About 31 results
https://drivepatents.com/patents/941395 · 22 Jun 2016
The invention relates to a braking actuator for an aircraft hydraulic brake, intended to be received in one of the cavities of a brake crown, the actuator comprising: - a sleeve (1) adapted to be received with sealing in the cavity of the crown; - a piston...
https://drivepatents.com/patents/945262 · 30 Mar 2016
The invention relates to an aircraft landing gear comprising an axle (3) intended to receive a wheel (4) comprising a rim (6) mounted to rotate on the axle (3) by means of at least one bearing (8), said bearing (8) comprising an inner ring (11) mounted aro...
https://drivepatents.com/patents/946232 · 10 Feb 2016
The invention relates to a method for driving an aircraft wheel in rotation, the wheel being equipped with a rim comprising two half-rims assembled by bolts (5), in which a drive member is controlled to generate a driving torque for the wheel, characterize...
https://drivepatents.com/patents/947784 · 9 Dec 2015
Method for managing braking of a wheel (4) of an aircraft (1) equipped with a brake (11), the aircraft comprising brake control means adapted to implement an anti-skid function of the wheel (4) requiring an estimation of a rotational speed of the wheel, th...
https://drivepatents.com/patents/955537 · 18 Nov 2015
The invention relates to an electromechanical brake actuator for an aircraft wheel, comprising an electric motor (2) with a stator (3) and a rotor (4), a screw/nut assembly in which one of the elements is driven in rotation by the motor and the other eleme...
https://drivepatents.com/patents/948648 · 30 Sep 2015
The invention relates to an aircraft wheel comprising a rim and a tire (20) received on the rim, the rim comprising two parts (1; 2) assembled together by means of assembly bolts (5), one of the parts comprising a housing (3) in which a sealing gasket (4) ...
https://drivepatents.com/patents/958501 · 5 Aug 2015
The invention relates to a method for monitoring at least two electromechanical actuators (5) for aircraft wheel braking, comprising, for each electromechanical actuator (5), the steps of: - determining a current value representative of the supply current ...
https://drivepatents.com/patents/950047 · 15 Jul 2015
Method for monitoring a locking member (12) of an electromechanical actuator (1), the monitoring method comprising the steps of: - determining a representative value of a supply current of a motor (11) during an idle operating phase of the electromechanica...
https://drivepatents.com/patents/959424 · 1 Jul 2015
Aircraft wheel rim in two parts, one main part (1) comprising a hub (2), a web (4) extending between the hub and an annular external portion (3) intended to receive a tire and shaped to present a bead (5) at one of its ends, the other of its ends being sha...
https://drivepatents.com/patents/950601 · 27 May 2015
The invention relates to an electromechanical actuator for a vehicle brake comprising a body (4) in which are arranged an electric motor (5) and a threaded pusher cooperating by means of a helical connection with a nut (8) driven in rotation by the electri...