GB2623348A - SMA actuator assembly - Google Patents

SMA actuator assembly Download PDF

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Publication number
GB2623348A
GB2623348A GB2215122.9A GB202215122A GB2623348A GB 2623348 A GB2623348 A GB 2623348A GB 202215122 A GB202215122 A GB 202215122A GB 2623348 A GB2623348 A GB 2623348A
Authority
GB
United Kingdom
Prior art keywords
coupling component
sma
coupling
sma element
encapsulated
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
GB2215122.9A
Other versions
GB202215122D0 (en
Inventor
Benjamin Simpson Brown Andrew
Farmer Geoffrey
matthew bunting Stephen
Howarth James
Eddington Robin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Cambridge Mechatronics Ltd
Original Assignee
Cambridge Mechatronics Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Cambridge Mechatronics Ltd filed Critical Cambridge Mechatronics Ltd
Priority to GB2215122.9A priority Critical patent/GB2623348A/en
Publication of GB202215122D0 publication Critical patent/GB202215122D0/en
Priority to PCT/GB2023/052673 priority patent/WO2024079487A1/en
Publication of GB2623348A publication Critical patent/GB2623348A/en
Pending legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
    • F03G7/06—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like
    • F03G7/061—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like characterised by the actuating element
    • F03G7/0614—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like characterised by the actuating element using shape memory elements
    • F03G7/06143—Wires
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
    • F03G7/06—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like
    • F03G7/061—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like characterised by the actuating element
    • F03G7/0614—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like characterised by the actuating element using shape memory elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
    • F03G7/06—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like
    • F03G7/061—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like characterised by the actuating element
    • F03G7/0616—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like characterised by the actuating element characterised by the material or the manufacturing process, e.g. the assembly
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
    • F03G7/06—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like
    • F03G7/064—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like characterised by its use
    • F03G7/0645—Clamping, fixing or crimping parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
    • F03G7/06—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like
    • F03G7/066—Actuator control or monitoring
    • F03G7/0665—Actuator control or monitoring controlled displacement, e.g. by using a lens positioning actuator
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
    • G02B7/02—Mountings, adjusting means, or light-tight connections, for optical elements for lenses

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Control Of Position Or Direction (AREA)
  • Prostheses (AREA)

Abstract

A shape memory alloy (SMA) actuator assembly 1 comprises a first part 3, a second part 4, an SMA element 2 configured to drive relative movement between the first and second parts. The SMA element is coupled to the first part via a first coupling component 31 which is encapsulated within the first part. The SMA element may be coupled to the second part via a second coupling component 41 which is encapsulated within the second part. Alternatively, the SMA element may be coupled to the first part via a second coupling component which is encapsulated within the first part, with the SMA element engaging the second part to drive the relative movement. The first coupling and/or second coupling component may be integrally formed and/or comprise a crimp. At least one further SMA element may be coupled to the first part via a third coupling component which is encapsulated within the first part, and the third coupling component may be separate from the first coupling component.

