A system for dissipating regenerated electric energy produced by an electric actuator of an aircraft, the dissipating system including: a resistor; two switching arms, each switching arm being connected in series with the resistor, the two switching arms being connected together in parallel, each switching arm including two switches connected to one another in series, each switch including two terminals and a control grid, each switch being capable of being controlled by controlling the potential applied to the control grid thereof; and a measurement system capable of measuring the voltage at the terminals of each switch.
SYSTÈME ET PROCÉD'E DE DISSIPATION DE L'ÉNERGIE ÉLECTRIQUE RÉGÉNERÉE PAR DES ACTIONNEURS
SYSTEM AND METHOD FOR DISSIPATING ELECTRIC ENERGY REGENERATED BY ACTUATORS
SYSTEM UND VERFAHREN ZUR ABLEITUNG VON DURCH AKTUATOREN REGENERIERTER ELEKTRISCHER ENERGIE
2020-11-11
Patent
Elektronische Ressource
Französisch
IPC: | H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen |
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