TW201812558A - Force sensing architectures - Google Patents

Abstract

An electronic device with a force sensing device is disclosed. The electronic device comprises a user input surface defining an exterior surface of the electronic device, a first capacitive sensing element, and a second capacitive sensing element capacitively coupled to the first capacitive sensing element. The electronic device also comprises a first spacing layer between the first and second capacitive sensing elements, and a second spacing layer between the first and second capacitive sensing elements. The first and second spacing layers have different compositions. The electronic device also comprises sensing circuitry coupled to the first and second capacitive sensing elements configured to determine an amount of applied force on the user input surface. The first spacing layer is configured to collapse if the applied force is below a force threshold, and the second spacing layer is configured to collapse if the applied force is above the force threshold.

Description

Force sensing architecture

The present disclosure generally relates to sensing one force applied to a surface and, more specifically, sensing a force with respect to a capacitive change.

Touch devices typically provide an identification of where the user is touching the device, including movements, gestures, and the like. By way of example, a touch device can provide information to a computing system that interacts with a graphical user interface (GUI), such as pointing components, reorienting or repositioning their components, editing or keystrokes, and others. GUI features. In another example, the touch device can provide information suitable for a user to interact with an application to an computing system, such as animations, photos, pictures, slide presentations, sounds, text, other audiovisual components, and Other inputs or manipulations.

However, in general, touch input is considered a binary input. A touch exists and is sensed, or the touch does not exist. One of the touch inputs provides another source of input information to a device. For example, a device's response to touch with one of the low applied forces may be different than for a touch with one of the high applied forces. The force sensing device can determine an amount or value of an applied force based on a deformation amount of a component that is subjected to the force.

Where the force input is applied to a touch screen (such as a multi-touch touch screen, the user touches the touch screen to select an object or application displayed on the display or interacts with the object or application) In the device, the noise generated by the display interferes with the operation of the touch screen. In some cases, the display noise can be electrically coupled to the touch screen and interfere with the operation of the touch screen. Such display noise can also be electrically coupled to a force sensing device. The amount of noise of the display will be greater than the magnitude of the force signal, making it difficult to distinguish the force signals from the display noise.

An electronic device includes: a user input surface defining an outer surface of the electronic device; a first capacitive sensor comprising a first pair of sensing elements, the first pair of sensing elements having a gas a gap, and the first capacitive sensor is configured to determine a first applied force on the user input surface that causes one of the air gaps to collapse; and a second capacitive sensor, Below the first capacitive sensor, the second capacitive sensor includes a second pair of sensing elements, the second pair of sensing elements having a deformable element therebetween, the second capacitive sensor configured A second applied force on the user input surface that causes deformation of one of the deformable elements is determined.

The first pair of sensing elements includes a common sensing element and a first driving element, the first driving element being spaced apart from the common sensing element and capacitively coupled to the common sensing element. The second pair of sensing elements includes the common sensing element and a second driving element, the second driving element being spaced apart from the common sensing element and capacitively coupled to the common sensing element. The common sensing element can be disposed between the first driving element and the second driving element. The shared sensing element can include an array of sensing regions.

The electronic device can further include a display element coupled to the first drive element. The electronic device can further include a base structure, wherein the display element is configured to flex relative to the base structure, the deformable element is coupled to the base structure, and the air gap is positioned between the deformable element and the display element between. The common sensing element can be coupled to the deformable element.

The electronic device can further include a display layer including: a display element positioned below the user input surface; and a rear polarizer positioned below the display element. The electronic device may further include: a conductive material sheet formed on a rear surface of one of the rear polarizers to generate a conductive surface on the rear surface of the rear polarizer; and a conductive frame along the conductive Formed by at least one edge of the sheet of material. The conductive bezel can be positioned outside of a user viewable area of the display layer. The sheet of conductive material may comprise a silver nanowire.

A capacitive force sensor for an electronic device includes: a first driving layer; a second driving layer positioned relative to the first driving layer; and a common sensing layer at the first driving Between the layer and the second driving layer; a first spacer layer between the first driving layer and the common sensing layer; and a second spacer layer in the common sensing layer and the second Between the drive layers.