Description

SMA ACUATOR ASSEMBLY
Field
The present application relates to a shape memory alloy (SMA) actuator assembly.
Summary
According to an aspect of the present invention, there is provided a shape memory alloy (SMA) actuator assembly comprising: a first part; a second part; an SMA element configured to (e.g. upon actuation) drive relative movement between the first and second parts; wherein the SMA element is coupled to the first part via a first coupling component which is encapsulated within the first part.
Optionally, the SMA element is coupled to the second part via a second coupling component which is encapsulated within the second part. Alternatively, the SMA element may be further coupled to the first part via a second coupling component which is encapsulated within the first part, wherein the SMA element engages the second part (e.g. is wrapped/hooked around a component of the second part) so as to drive the relative movement.
Optionally, the first coupling component is integrally formed, and/or the second coupling component is integrally formed.
Optionally, the first coupling component comprises a crimp, and/or the second coupling component comprises a crimp.
Optionally, the first part is a support structure of the SMA actuator assembly. Optionally, the second part is a movable part of the SMA actuator assembly. The movable part may comprise an electronic component such as an image sensor, a display, or an emitter. The movable part may comprise a lens assembly.
Optionally, the SMA actuator assembly comprises at least one further SMA element coupled to the first part via a third coupling component which is encapsulated within the first part, and the third coupling component is separate from (e.g. not integrally formed with) the first coupling component. This further SMA element may be coupled to the first and second parts, and configured to (e.g. upon actuation) drive relative movement between the first and second parts.
According to another aspect of the present invention, there is provided a method of manufacturing an SMA actuator assembly comprising a first and a second part that are movable relative to each other (such as the ones described above); the method comprising: coupling an SMA element to a first coupling component; and (e.g. subsequently) encapsulating the first coupling component within the first part.
Optionally, the SMA element is coupled to the first coupling component before the first coupling component is encapsulated.
Optionally, the method further comprises: coupling the SMA element to a second coupling component; and (e.g. subsequently) encapsulating the second coupling component within the second part. Alternatively, (e.g. where the SMA element is wrapped/hooked around a component of the second part) the method may further comprise: coupling the SMA element to a second coupling component; and (e.g. subsequently) encapsulating the second coupling component within the first part. The first and second coupling components may be encapsulated within the first part simultaneously.
Optionally, the SMA element is coupled to the second coupling component before the second coupling component is encapsulated.
Optionally, the SMA element is coupled to both the first and second coupling components before the first and/or second coupling components are encapsulated.
Optionally, the first and second coupling components are held apart by a sacrificial strut body (during at least part of the encapsulation).
Optionally, the method comprises: removing the sacrificial strut body holding apart the first and second coupling components after the first and/or second coupling components are encapsulated.
Optionally, encapsulating the first coupling component within the first part comprises moulding the first part at least partly around the first coupling component. Optionally, encapsulating the second coupling component within the second part comprises moulding the second part at least partly around the second coupling component. Optionally, encapsulating the second coupling component within the first part comprises moulding the first part at least partly around the second coupling component.
Optionally, encapsulating the first coupling component within the first part comprises additively manufacturing at least part of the first part so as to hold the first coupling component. Optionally, encapsulating the second coupling component within the second part comprises additively manufacturing at least part of the second part so as to hold the first coupling component. Optionally, encapsulating the second coupling component within the first part comprises additively manufacturing at least part of the first part so as to hold the first coupling component.
Optionally, additively manufacturing at least part of the first part so as to hold the first coupling component (and/or the second coupling component) comprises: additively manufacturing the first part up to and including a pocket (or pockets) shaped to fit the first coupling component (and/or the second coupling component) within it (or them); placing the first coupling component (and/or the second coupling component) into the pocket(s); (subsequently) additively manufacturing the rest of the at least part of the first part so as to (at least partly) enclose the first coupling component (and/or the second coupling component) within the pocket(s).
Optionally, additively manufacturing at least part of the second part so as to hold the second coupling component comprises: additively manufacturing the second part up to and including a pocket shaped to fit the second coupling component within it; (subsequently) placing the second coupling component into the pocket; (subsequently) additively manufacturing the rest of the at least part of the second part so as to (at least partly) enclose the second coupling component within the pocket.
