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1. (WO2017148591) HIGH-LIFT SYSTEM

Pub. No.:    WO/2017/148591    International Application No.:    PCT/EP2017/000292
Publication Date: Sat Sep 09 01:59:59 CEST 2017 International Filing Date: Sat Mar 04 00:59:59 CET 2017
IPC: B64C 3/50
B64C 13/38
B64D 45/00
G01L 1/12
G01L 3/10
B64C 13/50
Applicants: LIEBHERR-AEROSPACE LINDENBERG GMBH
Inventors: KOHLÖFFEL, Christian
HOLZHAUSER, Philipp
BERGER, Lutz
TRENKLE, Christian
Title: HIGH-LIFT SYSTEM
Abstract:
The present invention relates to a high-lift system of an aircraft comprising flaps arranged on the wings of the aircraft, and also comprising a central drive and drive shafts, of which in each case one extends into one of the wings starting from the central drive, wherein each of the drive shafts is connected to drive stations which are driven by the drive shafts and which are connected to the flaps in order to move them, wherein load sensors are respectively arranged on each of the drive stations and at the output of the central drive unit, and wherein a computer unit is provided, which is connected to the load sensors and evaluates the signals of said load sensors, wherein the load sensors are torque sensors and/or force sensors.