The first spacer layer can include an air gap. The capacitive force sensor can further include: a pair of opposing surfaces that define the air gap; and an anti-adhesion layer configured to prevent adhesion between the opposing surfaces. The air gap can have a thickness of about 1.0 mm or less. The second spacer layer can comprise a deformable material. The second spacer layer can comprise an array of deformable protrusions extending from a substrate layer.

The capacitive force sensor can further include a sensing circuitry operatively coupled to the first driver layer, the second driver layer, and the common sensing layer, and configured to determine A first applied force of a thickness of one of the first spacer layers and a second applied force that causes a thickness variation of one of the second spacer layers.

The first driving layer may include: an insulating substrate; a conductive material sheet formed on a rear surface of one of the insulating substrates to generate a conductive surface on the rear surface of the insulating substrate; and a conductive a bezel formed along at least one edge of the sheet of conductive material. The conductive bezel can include a continuous conductive bezel extending along the edges of the sheet of conductive material. The conductive bezel may include one or more conductive strips formed along respective edges of one of the sheets of conductive material

An electronic device can include: a cover member defining a user input surface of the electronic device; a first sensing element coupled to the cover member within an interior volume of the electronic device; a frame member Coupled to the cover member and extending into the interior volume of the electronic device; a second sensing element coupled to the frame member; and a third sensing element coupled to a base structure and coupled to the sensing The layers are separated.

The frame member can define an opening through which the third sensing element can be capacitively coupled to the second sensing element.

The first sensing element can comprise a layer of continuous transparent conductive material that substantially covers the entire surface of one of the substrates. The second sensing element can include a plurality of sensing regions, and the continuous transparent conductive material layer can overlap with the plurality of sensing regions of the plurality of sensing regions.

The third sensing element can include a plurality of driving regions, and each driving region can overlap with the plurality of sensing regions of the plurality of sensing regions. The first sensing element can further include a connection element electrically coupled to the layer of continuous transparent conductive material, and the electronic device can further include sensing circuitry configured to provide an electrical signal to the first sensing element And electrically coupling the sensing circuit system to a connector segment of the connecting component.

An electronic device can include: an insulating substrate positioned under a cap layer; a sheet of conductive material formed over a rear surface of the insulating substrate to create a rear surface of the insulating substrate a conductive surface; a conductive frame formed along at least one edge of the conductive material sheet; and an electrode layer positioned under the insulating substrate, wherein the conductive material sheet and the electrode layer together form a force sensitive The structure is configured to detect a force input on the cover layer.

The electronic device can further include: a drive circuitry coupled to the sheet of conductive material; and a sensing circuitry coupled to the electrode layer. The electrode layer can comprise an array of electrodes. The conductive bezel can include a continuous conductive bezel extending along the edges of the sheet of conductive material. The conductive bezel can include one or more conductive strips formed along respective edges of one of the sheets of conductive material.

An electronic device comprising: a display layer comprising a display element and a rear polarizer, the display element being positioned below a cover layer, the rear polarizer being positioned below the display element; a sheet of conductive material formed in a rear surface of one of the rear polarizers for producing a conductive surface on the rear surface of the rear polarizer; a conductive frame formed along at least one edge of the conductive material sheet; and a first electrode layer, It is positioned below the display layer. The sheet of conductive material and the first electrode layer can together form a force sensitive structure configured to detect a force input on the cover layer.

The electronic device can further include a touch sensitive layer positioned between the cap layer and the front polarizer. The electronic device can further include a conductive layer positioned between the touch sensitive layer and the front polarizer. The conductive bezel can include a continuous conductive bezel extending along the edges of the sheet of conductive material. The conductive bezel can include one or more conductive strips formed along respective edges of one of the sheets of conductive material.

The force sensitive structure may include a first force sensitive structure, the force input may include a first force, and the electronic device may further include a second force sensitive structure, the second force sensitive structure comprising a second electrode layer, The second electrode layer is positioned below the first electrode layer and spaced apart from the first electrode layer. The second force sensitive structure can be configured to detect a second force on the cover layer, wherein the second force is greater than the first force. The conductive bezel can be positioned outside of a user viewable area of the display layer.

