768 results about "Rotary actuator" patented technology

An aircraft wing is disclosed having a fixed wing with a tip, and a wing tip device rotatably mounted on a hinge at the tip of the fixed wing, such that the wing tip device is rotatable about the hinge, and an actuation system for rotating the wing tip device about the hinge. The actuation system includes a motor, at least one geared rotary actuator, a reduction gearbox, a clutch for selectively decoupling rotation of the motor from rotation of the geared rotary actuator, the geared rotary actuator is driveable by the motor and arranged to convert rotary motion into a different rotary motion and is arranged to rotate the wing tip device relative to the tip of the fixed wing. The clutch is coupled to the geared rotary actuator by a shaft and the shaft is fixed in rotation to a mass disposed radially outwardly from the shaft.

A sonar transducer mount and aiming system for attachment to an electric trolling motor, which includes a rotary actuator assembly and a rotating shaft. The rotary actuator assembly includes a housing that is secured to the electric trolling motor and a rotating coupler is rotationally driven. The rotating shaft is connected to and rotates with the rotating coupler and includes a sonar transducer mounting point. The rotating shaft of the sonar transducer mount and aiming system and the electric trolling motor shaft have a common axis of rotation and are configured to rotate independently from one another about the common axis of rotation.

A sonar transducer mount and aiming system for attachment to an electric trolling motor, which includes a rotary actuator assembly and a rotating shaft. The rotary actuator assembly includes a housing that is secured to the electric trolling motor and a rotating coupler is rotationally driven. The rotating shaft is connected to and rotates with the rotating coupler and includes a sonar transducer mounting point. The rotating shaft has a tubular shape with a through bore that is configured to receive at least a portion of an electric trolling motor shaft in a co-axial arrangement. The size and shape of the through bore is designed so that the electric trolling motor shaft may be positioned within the through bore in clearance fit such that the rotating shaft of the sonar transducer mount and aiming system is free to rotate independently of the electric trolling motor shaft.

A pipe handler that can include a wrench assembly with a backup tong and a torque wrench, and a rotary actuator coupled to the torque wrench, wherein rotation of the rotary actuator about a second axis rotates the torque wrench about a first axis. An iron roughneck that can include a torque wrench configured to rotate about a first axis, and a rotary actuator coupled to the torque wrench, the rotary actuator having a second axis about which the rotary actuator rotates, where the second axis and the first axis are substantially parallel with each other and spaced apart from each other, and where rotation of the rotary actuator about the second axis rotates the torque wrench about the first axis.

A rotor assembly deployment mechanism configured to deploy a rotor assembly of a vertical take-off and landing aircraft from a horizontal, forward thrust, position to a vertical, hover, position. The rotor assembly deployment mechanism is configured to deploy an electric motor and propeller together. The deployment mechanism provides significant stiffness and strength with the use of torsion box constructions. The deployment mechanism may utilize bar linkages wherein the primary linkage pivot is of a large diameter relative to the span of the pivot in order to provide significant stiffness. The deployment mechanism may utilize rotary actuators to drive the deployment and stowing of the rotor assembly.

An intelligent parcel locker and methods for forming a package container in the parcel locker are provided. The parcel locker includes multiple front plates connected by multiple actuatable linking pins, a first single vane rotary actuator to dispense linked first side plates, a second single vane rotary actuator to dispense linked second side plates, a third single vane rotary actuator to dispense linked top plates, and a fourth single vane rotary actuator to dispense linked bottom plates. The parcel locker further includes a computing device connected to the multiple rotary actuators and the actuatable linking pins, receives a request to form the package container of a size to hold a package, generates command signals to actuate the rotary actuators to form the package container, and actuates the actuatable linking pins to form a front door of the package container.

A friction stir spot welding apparatus includes a pin member formed in a solid cylindrical shape, a shoulder member formed in a hollow cylindrical shape, the pin member being inserted in the shoulder member, a rotary actuator that rotates the pin member and the shoulder member on an axis that is in agreement with an axial center of the pin member, and a linear actuator that linearly moves each of the pin member and the shoulder member along the axis. A tip-end part of the shoulder member is formed in a tapered shape.

A drilling system configured to install a tap assembly into a ship skin is disclosed. The drilling system comprises a remotely-operated underwater vehicle and a drilling assembly configured to be operated by the remotely-operated underwater vehicle. The drilling assembly comprises a frame comprising an attachment element configured to hold the drilling assembly to a surface of the ship skin. The drilling assembly further comprises a drill actuation system comprising a linear actuator attached to the frame and a rotary actuator, wherein an actuation of the linear actuator is configured to move the rotary actuator relative to the frame to install the tap assembly into the ship skin by driving the tap assembly with the rotary actuator and the linear actuator.

