Abstract:
The actuator is of the roto-linear type and comprises a sleeve (4), a clevis (1) and an operating rod (2) which transmits the load. An electromagnetic sensor (10) that measures and controls the load is placed inside the actuator, at the shoulder (6) of the clevis (1). This sensor is associated with measurement means for processing the signals from the said windings, which windings are torus-shaped and arranged inside a field frame (12) which is magnetically closed by an armature (13).
Abstract:
The invention relates to a damping circuit for a synchronous servomotor including at least one winding, wherein the circuit comprises at least one main damping resistor, a means for coupling the main damping resistor in series to the winding, and at least one additional damping cell comprising at least one additional damping resistor connected in parallel to the main damping resistor via a static switch coupled to a module for controlling the switch on the basis of a winding voltage. The control module includes, in parallel with the main damping resistor, a shunt having an output connected to the control input of the switch and a divider bridge connected to the shunt so as to form a comparator for comparing the winding voltage with the conduction voltage of the shunt.
Abstract:
The electric motor consists of a rotor (7) fitted with permanent magnets (12) and comprises a stator (11) the armature of which is made up of two parts: a stack of laminations forming round teeth (14) and a solid tube-shaped field frame (15) made of a material of the stainless steel kind enveloping the said stack of laminations. This armature constitutes a non-disengageable braking system that produces a damping effect in the face of possible movements of its rotor (7) which are brought about and/or imposed by the members with which it collaborates. This motor can be used for driving a roto-linear actuator device with satellite rollers which is used as an actuator for manoeuvring the control surfaces of an aircraft, for example an aileron.
Abstract:
An actuator comprising at least one multiphase motor (100) having phases (101) facing a rotor (102) secured to an outlet shaft associated with a braking member (2) and provided with means for connecting it to a movable element that is to be moved, the motors and the braking member being connected to at least one motor control unit (5) for controlling the motors by powering their phases. The motor has at least four phases wound in such a manner as to avoid a neutral point, and in that the control unit has one single-phase inverter per phase and is arranged to implement a nominal, three-phase mode of control, and a degraded mode of control that enables the rotor to be driven in rotation by powering two non-collinear phases thereof.