Control electronics 4 can connect or connects electric motor 3 to an electrical or electronic load R and/or the control electronics can deactivate or deactivates DC/DC converter 1 supplying electrical power to the electric motor, and to an electromechanical actuator. The control electronics may detect a counter voltage of the electric motor. The control electronics may only be supplied with a counter voltage of the electric motor or no voltage. The control electronics can be activated in the event of an electrical failure or in the loss of a supply voltage. The control electronics may be part of a low voltage system. The control electronics may be used to damp the movement of an electromechanical actuator of an aircraft primary flight control system.
Control electronics, electromechanical actuator, aircraft and method for damping the movement of an electromechanical actuator
2023-11-29
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2023
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