Steuersystem

Details

Veröffentlichungs-Nr.

EP2415669

Aktenzeichen

EP10400037

Anmeldetag

4. August 2010

Veröffentlichung

13. Mai 2015

Erteilung

13. Mai 2015

Rechtsraum

EP

IPC

B64C27/56B64C13/42

Abstract

The invention relates to a control system and to a method of operating such a control system, particularly to a control system for pilot command inputs for a helicopter, with a mechanical input signal (2), at least one electric position sensor (21, 21') for said input signal (2), at least one electric power supply (25, 25') and at least one controllable, electromechanical actuator (27, 27') fed by the at least one electric power supply (25, 25') and controlled by the at least one electric position sensor (21, 21'). The mechanical input signal (2) is applied mechanically to the at least one controllable electromechanical actuator (27, 27').

Anmelder

Firmen

AIRBUS HELICOPTERS DEUTSCHLAND GmbH
EUROCOPTER DEUTSCHLAND GmbH

Land

🇩🇪 Deutschland

Fachgebiete