公开(公告)号：US20230318513A1

公开(公告)日：2023-10-05

申请号：US18130139

申请日：2023-04-03

申请人： Liebherr-Aerospace Lindenberg GmbH

发明人： Frank KRONBURGER ,  Jilian KINZELMANN

IPC分类号： H02P29/04 ,  B64C13/50

CPC分类号： H02P29/04 ,  B64C13/50

摘要： 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.

公开(公告)号：US20190047723A1

公开(公告)日：2019-02-14

申请号：US16079175

申请日：2017-02-22

申请人： Liebherr-Aerospace Lindenberg GmbH

发明人： Rainer MIELZAREK ,  Frank KRONBURGER

IPC分类号： B64D43/00 ,  B64C13/50 ,  G06F13/40 ,  H04L12/40

摘要： The invention relates to an aircraft comprising at least one component and at least one electronic device for controlling the component, wherein the electronic device has at least one interface by means of which signals can be provided for controlling the component, wherein the electronic device has a combination of at least one micro-controller and at least one FPGA core, which are connected to one another via a communication connection, wherein the FPGA core can be configured such that signals can be processed that are each different from one another according to the configuration of the FPGA core.