Method and device for fault detection in the load path of a spindle actuator

A method and a device for fault detection in the load path of a spindle actuator which is provided for actuating a high-lift flap of an aircraft, wherein the spindle actuator has a redundant load path which is formed by a spindle and a secondary connection which are connected rotationally fixedly to...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BRUECKNER INA, GIEBELER CHRISTOPH, RECHTER HARALD, RECKSIEK MARTIN, HEINTJES MARK, CHRISTMANN MARKUS
Format:	Patent
Sprache:	eng
Schlagworte:	GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SURVEYING TESTING
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