Abstract: A dosing unit for use in an automatic dosing system of a water-bearing household appliance, for automatically dosing a dosing amount of a solid detergent, the dosing unit comprising a dosing cartridge for storing a bulk of the solid detergent and a dosing device for separating the dosing amount from the bulk and releasing the separated dosing amount by linearly displacing a sliding element from a separating position to a release position, wherein the dosing device includes a dosing channel, wherein, when the sliding element is in the separating position, the dosing channel is configured for receiving at least the dosing amount from the bulk and intermediately storing the dosing amount in a pre-dosing position, and, when the sliding element is in the release position, the dosing device is configured for releasing the dosing amount intermediately stored in the pre-dosing position.

Abstract: Broadly speaking, embodiments of the present techniques provide haptic button assemblies in which the haptic button has a low profile while still providing a satisfying tactile response or sensation to a user. Advantageously, the haptic button assemblies may have a profile that, for example, enables the assembly to be incorporated into the free space along an edge of a portable computing device. The haptic assemblies may, for example, be arranged to move the button perpendicularly with respect to the edge of the device.

Abstract: An actuator assembly (100) comprises: a support structure (51); a movable part (10) that is movable relative to the support structure; and a set of one or more actuating units (80). Each actuating unit (80) is configured, on actuation, to apply a force on the movable part (10) that is substantially directed along a line in a plane perpendicular to a primary axis (z). Each actuating unit (10) comprises: a force-modifying mechanism (84) connected to one of the support structure (51) and the movable part (10); a coupling link (83) connected between the force-modifying mechanism (84) and the other of the support structure (51) and the movable part (10); and an SMA element (70a) connected between the force-modifying mechanism (84) and the one of the support structure (51) and the movable part (10).

Abstract: An SMA actuator assembly (2) comprising: a support structure (10); a movable part (20) that is movable relative to the support structure; and an SMA wire (30) connected at its ends to the movable part and/or the support structure and arranged to move the movable part relative to the support structure, wherein the SMA wire is arranged to be in contact between its ends with one or more contact portions of the movable part and/or support structure, and wherein each contact portion comprises a plurality of contact sections (10a, 20a) that are in direct contact with the SMA wire, wherein the plurality of contact sections are separated by one or more gaps between the contact sections.

Abstract: An apparatus comprising: a support structure; a movable part comprising an electronic component, wherein a primary axis is defined with reference to the support structure and passes through the electronic component; an actuator assembly configured to move the movable part relative to the support structure; and a flexible connector for making electrical connections to the electronic component.

Abstract: A method suitable for use by a time-of-flight (TOF) imaging system (500), wherein the system emits illumination in multiple configurations, each configuration having a different spatially-varying intensity over a field of view of an image sensor (512), the method comprising: moving an actuation mechanism (506) to change the illumination via a first sequence of configurations from a first configuration (A) to a final configuration (B); moving the actuation mechanism (506) to subsequently change the illumination via a second sequence of configurations from the final configuration to the first configuration or a second configuration; and obtaining a set of data from the image sensor (512) for each of the configurations (A, B) in the first and second sequences, thereby obtaining two sets of data for each configuration that are suitable for producing two depth image frames, wherein the two sets of data corresponding to the final configuration are consecutively obtained from the first and second sequences.

Abstract: Embodiments herein provide haptic button assemblies with a shape memory alloy actuator (SMA) in which the haptic button has a low profile while still providing a satisfying tactile response or sensation to a user. Advantageously, the haptic button assemblies may have a profile that, for example, enables the assembly to be incorporated into the free space along an edge of a portable computing device. The haptic assemblies may for example, be arranged to move the button perpendicularly with respect to the edge of the device.

Abstract: An actuator assembly comprises a support structure (6), a movable part (5) movable relative to the support structure, at least one shape memory alloy (SMA) wire (2) connected between the support structure and the movable part via wire attach components and arranged, on contraction, to drive movement of the movable part and a control circuit configured to apply drive signals to the at least one SMA wire so as to drive movement of the movable part relative to the support structure between predetermined positions in a repeated pattern; wherein the length of the at least one SMA wire extending between respective wire attach components is less than 5 mm.

Abstract: Broadly speaking, embodiments of the present techniques provide haptic button assemblies in which the haptic button has a low profile while still providing a satisfying tactile response or sensation to a user. Advantageously, the haptic button assemblies may have a profile that, for example, enables the assembly to be incorporated into the free space along an edge of a portable computing device. The haptic assemblies may, for example, be arranged to move the button perpendicularly with respect to the edge of the device.

Abstract: A time-of-flight sensor system 10 comprising: an illumination source 11 for illuminating a subject 19 to which a time-of-flight is to be measured; an optical system configured to, using an at least one actuator, transition the illumination source 11 between providing spot illumination and flood illumination; and a sensor 12 comprising a sensor surface. The sensor surface is configured to sense light scattered by the subject 19 from the illumination source 12 and to provide data dependent on sensed light. The spot illumination has a spatially non-uniform intensity over the sensor surface, and the optical system is configured to move the spot illumination across at least part of the sensor surface to generate an output frame, wherein the at least one actuator comprises at least one shape memory alloy (SMA) component.

Abstract: A camera assembly is disclosed. The camera assembly comprises: a first part; a second part tiltable with respect to the first part, the second part including an image sensor and a lens system, wherein the lens system is above the image sensor with respect to a primary axis passing through the image sensor; a drive system configured, in response to drive signals, to cause tilting of the second part with respect to the first part, wherein the tilting is about first and/or second axes which are not parallel and which are perpendicular to the primary axis; and one or more flexible connectors operatively connected to the second part, wherein the one or more flexible connectors are routed to pass between the second part and the first part below the image sensor with respect to the primary axis.