Latch assemblies are provided with a paddle lever having an outwardly extending actuator flange and a rotary actuator plate which includes a fixed actuator pin extending outwardly from the actuator plate and adapted to being operatively engaged with the actuator flange of the paddle lever when manually moved into the unlatched condition thereof. At least one pair of arcuate spirally patterned and circumferentially separated cam slots are defined in the rotary actuator plate such that a latch pin associated with a latch bolt is operatively received within a selected one of the cam slots. Movement of the paddle lever from the latched condition into the unlatched condition thereof responsively engages the actuator flange with the actuator pin thereby causing rotation of the actuator plate about a rotary axis thereof and movement of the latch pin within the selected one of the cam slots whereby the latch pin is retracted to unlatch a moveable component from a fixed component.

An example hinged device flexible substrate testing system includes: a first plate comprising a first surface configured to hold stationary a first side of a hinged device under test; a second plate comprising a second surface configured to hold a second side of the hinged device under test; a first cam follower coupled to the second plate; a first drive arm configured to move the first cam follower to cause the second plate to rotate about a hinge pivot axis of the hinged device under test; an actuator configured to rotate the drive arm; and a load cell configured to measure loads on the first plate while the actuator moves the second plate.

A wing for an aircraft, including a main wing and a slat assembly including a slat and at least one connection assembly movably connecting the slat to the main wing, such that the slat is movable between a retracted position and at least one extended position, such that the connection assembly has an elongate slat track, and the front end of the slat track is mounted to the slat, such that the rear end and / or the intermediate portion of the slat track are mounted to the main wing by a roller or slide bearing such that the slat track is movable along the track longitudinal axis, such that the connection assembly has a drive unit configured for driving the slat track, such that the drive unit includes a rotary actuator having at least one drive arm rotatably driven about a rotation axis and drivingly engaging the slat track.

Wing deployment apparatus and methods are disclosed herein. An example wing deployment apparatus includes a rotary actuator coupled to a torque coupler having a locking key disposed in an opening. The locking key moves between an outer radial position and an inner radial position. A lead screw is rotationally coupled to the torque coupler. The lead screw has a first recess to accept the locking key when the locking key is in the inner radial position. A nut is threadably engaged to the lead screw and includes a second recess to accept the locking key when the locking key is in the outer radial position. The locking key prevents movement of the nut along the axis of rotation when the locking key is in the outer radial position. A wing is operatively coupled to the nut to move the wing to a deployed position.

Electrical connector assembly devices, systems, and methods including a demating device configured to separate a first connector and a second connector of an electrical connector assembly. The demating device includes a housing body, a drive assembly including: a drive lever, a trigger configured to push against the drive lever, a drive assembly rod, and a spring mounted around the drive assembly rod; and a demating assembly including: a movable plate having at least two sides, wherein each of the two sides includes at least two prongs; a stationary plate having at least two sides, wherein each of the two sides includes at least two prongs; and a rotary actuator configured to rotate the movable plate.

Expandable fusion devices, systems, instruments, and methods thereof. The expandable fusion implant may include an upper endplate assembly and a lower endplate assembly. The upper and lower endplate assemblies may be configured to expand in width. A rotatable actuator may move one or more driving ramps, which mate with an upper ramp and a lower ramp, respectively. The actuator may cause independent movement of one or more of the driving ramps, thereby causing an expansion in height of the upper and lower endplate assemblies.

A device and a method for actuating a joint of a human, an animal or a robot are disclosed. An elongated, lengthwise flexible and torsionally elastic body is provided for transmitting torque. Based at least in part on torsional deformation information of the body, torque is transmitted via the body. In an embodiment, a flexible drive shaft is provided, whereby the flexible drive shaft comprises said body. Furthermore, use of a flexible drive shaft as compliant element and as torque transmission element in a rotary actuator for actuating a mechanical joint is disclosed. In addition, use of a flexible drive shaft for determining an impedance of a joint of a human or an animal is also disclosed.

A rotary actuator includes a housing having a first end and a second end spaced from the first end along an axis. The housing defines a cavity extending circumferentially about the axis. An output shaft is arranged coaxially with the axis. The output shaft extends outwardly from the cavity through the first end. A drive system is disposed in the cavity and axially spaced from the first end. A gearbox is disposed in the cavity between the output shaft and the drive system. The gearbox is coupled to the drive system and the output shaft. A rotational controller is disposed in the cavity between the drive system and the second end. The rotational controller is configured to actuate the drive system to adjust an angular position of the output shaft.