The electronic device can further include: a drive circuitry coupled to the sheet of conductive material; and a sensing circuitry coupled to the first electrode layer. The first electrode layer can include an array of electrodes. The sheet of conductive material may comprise a silver nanowire.

A method of forming a conductive bezel on a surface of a film substrate can include applying a plurality of masks to the surface of the film substrate, each mask defining a region on the surface of the film substrate, The region will be surrounded by a respective conductive bezel; a conductive material is formed on the surface of the film substrate and the mask; the mask is removed from the surface of the film substrate to produce the conductive bezel; The conductive bezels are individually cut to create individual segments of the film substrate, each segment including a respective conductive bezel. The method can further include forming a protective layer over the surface of the film prior to singulating the conductive bezels.

Forming the conductive material on the surface of the film substrate and over the masks may include blanket depositing the conductive material on the surface of the film substrate and the masks. The film substrate can comprise a polarizer film comprising a sheet of conductive material formed on the surface of the polarizer film. The polarizer film can be attached to one of the display elements in an electronic device.

An electronic device can include: a user input surface defining an outer surface of the electronic device; a first capacitive sensing component; and a second capacitive sensing component capacitively coupled to the first capacitive sensing component; a first spacer layer between the first capacitive sensing element and the second capacitive sensing element; a second spacer layer between the first capacitive sensing element and the second capacitive sensing element And having a composition different from the first spacer layer; and sensing circuitry coupled to the first capacitive sensing component and the second capacitive sensing component, the sensing circuitry configured to determine The force exerted on one of the user input surfaces. The first spacer layer can be configured to collapse if the applied force is below a force threshold, and the second spacer layer can be configured to apply a force above the force threshold In the case of collapse.

The outer surface is substantially linearly deflectable relative to the force when the applied force is below the force threshold, and the outer surface is substantially relative to the force when the applied force is above the force threshold Nonlinear deflection. The sensing circuitry can determine the applied force using different force deflection correlations based on whether the first spacer layer is completely collapsed.

The first spacer layer can be an air gap, and the second spacer layer can comprise a deformable element. The deformable element can comprise an array of deformable protrusions extending from a substrate layer. The electronic device can further include a sensor configured to detect whether the first spacer layer is completely collapsed.

A force sensing device for an electronic device includes: a stack including a first capacitive sensing element; a structure under the stack and including a capacitive coupling to one of the first capacitive sensing elements a capacitive sensing element; an air gap between the stack and the structure; and a contact sensor. The stack can be configured to move relative to the structure in response to a force applied to a user input surface of the electronic device, thereby causing a thickness variation of the air gap, the first capacitive sensing element and the The second capacitive sensing element can be configured to provide a capacitance measurement corresponding to the thickness variation of the air gap, and the contact sensor can be configured to detect a complete collapse caused by the air gap Between the stack and the structure. The force sensing device can further include a deformable element between the first capacitive sensing element and the second capacitive sensing element.

The touch sensor can include a sensing region and a conductive element configured to contact the sensing regions as the stack contacts the structure through the air gap. The force sensing device can further include a deformable element on a first side of the air gap, wherein the conductive elements are disposed on the deformable element, and the sensing regions are disposed in one of the air gaps On the second side, the second side is opposite the first side. The deformable member can include a protrusion extending from a base layer, and the conductive elements can be coupled to the protrusions.

The contact sensor can include a capacitive sensing region on a first side of the air gap and a dielectric member on a second side of the air gap, the second side being opposite the first side, And the dielectric elements are capacitively coupled to the capacitive sensing regions. The capacitive sensing regions can be integrated with the first capacitive sensing component and the dielectric components are coupled to the deformable component.

