RUDDER SYSTEM ARCHITECTURE FOR ELECTRICAL ACTUATORS

RUDDER SYSTEM ARCHITECTURE FOR ELECTRICAL ACTUATORS

An electromechanical rudder system control using electromagnetic actuators provides dual redundancy to comply with safety demands. Diversity of possible interconnection distribution allows the manufacturer to choose the proper configuration to satisfy aircraft safety design, hardware savings and ove...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: GALVÃO, Marcelo, CAMPOS, Marcos Vinícius, FERREIRA, Daniel Paulo de Tarso
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:An electromechanical rudder system control using electromagnetic actuators provides dual redundancy to comply with safety demands. Diversity of possible interconnection distribution allows the manufacturer to choose the proper configuration to satisfy aircraft safety design, hardware savings and overall system quality improvements.