The pockets may also be referred to as cavities.
Optionally, additively manufacturing at least part of the first part so as to hold the first coupling component (and/or the second coupling component) comprises: additively manufacturing a portion of the first part comprising a main body, a pocket (or pockets) shaped to fit the first coupling component (and/or the second coupling component) within it (or them), and a lid (or lids) connected to the main body via a living hinge (or living hinges); (subsequently) placing the first coupling component (and/or the second coupling component) into the pocket(s); (subsequently) closing the lid(s) so as to (at least partly) enclose the first coupling component (and/or the second coupling component) within the pocket(s); (subsequently) additively manufacturing the rest of the at least part of the first part so as to seal the first coupling component (and/or the second coupling component) within the pocket(s).
Optionally, additively manufacturing at least part of the second part so as to hold the second coupling component comprises: additively manufacturing a portion of the second part comprising a main body, a pocket shaped to fit the second coupling component within it, and a lid connected to the main body via a living hinge; (subsequently) placing the second coupling component into the pocket; (subsequently) closing the lid so as to (at least partly) enclose the second coupling component within the pocket; (subsequently) additively manufacturing the rest of the at least part of the second part so as to seal the second coupling component within the pocket.
Optionally, the method comprises locally cooling the SMA element during at least part of the encapsulation, for example during the moulding or the additive manufacturing of the first and/or the second parts.
Optionally, the method comprises providing a sealing around the SMA element so as to protect the SMA element from being damaged (e.g. from high temperatures) during at least part of the encapsulation, for example during the moulding or the additive manufacturing of the first and/or the second parts.
Brief description of the drawings
Certain embodiments of the present invention will now be described, by way of example only, with reference to the accompanying drawings in which: Fig. 1 is a schematic view of an SMA actuator assembly.
Detailed description
The present invention describes ways of manufacturing the shape memory alloy (SMA) actuator assembly 1 shown in Fig. 1. The SMA actuator assembly 1 comprises a first part 3 (which may be a support structure) and a second part 4 (which may be a movable part). A first coupling component 31 (which may be a crimp) is held within and encapsulated within the first part 3. A second coupling component 41 (which may be a crimp) is held within and encapsulated within the second part 4. The first and second coupling components 31,41 are coupled to an SMA element 2, which is an SMA wire 2 in Fig. 1. The SMA wire 2 is configured to move the first part 3 and the second part 4 relative to each other when actuated by being contracted. The SMA wire 2 contracts when heated. The SMA wire 2 may be heated by passing a current through the SMA wire 2.
The SMA actuator assembly 1 may be manufactured using an insert moulding process comprising: 1) Placing inside a mould the first coupling component 31 and/or the second coupling component 41 holding the SMA wire 2.
2) Closing the mould.
3) Injecting molten material (e.g. plastic) into the mould and over the coupling component(s) provided inside the mould, to form the first part 3 and/or the second part 4.
During this manufacturing process, the first and second coupling components 31,41 may be connected via a disposable fret (herein also referred to as a sacrificial strut body) holding apart the two coupling components 31, 41. Where this is the case, the manufacturing process could also involve: 4) Removing the disposable fret (i.e. the sacrificial strut body) from the first and second coupling components 31, 41.
One of the issues with the above methods of manufacturing is that the SMA wire 2 may be damaged by the temperatures of the injection moulding process. To mitigate this risk, one may provide: * local cooling around the SMA wire 2; * sealing around the SMA wire 2 without damaging the wire.
The latter may be done by providing flexibility in the crimps so that the crimps mount on a reference surface in the tool and there is a wire sealing surface at the crimp thickness above.
Alternatively, the SMA actuator assembly 1 may be manufactured using an additive manufacturing process (e.g. a 3D printing process) comprising: 1) Additively manufacturing (e.g. 3D printing) the first part 3 up to and including a pocket (e.g. a cavity, a space) shaped to hold the first coupling component 31 and/or additively manufacturing the second part 4 up to and including a pocket shaped to hold the second coupling component 41.
2) (Optionally) Pausing the additive manufacturing 3) Placing the first coupling component 31 within the pocket of the first part 3 and/or placing the second coupling component 41 within the pocket of the second part 4.
4) Additively manufacturing (e.g. 3D printing) over the first coupling component 31 and/or the second coupling component 41 so as to (at least partly) enclose it/them within the pocket(s). In other words, restarting the additive manufacturing (e.g. the print) at the layer that rests on top of the inserted coupling component(s) so as to seal the inserted coupling component(s) within the pocket(s).