A sensor assembly for an electronic device can include: a substrate; a plurality of protrusions including a deformable material extending from the substrate; and a plurality of sensing elements disposed on the protrusions Free end. The sensing elements can be at least partially embedded in the protrusions. The sensing elements can be coated on the protrusions. The sensing elements can comprise a conductive material. The sensing elements can comprise a dielectric material. The substrate and the plurality of protrusions can be a one-piece assembly. The sensor assembly can further include an additional protrusion that does not include at least any of the sensing elements.

Reference will now be made in detail to the exemplary embodiments embodiments It should be understood that the following description is not intended to limit the embodiments to a preferred embodiment. On the contrary, the invention is intended to cover various alternatives, modifications, and equivalents of the embodiments of the invention as described in the appended claims.

The present disclosure relates to force sensing that can be incorporated into a wide variety of electronic or computing devices such as, but not limited to, computers, smart phones, tablets, trackpads, wearable devices, small-sized devices, and the like. Device. A force sensing device can be used to detect one or more user force inputs on an input surface, and then a processor (or processing unit) can correlate the sensed inputs with a force measurement and provide a And so on to the arithmetic device. In some embodiments, a force sensing device can be used to determine the force input to a trackpad, a touchscreen display, or another input surface.

The device can be configured to respond to force input or force input in a variety of ways. For example, a device can be configured to display a visual aid, and a user can interact with a visual cue by touching the surface of a touch screen. Visual cues can include application icons, virtual buttons, selectable areas, text entry areas, virtual buttons, or the like. The touch screen can detect the occurrence and location of a touch event. By incorporating a force sensor (such as disclosed herein), the device can detect not only the occurrence and location of a touch, but also the ability to detect one of the forces applied by the input. The device can then take different actions based on the applied force. For example, if a user touches an application icon with a force input below one of the thresholds, the device can open the application. If the user touches the application icon above one of the thresholds, the device can open a shortcut menu containing one of the additional visual cues associated with the application. As another example, a force sensor can be used to determine a weight associated with an applied force such that a device can be used as a scale. Other applications for force input are also envisaged.

The force sensing device can include an input surface, one or more sensing layers (such as capacitive sensing elements, drive layers, sensing layers, and the like), one or more spacer layers (eg, air gaps, deformable) Element), and a substrate or support layer. The input surface provides a user with an engagement surface, such as an exterior surface of a trackpad or a cover glass of a display. The force sensing device can be combined with other components of an electronic device, such as a touch screen, a display, or the like. In such cases, components of the force sensing device, such as one or more sensing layers, may be interspersed with other layers, such as a cover glass, a filter, a touch sensing layer, a backlight assembly, a display element ( For example, a liquid crystal display assembly), or the like.

A user input applied to one of the input surfaces of the force sensing device causes one or more layers of the force sensing device to deflect in one of the applied forces such that a spacer layer (eg, an air gap) collapses. This deflection changes the distance between the components of the force sensing device (such as the distance between two complementary sensing layers), which can be detected by the force sensing device and correlated with a particular applied force. When the spacer layer has completely collapsed (eg, the components defining the opposite sides of the gap have been in contact with each other), the additional force applied to the input surface will not result in a significant additional change in the distance between the layers of the force sensing device. That is, the force sensing device has reached its maximum detectable force.

The force sensing device described herein includes a first spacer layer, such as an air gap, and a second spacer layer, such as a deformable member, that produces a progressive deformation in response to an applied force. For example, an air gap and a deformable element may be disposed between the first sensing layer and the second sensing layer such that an applied force first causes the air gap to collapse, and once the air gap has completely collapsed, it may immediately cause The deforming element is compressed or otherwise deformed. As the applied force increases and the deformable element becomes more compressed, the deformable element imparts an increasingly higher reactivity to the applied force. Thus, a force sensing device comprising a deformable element and an air gap can sense a greater force for a given deflection than a force sensed in a force sensing device that does not contain one of the deformable elements. .

The force sensing devices described herein can also include contact sensors that indicate when adjacent layers of an air gap are in contact with each other (eg, when the air gap has completely collapsed). Such a touch sensor can be used to indicate to a processor or sensing circuitry whether the force sensing device is operating in an air gap force pattern or a deformable element force pattern, which can improve the quality of the force sensing device And / or accuracy.

