 15A, 15B, 17A, 17B), a regenerative brake comprising a reversible taxi motor coupled to the wheel (13A, 13B, 15A, 15B, 17A, 17B), a sensor (202) 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 (204), the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller (204), cause the controller to perform operations comprising: receiving, by the controller, a command signal and the friction brake temperature and calculating, by the controller (204), a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal.
SYSTEM AND METHOD FOR AIRCRAFT ELECTRIC TAXI BRAKE OPTIMIZATION
SYSTEM UND VERFAHREN ZUR OPTIMIERUNG DER ELEKTRISCHEN ROLLBREMSE EINES LUFTFAHRZEUGS
SYSTÈME ET PROCÉDÉ D'OPTIMISATION DU FREINAGE ÉLECTRIQUE PENDANT LE TAXI D'UN AVION
2020-05-13
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
SYSTEM AND METHOD FOR AIRCRAFT ELECTRIC TAXI BRAKE OPTIMIZATION
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