Aircraft braking device equipped with a sensor for measuring the braking torque of said device.
A removable mechanical fixation of a deformation sensor to a test body for aircraft braking systems addresses adhesive and temperature-related errors, enhancing measurement precision and maintenance in aircraft braking torque measurement.
FR3163052B1Active Publication Date: 2026-06-26SAFRAN LANDING SYSTEMS
Patent Information
- Authority / Receiving Office
- FR · FR
- Patent Type
- Patents
- Current Assignee / Owner
- SAFRAN LANDING SYSTEMS
- Filing Date
- 2024-06-06
- Publication Date
- 2026-06-26
Smart Images
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Abstract
An aircraft wheel braking device comprising at least one stack of rotor and stator discs, an actuator housing, an actuator mounted in the actuator housing to exert a pressing force on the disc stack, the actuator housing comprising a landing gear connection portion and an actuator receiving portion and being provided with a first deformation sensor. The first deformation sensor comprises a test body having a first end mechanically and removably fixed to the connection portion and a second end mechanically and removably fixed to the receiving portion, and a transducer fixed to the test body for measuring a deformation of the test body. Lander and aircraft comprising such a device. [Figure from the summary: Fig. 4]
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