During this manufacturing process, the first and second coupling components 31,41 may be connected via a disposable fret (herein also referred to as a sacrificial strut body) holding apart the two coupling components 31, 41. Where this is the case, the manufacturing process would also involve: 5) Removing the disposable fret (i.e. the sacrificial strut body) from the first and second coupling components 31, 41.
The coupling components 31, 41 may be attached/bonded (e.g. glued) into the pockets.
This manufacturing process works best where the inserted coupling component has a flat upper surface and no recessed upper surfaces that would require unsupported layers. There are some methods of optimising the shape of the print to accommodate these types of features but they are limiting and dependant on the additive manufacturing technology/3D printing technology being used.
Where the inserted coupling component does not have a flat upper surface, the following alternative method of additive manufacturing may be more appropriate: 1) Additively manufacturing (e.g. 3D printing) a portion of the first part 3 including: (i) its main body comprising a pocket shaped to hold the first coupling component 31, (ii) a lid, and (iii) a living hinge connecting the lid and the main body; and/or additively manufacturing a portion of the second part 4 including: (i) its main body comprising a pocket shaped to hold the second coupling component 41, (ii) a lid, and (iii) a living hinge connecting the lid and the main body of the second part.
2) Placing the first coupling component 31 within the pocket of the first part 3 and/or placing the second coupling component 41 within the pocket of the second part 4.
3) Closing the lid over the coupling component(s) 31, 41 so as to (at least partly) enclose it (or them) within the pocket(s).
4) Additively manufacturing the rest of the first part 3 so as to seal the first coupling component 31 within the pocket of the first part, and/or the rest of the second part 4 so as to seal the second coupling component 41 within the pocket of the second part.
During this manufacturing process, the first and second coupling components 31,41 may be connected via a disposable fret (herein also referred to as a sacrificial strut body) holding apart the two coupling components 31, 41. Where this is the case, the manufacturing process would also involve: 5) Removing the disposable fret (i.e. the sacrificial strut body) from the first and second coupling components 31, 41.
The coupling components 31,41 may be attached/glued into the pockets.
SMA element The term 'shape memory alloy (SMA) element' may refer to any element comprising SMA. The SMA element may be described as an SMA wire. The SMA element may have any shape that is suitable for the purposes described herein. The SMA element may be elongate and may have a round cross section or any other shape cross section. The cross section may vary along the length of the SMA element. The SMA element might have a relatively complex shape such as a helical spring. It is also possible that the length of the SMA element (however defined) may be similar to one or more of its other dimensions. The SMA element may be sheet-like, and such a sheet may be planar or non-planar. The SMA element may be pliant or, in other words, flexible. In some examples, when connected in a straight line between two components, the SMA element can apply only a tensile force which urges the two components together. In other examples, the SMA element may be bent around a component and can apply a force to the component as the SMA element tends to straighten under tension. The SMA element may be beam-like or rigid and may be able to apply different (e.g. non-tensile) forces to elements. The SMA element may or may not include material(s) and/or component(s) that are not SMA. For example, the SMA element may comprise a core of SMA and a coating of non-SMA material. Unless the context requires otherwise, the term 'SMA element' may refer to any configuration of SMA material acting as a single actuating element which, for example, can be individually controlled to produce a force on an element. For example, the SMA element may comprise two or more portions of SMA material that are arranged mechanically in parallel and/or in series. In some arrangements, the SMA element may be part of a larger SMA element. Such a larger SMA element might comprise two or more parts that are individually controllable, thereby forming two or more SMA elements. The SMA element may comprise an SMA wire, SMA foil, SMA film or any other configuration of SMA material. The SMA element may be manufactured using any suitable method, for example by a method involving drawing, rolling or deposition and/or other forming process(es). The SMA element may exhibit any shape memory effect, e.g. a thermal shape memory effect or a magnetic shape memory effect, and may be controlled in any suitable way, e.g. by Joule heating, another heating technique or by applying a magnetic field.
Other variations It will be appreciated that there may be many other variations of the above-described examples.
The coupling components 31, 41 may comprise electrical connection portions configured to allow the SMA wire 2 to be electrically connected to e.g. a control circuit.
The first and second coupling components may be both encapsulated within the first part, and e.g. have the SMA wire hooked to or wrapped around a component of the second part. Alternatively, the first and second coupling components may be both encapsulated within the second part, and e.g. have the SMA wire hooked to or wrapped around a component of the first part.

