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.
RUDDER SYSTEM ARCHITECTURE FOR ELECTRICAL ACTUATORS
2022-01-13
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
2012-3244 Improving Rudder Effectiveness with Sweeping Jet Actuators
British Library Conference Proceedings | 2012
|