Air gaps, deformable elements, and contact sensors can be used in a variety of different force sensing architectures having various numbers and configurations of spacer layers, sensing layers, contact sensors, and the like. Examples of such architectures are described herein.

1 through 2 show example electronic devices that can incorporate the force sensing devices described herein. For example, Figure 1 shows an electronic device 100 (e.g., a mobile computing device) that can incorporate the force sensing devices described herein. The electronic device 100 can include a housing 104 and a display 102. Display 102 can provide a visual output to one of the users in viewable area 108 of the user. The display 102 can be implemented using any suitable technique, including but not limited to the use of liquid crystal display (LCD) components, light emitting diode (LED) components, organic light emitting display (OLED) components, organic electroluminescent (OEL) components, and A multi-touch sensing touch screen like this. In some embodiments, display 102 can be used as an input device that allows a user to interact with mobile computing device 100. For example, the display can be a multi-touch touch screen LED display.

Device 100 can also include an I/O device 106. The I/O device 106 can be in the form of a home button that can be a mechanical button, a soft button (eg, a button that does not physically move but still accepts input), on a display One of the above illustrations or images and so on. Further, in some embodiments, I/O device 106 can be integrated as a component of cover member 110 and/or housing 104 of the electronic device. The device 100 can also include other types of I/O devices, such as a microphone, a speaker, a camera, a biometric sensor, and one or more ports, such as a network communication port and/or a power line port.

The cover member 110 can be positioned over the front surface of the device 100 (or a portion of the front surface). At least a portion of the cover member 110 can be used as an input surface for receiving touch and/or force input. Cover member 110 can be formed from any suitable material, such as glass, plastic, sapphire, or combinations thereof. In an embodiment, the cover member 110 covers the display 102 and the I/O device 106. The touch input and the force input can be received by covering a portion of the cover member 110 of the display 102 and by covering a portion of the cover member 110 of the I/O device 106.

In another embodiment, the cover member 110 covers the display 102 but does not cover the I/O device 106. The touch input and the force input can be received by covering a portion of the cover 110 of the display 102. In some embodiments, the I/O device 106 can be disposed in one of the openings or apertures formed in the cover member 110. The aperture can extend through the housing 104 and one or more components of the I/O device 106 can be positioned in the housing 104.

A force sensing device can be configured to detect force input on display 102. A force sensing device can also be configured to detect a force input on a portion of the housing 104, such as a rear or side of the housing 104, or around a frame portion of the display 102. In addition to the force sensing device, display 102 can also include one or more touch sensors, such as a multi-touch capacitive grid, or the like. In these embodiments, display 102 can detect both force input and position or touch input. The device 100 in FIG. 1 is embodied as a tablet (eg, a mobile computing device), but this is merely one example device that can include the force sensing device described herein. Examples of other devices that may include the force sensing devices described herein include other mobile computing devices, wearable electronic devices (eg, watches), mobile handsets, laptops or desktops, computer peripherals (eg, Provide a trackpad input to the computer), or the like.

2 shows a laptop 200 that includes a trackpad 206 (or other input surface), a display 202, and a housing 204. The outer casing 204 can extend partially around the track pad 206 and/or display 202. The force sensing device can be configured to detect force inputs on the trackpad 206, display 202, or both.

In another example (not shown), a force sensing device can be incorporated into a trackpad that can be coupled to a computer but housed in a separate housing or housing. For example, a separate trackpad including a force sensing device can be configured to connect to a computer as a peripheral input device, similar to a mouse or trackball.

3A is a cross-sectional view of the device 100 of FIG. 1 taken along line AA of FIG. 1, showing an assembly 300 that provides display, touch sensing, and force sensing functionality to the device 100. Or can be integrated with other components to provide such functionality. For example, FIG. 5, FIG. 12, FIG. 14, FIG. 16, FIG. 23A, and FIG. 26 illustrate a force sensing structure and/or device that can be integrated with the assembly 300 or an assembly similar to the assembly 300. Example.