Wing deployment apparatus and methods are disclosed herein. An example wing deployment apparatus includes a rotary actuator coupled to a torque coupler having a locking key disposed in an opening. The locking key moves between an outer radial position and an inner radial position. A lead screw is rotationally coupled to the torque coupler. The lead screw has a first recess to accept the locking key when the locking key is in the inner radial position. A nut is threadably engaged to the lead screw and includes a second recess to accept the locking key when the locking key is in the outer radial position. The locking key prevents movement of the nut along the axis of rotation when the locking key is in the outer radial position. A wing is operatively coupled to the nut to move the wing to a deployed position.

The present disclosure is directed to a multifunctional tailgate door and cargo load system that includes a multidirectional bumper apparatus with adaptable tow hitch receiver. The multifunctional tailgate door is adjacent to a cargo bed area having a rail system attached to the multifunctional tailgate door. The rail system having a linear actuator includes a rotary actuator hinge that enables the multifunctional tailgate door to function in a first direction and in a second direction. The multidirectional bumper apparatus is operable in a first direction and in a second direction, and may work in conjunction with the multifunctional tailgate door. The multifunctional tailgate door has at least one anchor that works in conjunction with the cargo load system. The cargo load system includes a plurality of ports in a rear cargo floor surface having a plurality of winches and at least one motor for securing a cargo load.

The invention provides a humanoid robot and a dexterous hand thereof. The humanoid robot comprises a palm shell defining a containing cavity; the thumb comprises a first rotary actuator, a second rotary actuator, a transmission assembly and a thumb assembly, the first rotary actuator and the second rotary actuator are fixedly connected to the inner wall of the containing cavity, the transmission assembly is in transmission connection between the first rotary actuator and the second rotary actuator, and at least part of the thumb assembly extends out of the containing cavity; the thumb component is in transmission connection with the transmission component; each finger comprises a finger piece and a linear actuator, the linear actuators are fixedly connected to the cavity wall of the containing cavity, at least part of each finger piece extends out of the palm shell, and each finger piece comprises a connecting base, a finger near knuckle, a finger far knuckle, a finger far knuckle and a finger far knuckle rubber coating; and a connector board electrically connected to the first rotary actuator, the second rotary actuator, and the linear actuator. The dexterous hand is compact in layout, small in occupied space and high in movement precision, and the grabbing force of the dexterous hand is improved.

An actuator (20) arranged to be connected to a mechanical chain (13) of a mechanical system (10) for controlling the flight of a vehicle, comprising a first motor (22a), a first output arrangement (23a) driven in rotation about an axis of rotation (X1-X1) by the first motor (22a) and forming a first mechanical pathway, a second motor (22b), a second output arrangement (23b) driven in rotation about the axis of rotation (X1-X1) by the second motor (22b) and forming a second mechanical pathway, an output member (24) configured to be connected to the mechanical chain (13), a first and a second coupling / decoupling device (25a, 25b) connecting, in terms of rotation about the axis of rotation (X1-X1), respectively the first output arrangement (23a) and the second output arrangement (23b) with the output member (24) in a coupled position. The actuator (20) comprising an electronic control unit (40) configured to detect a blockage of one of the mechanical pathways of the actuator (20) and to control the torques of the motors (22a, 22b) separately.

An aircraft wing is disclosed having a fixed wing with a tip, and a wing tip device rotatably mounted on a hinge at the tip of the fixed wing, such that the wing tip device is rotatable about the hinge, and an actuation system for rotating the wing tip device about the hinge. The actuation system includes a motor, at least one geared rotary actuator, a reduction gearbox, a clutch for selectively decoupling rotation of the motor from rotation of the geared rotary actuator, the geared rotary actuator is driveable by the motor and arranged to convert rotary motion into a different rotary motion and is arranged to rotate the wing tip device relative to the tip of the fixed wing. The reduction gearbox is positioned between the clutch and the geared rotary actuator along a drive train between the motor and the geared rotary actuator.

The invention relates to a rotary actuator (1) comprising: - a stator (10), - at least one stator coil (11) which is connected to the stator (10) in such a way that a force acting on the stator coil (11) is transferred to the stator (10); - an armature (20) rotatable about an axis of rotation (2) relative to the stator (10), - at least one armature coil (21) which is connected to the armature (20) in such a way that a force acting on the armature coil (21) is transferred to the armature (20); - Power lines (3) through which at least one stator coil (11) can be energized, - Cable (4) through which the at least one armature coil (21) can be energized, - a rotation angle limiting device (5) by which rotation of the armature relative to the stator is limited to a rotation angle range of 0 to 359 degrees.

