VERFAHREN ZUM VERWALTUNG EINER ARCHITEKTUR EINES ELEKTROMECHANISCHEN FLUGZEUGBREMSSYSTEMS SOWIE BREMSSYSTEMSARCHITEKTUR

The method involves controlling an electromechanical actuator (EMA) that is not connected to a battery assembly to exert a force equal to a unitary maintenance force that is determined independently of a braking request of a pilot. The unitary maintenance force is a predetermined force and is calcul...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: DELLAC, STEPHANE, SIBRE, JEROME, GIROD, PIERRE
Format: Patent
Sprache:ger
Schlagworte:
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Beschreibung
Zusammenfassung:The method involves controlling an electromechanical actuator (EMA) that is not connected to a battery assembly to exert a force equal to a unitary maintenance force that is determined independently of a braking request of a pilot. The unitary maintenance force is a predetermined force and is calculated based on thrust of aircraft engines. An independent claim is also included for braking system architecture to implement a method of controlling the architecture.