Device 100 includes a cover 303 that is coupled to housing 104 and defines an exterior surface of device 100. The cover member 303 can be a single layer or can comprise multiple layers and can be formed from or comprise any suitable material(s), such as glass, treated glass, plastic, diamond, sapphire, ceramic. , oil resistant coatings, hydrophobic coatings, or the like. Device 100 may also include other internal components including circuit boards, cameras, sensors, antennas, processors, tactile elements, speakers, or the like, which are omitted from Figure 3A for clarity.

Cover 303 can be coupled to housing 104 via an interface member 305. Figure 3B is an expanded view of the zone 317 shown in Figure 3A, showing in detail the joint between the cover member 303 and the housing 104.

The interface member 305 can be or can include an adhesive that secures the cover member 303 to one of the lugs 307 or other features of the housing 104. For example, the interface member 305 can be a pressure sensitive adhesive (PSA), a heat sensitive adhesive (HSA), an epoxy, or other bonding agent. The interface member 305 can be flexible or rigid. Where the interface member 305 is flexible, it may be helpful to protect the cover member 303 (the cover member may include glass or other frangible material) from damage due to shock and impact. Additionally, as discussed herein with respect to Figures 23A-25, the interface member 305 can include or cooperate with a sensing element that can detect the degree of deformation of one of the interface members 305, along with suitable processing circuitry. Next, the degree of deformation detected by the interface member 305 can be used to determine information such as the force applied to one of the covers 303.

Referring to FIG. 3A, assembly 300 includes an upper stack 304, which may include one or more layers or components of a display, including a liquid crystal matrix, light emitting diodes (LEDs), light guides, filters, (eg, , polarizing filter), diffuser, electrode, shielding layer (eg, indium tin oxide layer), or the like. The upper stack 304 can be coupled to the cover 303, such as with a PSA, HSA, or the like. The upper stack 304 can also include sensing elements for detecting the presence and/or location of a touch input on the cover member 303, including, for example, capacitive sensing elements, resistive sensing elements, and the like.

The assembly 300 also includes a lower stack 308 that can be separated from the upper stack 304 above at least a portion of the lower stack 308 by an air gap 306. The air gap 306 separating the upper stack 304 from the lower stack 308 can be from about 25 microns to about 100 microns thick, although other sizes are possible. The air gap 306 can help prevent deformation of the assembly in the lower stack 308 in response to a force applied by one of the covers 303, which can cause undesirable optical artifacts on the display 102. For example, the lower stack 308 can include a light source, a light guide, a diffuser, or other optical component that, if rigidly coupled to the upper stack 304, can be deflected when a force is applied to the cover 303 at that time. By separating these elements from the upper stack 304 with an air gap 306, undesired deformation can be reduced.

The lower stack 308 can include a frame member 309 that supports other components of the lower stack 308 and couples the lower stack 308 to the upper stack 304. For example, the frame member 309 can support components of the lower stack 308 (including light sources, light guides, diffusers, sensing elements, or the like) in a spaced configuration relative to the upper stack 304 and/or the cover 303. ).

Frame member 309 can be coupled to upper stack 304 and/or cover member 303 and can extend into an interior volume of an electronic device. The frame member 309 can be coupled to the upper stack 304 and/or the cover member 303 by a bonding member 311 (which can be or include an adhesive or other bonding agent). Frame member 309 can be formed from any suitable material or include any suitable material such as metal, plastic, or the like. As described herein, the assembly 300 can include sensing elements for sensing a force applied to one of the covers 303. Such sensing elements may rely on the ability to electromagnetically interact with other sensing elements to determine the applied force. For example, a capacitive sensing layer may need to be capacitively coupled to a capacitive driving layer to detect a change in distance between the sensing layer and the driving layer. Accordingly, the frame member 309 can define an opening in a central portion of the frame member 309. The opening may reduce or eliminate interference, shielding, or other negative effects of one of the solid layers between the sensing elements. As shown, a stiffening member 312 formed of a dielectric material (or any other material that does not shield or otherwise interfere with the sensing layer and the drive layer) is disposed in the opening. In some embodiments, the stiffening member 312 can be omitted from the frame member 309 and the opening can remain unfilled.