An actuator assembly for moving a movable aerodynamic surface of an aircraft is disclosed including an input section for introducing an externally provided rotary motion into the actuator assembly, and a geared rotary actuator having at least one actuator slice having a planetary gear with a sun gear couplable to the input section, a fixed gear attachable to a fixed component of the aircraft and an output gear couplable with the movable aerodynamic surface. At least one clutch is connected to the geared rotary actuator and is configured to couple the movable surface with the input section and to selectively decouple the movable surface from the input section, such that it is freely movable.

A remotely controlled powered chair may include a support frame, a seat pivotally mounted on the support frame, an rotary actuator mounted between the support frame and the seat to drive the seat to move relative to the support frame, a backrest pivotally mounted on the seat, and a linear actuator mounted between the seat and the backrest to drive the backrest to move relative to the seat. Thus, the rotary actuator may be controlled by an electrically control device to drive the seat to pivot relative to the support frame reciprocally in a pendulum manner so that the seat is pivoted relative to the support frame automatically. In addition, the linear actuator may be controlled by the electrically control device to adjust the inclined angle of the backrest so as to provide a comfortable sensation to the user.

An intermediary support structure that includes a linear or rotational actuator to move the single display tile from a first position in a first plane along a predetermined path to a second position in the first plane. The first position is a loading position of the single display tile in the tiled display and the second position is a position in which the single display tile lies when installed in its operative position in the tiled display. When the single display tile is located in the first position, there is a distance between the loading position and the operative position, the linear or rotational actuator is configured so that the distance becomes smaller as the single display tile is moved along the predetermined path towards the second position. The linear or rotational actuator is accessible and remains accessible until an adjacent display tile is covering an access to the actuator.

A vehicle is provided which has a vehicle body, at least one hub of a wheel, and a suspension connecting the hub to the vehicle body. The suspension has a suspension arm hinged to the vehicle body and to the hub, a spring, and an electromechanical rotary actuator operable between an active adjustment condition and a damping condition of the motion of the suspension, via a leverage.

The present invention provides a feed dispensing and distributing apparatus (1) which distributes one portion at the time evenly over an aquaculture cage using a rotationally connected distributing unit, said apparatus comprising a feed portion container (2), a portion dispenser (3), a feed guiding tube (5), a weighing device (4) adapted to determine the weight of feed that has not been released from the feed portion container (2) and the feed guiding tube (5), a rotational feed distributer (6) comprising a rotating disc portion (11), radial blades (12), and a rotary actuator (7) for driving the rotational feed distributer, and a computing device (8), wherein the computing device (8) regulates the speed of the rotational feed distributer (6) during the distribution of a portion of feed in relation to the weight of the feed that has not been released onto the rotational feed distributer (6). A method for dispensing and distribution feed over an aquaculture cage comprises releasing feed from the feed portion dispenser (2) into the portion guiding structure (10), releasing the feed onto the rotational feed distributer (6), determining the weight of the not-released feed, and regulating the speed of the rotational feed distributer (6) in relation to the weight of the feed.

Disclosed is a rotary actuator unit with a casing and an internal rotating shaft integral with rotating end flanges projecting from said casing at a main axis of rotation, a load cell apt to detect a load acting on one of said rotating end flanges, further comprising an articulated link parallelogram frame defined by a pair of end brackets constrained to said rotating end flanges, equipped with respective hinge bodies defining parallel hinge axes in which first hinge pins are pivotingly engaged, a pair of lower and upper end plates hinged at proximal end to said hinge pins, said lower and upper end plates being provided with second hinge pins at a distal end, and an attachment plate hinged at respective ends to said second hinge pins, and in which said upper end plates is abutting said load cell and attachment plate has fastening means to engage a user structure.

An actuator assembly and a camera module are described. The actuator assembly includes a first portion, a second portion, and a first support device mechanically coupling the first portion to the second portion. The actuator assembly also includes a first drive device including four segments of shape memory alloy wires. The first support means and the first drive means are configured such that the second portion is rotatable relative to the first portion about an axis parallel to the first direction. The actuator assembly also includes a third portion and a second support device mechanically coupling the second portion to the third portion. The actuator assembly further comprises a second driving device, and the second driving device comprises four sections of shape memory alloy wires. The second support means, the first drive means and the second drive means are configured such that the third portion moves toward or away from the first portion in the first direction in response to a torque applied by the first drive means and / or the second drive means about an axis parallel to the first direction.