The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 21, 2025

Filed:

Feb. 24, 2022
Applicant:

Safran Landing Systems, Velizy-Villacoublay, FR;

Inventors:

Nadia Bour, Moissy-Cramayel, FR;

Alexandre Biava, Moissy-Cramayel, FR;

Didier Da Costa, Moissy-Cramayel, FR;

Assignee:

SAFRAN LANDING SYSTEMS, Velizy-Villacoublay, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01B 5/02 (2006.01); B64C 25/42 (2006.01);
U.S. Cl.
CPC ...
G01B 5/025 (2013.01); B64C 25/42 (2013.01);
Abstract

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


Find Patent Forward Citations

Loading…