Claims (21)

  1. SClaims 1. A shape memory alloy (SMA) actuator assembly comprising: a first part; a second part; an SMA element configured to drive relative movement between the first and second parts; wherein the SMA element is coupled to the first part via a first coupling component which is encapsulated within the first part.
  2. 2. An SMA actuator assembly according to claim 1, wherein the SMA element is coupled to the second part via a second coupling component which is encapsulated within the second part.
  3. 3. An SMA actuator assembly according to claim 1, wherein the SMA element is further coupled to the first part via a second coupling component which is encapsulated within the first part, and wherein the SMA element engages the second part so as to drive the relative movement.
  4. 4. An SMA actuator assembly according to any preceding claim, wherein the first coupling component is integrally formed, and/or the second coupling component is integrally formed.
  5. 5. An SMA actuator assembly according to any preceding claim, wherein the first coupling component comprises a crimp, and/or the second coupling component comprises a crimp.
  6. 6. An SMA actuator assembly according to claim 5, wherein the first part is a support structure of the SMA actuator assembly.
  7. 7. An SMA actuator assembly according to any of claims Ito 6, comprising at least one further SMA element coupled to the first part via a third coupling component which is encapsulated within the first part, and the third coupling component is separate from the first coupling component.
  8. 8. A method of manufacturing an SMA actuator assembly comprising a first and a second part that are movable relative to each other; the method comprising: coupling an SMA element to a first coupling component; and encapsulating the first coupling component within the first part.
  9. 9. A method according to claim 8, wherein the SMA element is coupled to the first coupling component before the first coupling component is encapsulated.
  10. 10. A method according to claim 8 or 9, further comprising: coupling the SMA element to a second coupling component; and encapsulating the second coupling component within the second part.
  11. 11. A method according to claim 8 or 9, further comprising: coupling the SMA element to a second coupling component; and encapsulating the second coupling component within the first part.
  12. 12. A method according to claim 10 or 11, wherein the SMA element is coupled to the second coupling component before the second coupling component is encapsulated.
  13. 13. A method according to any of claims 10 to 12, wherein the SMA element is coupled to the first and second coupling components before the first and/or second coupling components are encapsulated.
  14. 14. A method according to any of claims 10 to 13, wherein the first and second coupling components are held apart by a sacrificial strut body.
  15. 15. A method according to claim 14, comprising: removing the sacrificial strut body holding apart the first and second coupling components after the first and/or second coupling components are encapsulated.
  16. 16. A method according to any of claims 8 to 15, wherein encapsulating the first coupling component within the first part comprises moulding the first part at least partly around the first coupling component.
  17. 17. A method according to any of claim 8 to 15, wherein encapsulating the first coupling component within the first part comprises additively manufacturing at least part of the first part so as to hold the first coupling component.
  18. 18. A method according to claim 17, wherein additively manufacturing at least part of the first part so as to hold the first coupling component comprises: additively manufacturing the first part up to and including a pocket shaped to fit the first coupling component within it; placing the first coupling component into the pocket; additively manufacturing the rest of the at least part of the first part so as to at least partly enclose the first coupling component within the pocket.
  19. 19. A method according to claim 17, wherein additively manufacturing at least part of the first part so as to hold the first coupling component comprises: additively manufacturing a portion of the first part comprising a main body, a pocket shaped to fit the first coupling component within it, and a lid connected to the main body via a living hinge; placing the first coupling component into the pocket; closing the lid so as to at least partly enclose the first coupling component within the pocket; additively manufacturing the rest of the at least part of the first part so as to seal the first coupling component within the pocket.
  20. 20. A method according to any of claims 8 to 19, comprising locally cooling the SMA element during at least part of the encapsulation.
  21. 21. A method according to any of claims 8 to 20, comprising providing a sealing around the SMA element so as to protect the SMA element from being damaged during at least part of the encapsulation.
GB2215122.9A 2022-10-13 2022-10-13 SMA actuator assembly Pending GB2623348A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB2215122.9A GB2623348A (en) 2022-10-13 2022-10-13 SMA actuator assembly
PCT/GB2023/052673 WO2024079487A1 (en) 2022-10-13 2023-10-13 Sma actuator assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2215122.9A GB2623348A (en) 2022-10-13 2022-10-13 SMA actuator assembly

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GB202215122D0 GB202215122D0 (en) 2022-11-30
GB2623348A true GB2623348A (en) 2024-04-17

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Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140060036A1 (en) * 2012-08-31 2014-03-06 GM Global Technology Operations LLC Compensating for incomplete reversal in mechanisms incorporating shape memory alloy wire
WO2018173743A1 (en) * 2017-03-23 2018-09-27 株式会社デンソー Movable device, production method therefor, and control method therefor

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015001439B4 (en) * 2015-02-09 2016-09-15 Solvo GmbH Actuator arrangement with shape memory actuators and operating method
GB201508968D0 (en) 2015-05-26 2015-07-01 Cambridge Mechatronics Ltd SMA wire assembly
WO2018055972A1 (en) * 2016-09-20 2018-03-29 株式会社デンソー Actuator device
GB201803084D0 (en) * 2018-02-26 2018-04-11 Cambridge Mechatronics Ltd Haptic button with SMA

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140060036A1 (en) * 2012-08-31 2014-03-06 GM Global Technology Operations LLC Compensating for incomplete reversal in mechanisms incorporating shape memory alloy wire
WO2018173743A1 (en) * 2017-03-23 2018-09-27 株式会社デンソー Movable device, production method therefor, and control method therefor

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WO2024079487A1 (en) 2024-04-18

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