Device and method for monitoring a disk brake system of an aircraft landing gear

Abstract

An assembly of a disk brake system (2) of an aircraft landing gear (I) and a monitoring device (3), the disk brake system (2) comprising at least one stator disk (21) and at least one rotor disk (22) configured to be pressed against said stator disk (21), the monitoring device (3) comprising a tape (30), the tape (30) comprising at least one visual information item associated with a predetermined circumferential range of the stator disk (21), the tape (30) being positioned in contact with the circumference of the stator disk (21), a first gripping member (31) attached to a first end of the tape (30) and a second gripping member (32) attached to a second end of the tape (30) so as to make it possible to stretch the tape around the circumference of the stator disk (21) in order to accurately determine the circumference of the stator disk (21).

Dependencies are inferred from the claim text.