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|1. (WO2017148591) HIGH-LIFT SYSTEM|
|Applicants:||LIEBHERR-AEROSPACE LINDENBERG GMBH
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.