Liebherr-aerospace Lindenberg Gmbh

Philipp Kegel

Markus Bildstein

Christian Schilling

Klaus Schmelz

Georg Ried

Michael Koros

Albert Petretti

This present disclosure relates to a motor arrangement for controlling pilot valves having at least three motors, having at least one stator each and at least one rotor each, wherein the motors are provided at a common rotating shaft, with each motor being coupled to the rotating shaft via at least one respective mechanical coupling.

Redundant modular pivot angle motor

The present invention relates to an actuation device for the actuating of an adjustment surface of an aircraft such as an elevator, a rudder or the like, of landing gear or another aircraft or surface vehicle actuator, comprising an electrohydraulic actuator having a servo control cylinder, a pump for pressure fluid action on the servo control cylinder as well as an electric motor for the actuation of the pump, with the electric motor having a liquid cooling. In accordance with the invention, the actuation device is characterized in that a leak flow of the pump is guided over a leak passage through the electric motor to cool the electric motor.

Actuation device

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Heimenkirch, Germany

Philipp Kegel