System, aircraft and procedure

DE102025101761A1Undetermined Publication Date: 2026-07-23LIEBHERR AEROSPACE LINDENBERG GMBH
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Patent Information

Application Number
DE102025101761
Authority / Receiving Office
DE · DE
Patent Type
Applications
Current Assignee / Owner
Filing Date
2025-01-20
Publication Date
2026-07-23

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Abstract

The present invention relates to a system for controlling a component of an aircraft, comprising an actuator for controlling the component, a servo unit configured to control the actuator, and a control unit configured to control the servo unit, wherein the actuator has one or more sensors, each for detecting a state of the actuator, and wherein the control unit is configured to control and / or regulate the servo unit based on the state detected by the sensor or on the basis of the states of the actuator detected by the sensors.
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Citation Information

Patent Citations

  • Flight control system with a hydraulic servo actuator

    DE102020129344A1

  • A flight control method for rotorcraft, and a rotorcraft

    EP3336649A1

  • Electro-hydraulic servovalve control with input

    EP4100807B1