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Patent Searching and Data


Title:
DEVICE AND METHOD FOR MONITORING A DISC BRAKE SYSTEM OF AN AIRCRAFT LANDING GEAR
Document Type and Number:
WIPO Patent Application WO/2022/189152
Kind Code:
A1
Abstract:
An assembly of a disc brake system (2) of an aircraft landing gear (1) and a monitoring device (3), the disc brake system (2) comprising at least one stator disc (21) and at least one rotor disc (22) configured to be pressed against said stator disc (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 disc (21), the tape (30) being positioned in contact with the circumference of the stator disc (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 disc (21) in order to accurately determine the circumference of the stator disc (21).

Inventors:
BOUR NADIA (FR)
BIAVA ALEXANDRE (FR)
DA COSTA DIDIER (FR)
Application Number:
PCT/EP2022/054588
Publication Date:
September 15, 2022
Filing Date:
February 24, 2022
Export Citation:
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Assignee:
SAFRAN LANDING SYSTEMS (FR)
International Classes:
F16D66/02; F16D55/36; G01B5/02
Domestic Patent References:
WO2019210971A12019-11-07
Foreign References:
US4441258A1984-04-10
EP3480485A12019-05-08
US2262664A1941-11-11
GB2106250A1983-04-07
AU6900574A1975-11-20
US8807290B22014-08-19
FR3070191A12019-02-22
Attorney, Agent or Firm:
ARGYMA (FR)
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