Abstract: Process for detecting the under-inflation of a tire of the landing gear of an aircraft in the course of taxiing, said landing gear being formed by at least one bogie comprising a beam provided with a pair of twin wheels at each of its ends provision is made of two bridge assemblies of four strain gauges disposed on each of the parts of the beam located between the median spindle for articulation of said beam to the leg and the corresponding pair of wheels, each bridge being supplied by its diagonal transverse to said beam, while the torsion signal is taken from the diagonal longitudinal with respect to the beam.

Abstract: System for braking a vehicle comprising an anti-skid device receiving speed data from a detector coupled to a non-braked wheel, wherein the system comprises a correction device comprising on the one hand first apparatus adapted to tramsmit to the anti-skid device the speed data each time that the variations of these data in time are lower than a deceleration threshold representative of the aquaplaning of the non-braked wheel, and, on the other hand, second apparatus adapted, each time that the variations of the velocity data are greater than the threshold, to transmit to the anti-skid device an estimated decreasing speed datum. The invention is more particularly applied to the braking of aircraft.

Abstract: The present invention relates to a method and device for controlling a hydraulic disc brake, particularly for heavy-transport aircraft, wherein the functioning of the brake is servo-controlled so that the braking torque which it exerts follows the variations of a predetermined reference torque.

Abstract: A braking system for an aircraft undercarriage with carbon disc brakes comprises apparatus responsive to the rotational speed of the wheels for regulating the rate of increase of braking pressure.