Abstract: A resonant actuator assembly (1) comprising: a support structure (3); a movable part (5) that is capable of relative motion with respect to the support structure; and an actuator arrangement (7) arranged to drive relative motion of the movable part, the resonant actuator assembly being arranged to provide a restoring force to the movable part on displacement from an equilibrium position with respect to the support structure, and the actuator arrangement being arranged to drive the relative motion of the movable part at a resonance of the resonant actuator assembly, the restoring force being non-linear with the displacement.

Abstract: Broadly speaking, embodiments of the present techniques provide haptic button assemblies in which the haptic button has a low profile while still providing a satisfying tactile response or sensation to a user. Advantageously, the haptic button assemblies may have a profile that, for example, enables the assembly to be incorporated into the free space along an edge of a portable computing device. The haptic assemblies may, for example, be arranged to move the button perpendicularly with respect to the edge of the device.

Abstract: An actuator assembly (23) includes a first part (24), a second part (25), and a bearing arrangement (26) mechanically coupling the first part (24) to the second part (25). The actuator assembly (23) also includes a drive arrangement (11, 20) including a total of four lengths of shape memory alloy wire (141, 142, 143, 144). The drive arrangement (11, 20) and the bearing arrangement (26) are configured such that the second part (25) is movable towards or away from the first part (24) along a primary axis (z), and the second part (25) is movable relative to the first part (24) along a first axis (x) and/or a second axis (y). The first and second axes (x, y) are perpendicular to the primary axis (z) and the second axis (y) is different to the first axis (x).

Abstract: A shape memory alloy (SMA) actuator (100) for a camera assembly, comprising:—a support structure supporting an electronic component, wherein the electronic component is susceptible to interference caused by magnetic flux;—a moveable part moveable relative to the support structure; one or more SMA components (12) connected between the moveable part and the support structure, wherein the one or more SMA components are configured to, on contraction, drive movement of the movable part;—a first electrical path and a second electrical path defined between, and/or including, each of the one or more SMA components (12) and respective electrical terminals (3a); and wherein the first and second electrical paths of each of the one or more SMA components are configured to, at least in part, extend adjacently to and in parallel with each other, and enabling the electrical current in the respective paths to flow in opposite directions, so as to minimise combined magnetic flux from the first and second electrical paths into

Abstract: The actuator assembly comprises a first part (102), a second part (110) and a helical bearing arrangement. The helical bearing arrangement is arranged to guide helical movement of the second part with respect to the first part around a helical axis H such that rotation of the second part around the helical axis is converted into helical movement of the second part. The first and second parts comprise respective stops (152, 162) that are arranged such that the stops are spaced from each other throughout an operating range of said helical movement of the second part relative to the first part. The stops are configured to engage if the second part is moved relative to the first part in at least one direction other than the direction of said helical movement such that the engagement of the stops restricts relative movement of the first and second parts.

Abstract: An actuator assembly (23) is described which includes first part (24), a second part (25) and a bearing arrangement (26) mechanically coupling the first part (24) to the second part (25). The bearing arrangement (26) includes a first bearing (27) mechanically coupling the first part (24) to a third part (28). The actuator assembly (23) also includes a drive arrangement (11, 20). The drive arrangement (11, 20) includes four lengths of shape memory alloy wire (141, 142, 143, 144). Each length of shape memory alloy wire (141, 142, 143, 144) is connected between the third part (28) and the second part (25). The drive arrangement (11, 20) and the bearing arrangement (26) are configured such that in response to a torque applied about a primary axis (z) by the drive arrangement (11, 20), the first bearing (27) generates movement of the first part (24) towards or away from the second part (25) and the third part (28) along the primary axis (z).

Abstract: A shape memory alloy apparatus (1) comprising: a member (3) comprising a first end portion (5) and a second end portion (7); and a shape memory alloy component (9) connected to the member (3). The shape memory alloy component (9) being configured to, on contraction, change the separation between the first end portion (5) and the second end portion (7) of the member (3), the member (3) being configured to be in tension during contraction of the shape memory alloy component (9), wherein the said separation changes in a direction that is angled to the direction of contraction.

Abstract: An actuation apparatus comprising: a support structure; a movable element; a helical bearing arrangement supporting the movable element on the support structure and arranged to guide helical movement of the movable element with respect to the support structure along a helical path around a helical axis; an actuating mechanism configured to drive rotation of the movable element around the helical axis which the helical bearing arrangement converts into said helical movement; and a loading arrangement configured to exert a biasing force on the movable element in a direction that is at least substantially normal to the helical path over an operating range of the helical movement.

Abstract: A method suitable for use by a time-of-flight (TOF) imaging system (500), wherein the system emits illumination in multiple configurations, each configuration having a different spatially-varying intensity over a field of view of an image sensor (512), the method comprising: moving an actuation mechanism (506) to change the illumination via a first sequence of configurations from a first configuration (A) to a final configuration (B); moving the actuation mechanism (506) to subsequently change the illumination via a second sequence of configurations from the final configuration to the first configuration or a second configuration; and obtaining a set of data from the image sensor (512) for each of the configurations (A, B) in the first and second sequences, thereby obtaining two sets of data for each configuration that are suitable for producing two depth image frames, wherein the two sets of data corresponding to the final configuration are consecutively obtained from the first and second sequences.