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AssigneeLiebherr-Aerospace Lindenberg GmbH
InventorsFrank KRONBURGER, Jilian KINZELMANN
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The present invention relates to control electronics, preferably for an electromechanical actuator, preferably for use in a primary flight control system of an aircraft, wherein the control electronics can connect or connects an electric motor, preferably of the electromechanical actuator, to an electrical or electronic load and/or wherein the control electronics can deactivate or deactivates a DC/DC converter supplying electrical power to the electric motor, and to an electromechanical actuator and to a method for damping the movement of an electromechanical actuator.
Control electronics, preferably for an electromechanical actuator, preferably for use in a primary flight control system of an aircraft, wherein the control electronics is configured to connect an electric motor, preferably of the electromechanical actuator, to an electrical or electronic load and/or in that the control electronics is configured to deactivate a DC/DC converter which supplies the electric motor with electrical power.
Dependencies are inferred from the claim text.