A friction clutch having an electromagnet assembly including a coil and a magnet connected to the coil. When the coil is energised, a magnetic field is generated and passes through the magnet and a magnetisable conductive body adjacent to the magnet, such that a displaceable magnetisable armature portion can be brought from one position into another position. The coil has a plurality of outer portions each having an associated outer dimension of the outer portion. The magnet completely covers an outer portion of the coil by a magnet side. Two further outer portions of the coil are not covered by the magnet or are not covered by more than 20% of an outer dimension of the further outer portion, or wherein, in the case a single further outer portion covered by the magnet, the outer portion is not covered by more than 70%.

A braking assembly for a strain wave gearing of a surgical robotic manipulator, the braking assembly including a first braking member fixedly coupled to an input portion of a strain wave gearing of a surgical robotic manipulator; and a second braking member fixedly coupled to an output portion of the strain wave gearing, and wherein during a braking operation the first braking member contacts the second braking member to mechanically brake the input portion to the output portion.

A braking assembly for a strain wave gearing of a surgical robotic manipulator, the braking assembly including a first braking member fixedly coupled to an input portion of a strain wave gearing of a surgical robotic manipulator; and a second braking member fixedly coupled to an output portion of the strain wave gearing, and wherein during a braking operation the first braking member contacts the second braking member to mechanically brake the input portion to the output portion.

An axially oriented, two-position linear actuator includes a fixed stator having a single stator coil and a linear movable translator. The linear actuator is oriented axially in that the stator and the translator are axially offset from one another and the translator is axially movable between first and second end positions toward and away from the stator. For the translator to move between the end positions, the stator coil attracts or repels the translator depending on the polarity of the electrical current of the stator coil. The linear actuator may be part of a clutch assembly, such as a dynamically controllable clutch, for use in controlling coupling members of the clutch assembly.

An electromagnetic friction disk clutch with a shaft, an electromagnet arrangement, a rotor for driving the shaft, and an armature disk which is connected to the shaft and moveable in a sprung manner in a direction which is axial to a shaft axis. In a shifting state of the friction disk clutch, the armature disk can be connected to the rotor in a frictionally locking manner, the rotor being mounted rotationally by a rotor bearing unit with respect to the housing section and with respect to the shaft, a magnetic effect is generated for connecting the armature disk to the rotor. The rotor bearing unit is offset with respect to the electromagnet arrangement in an axial direction with respect to the shaft, and overlaps the electromagnet arrangement in the axial direction with respect to the shaft.

An electronic locking differential includes a lock ring and a coil that moves the lock ring to engage gears of the electronic locking differential, an energy storage capacitor that powers the coil during at least a portion of engagement of the lock ring with the gears, and a controller. The controller charges the energy storage capacitor to a first predefined voltage prior to the engagement.

A method for manufacturing a laminated iron core includes providing a plurality of annular iron core piece rows, each of which is configured by annularly arranging a plurality of divided iron core pieces including yokes and teeth, and the yokes of the annularly-adjacent divided iron core pieces in the annular iron core piece row are mutually different in shape. In the method, the annular iron core piece rows are laminated by changing a rotational angle of the newly laminated annular iron core piece row relatively to the lastly laminated annular iron core piece row laminated so that the divided iron core piece with a shape different from that of the divided iron core piece is laminated on the lastly laminated divided iron core piece.

An actuation system for an aircraft can include an actuator and a plurality of clutches connected to and structured to be moved by the actuator. The actuation system can include a plurality of control levers connected to the plurality of clutches and structured to be moved by the plurality of clutches when the plurality of clutches are moved by the actuator. The actuation system can include a processor connected to the actuator and to the plurality of clutches. The processor can identify one or more clutches connected to one or more control levers of the plurality of control levers for controlling an operation of the aircraft, and cause the one or more clutches connected to the one or more control levers to be in an engaged stat. The processor can activate the actuator to cause movement of the one or more control levers via the one or more clutches.

An actuation system for an aircraft can include an actuator and a plurality of clutches connected to and structured to be moved by the actuator. The actuation system can include a plurality of control levers connected to the plurality of clutches and structured to be moved by the plurality of clutches when the plurality of clutches are moved by the actuator. The actuation system can include a processor connected to the actuator and to the plurality of clutches. The processor can identify one or more clutches connected to one or more control levers of the plurality of control levers for controlling an operation of the aircraft, and cause the one or more clutches connected to the one or more control levers to be in an engaged stat. The processor can activate the actuator to cause movement of the one or more control levers via the one or more clutches.

The present document relates to a method of disengaging a clutching device. The method comprises sweeping an output torque of an electric motor drivingly connected to the clutching device such that a torque transmitted by the clutching device vanishes at least temporarily during the sweep, and disengaging the clutching device during the sweep. The present document further relates to an electric driveline for carrying out the method.