Where the frame member 309 defines an opening to facilitate or improve electrical, capacitive, and/or electromagnetic interaction between the sensing elements, the opening may substantially coincide with a touch sensitive area of a display and/or display 102. Accordingly, the sensing element can be capable of providing force (or other) sensing functionality to substantially the touch sensitive area of the entire display and/or display 102.

The lower stack 308 can include one or more layers or components of a display. For example, the lower stack 308 can include a light source 313 that includes one or more LEDs, fluorescent light, or the like. Light source 313 can emit light into an optical stack 315 that includes one or more optical components including, but not limited to, reflectors, diffusers, polarizers, light guides (eg, lightguide films), and lenses ( For example, Fresnel lens). The lighting configurations shown in Figures 3A-3B are merely exemplary, and the lower stack 308 may include lighting configurations other than those shown in Figures 3A-3B.

Upper stack 304 and lower stack 308 are described above as including display elements. In applications where the assembly 300 does not provide display functionality, such as components in which the assembly 300 is a trackpad 206 or coupled to the trackpad 206, the upper stack 304 and the lower stack 308 may include components other than those described above. And/or layers, or may be omitted or replaced with other components.

A first spacer layer (such as an air gap 310) and a second spacer layer (such as a deformable element 314) are below the lower stack 308. The air gap 310 can be from about 0.5 mm to about 1.0 mm thick, although other sizes are possible.

The first spacer layer and the second spacer layer are configured to vary in thickness in response to an applied force. For example, one of the thicknesses of the air gap 310 (eg, the distance between opposing surfaces defining the air gap) may be reduced as a force is applied to the cover member 303. Similarly, the thickness of one of the deformable elements 314 can be reduced as a force is applied to the cover member 303.

The deformable element 314 can comprise any suitable material, such as polyfluorene oxide, polyurethane foam, rubber, gel, or the like. Additionally, the deformable element 314 can have any suitable structure, such as a plurality of flexible or deformable protrusions (as shown) that can be formed as cylinders, beams, pyramids, channels containing sidewalls, cones, undulations Projections, bumps, or the like. The deformable element 314 can also or alternatively comprise an open or closed cavity, such as a sponge or a foam. The deformable element 314 can also have a substantially homogeneous, non-porous composition. As yet another example, the deformable element 314 can comprise a plurality of discrete pieces of deformable material, such as dots, pads, or the like.

The foregoing materials and configurations for the first spacer layer and the second spacer layer are merely examples, however, and the first spacer layer and the second spacer layer may be formed of any suitable material or a combination thereof. For example, a first foam material may be substituted for the air gap 310, and the deformable element 314 may include a second foam material having a density, a thickness, a composition, or The spring coefficient is different from the first foam material. In another example, the first spacer layer and the second spacer layer can be substantially identical and can comprise the same material or be formed from the same material.

The deformable element 314 can be coupled to or adjacent to a base structure or layer 316. The base structure 316 can be a substrate or support layer dedicated to the assembly 300, or can be another component of an electronic device, such as a battery pack, a housing or a portion of a housing, a circuit board, or any other component.

3C-3E illustrate the physical response progress of the assembly 300 to one of the input forces 302 on the upper stack 304. As mentioned above, the input force 302 can correspond to a user touching a user input surface of an electronic device, such as a cover 303, with a finger, stylus, or other item. The input force 302 can be transmitted to the surface of the upper stack 304 through the cover member 303.

FIG. 3C illustrates a portion of assembly 300 (represented by region 301 in FIG. 3A) before input force 302 is applied to upper stack 304. FIG. 3D illustrates the assembly 300 after the force input has caused the upper stack 304 to deflect or flex enough to completely collapse the air gap 306. In particular, the upper stack 304 has been deflected toward the lower stack 308 such that the upper stack 304 is in contact with the lower stack 308 in at least one location. The stiffness of the upper stack 304 and the size of the air gap 306 can determine the force that causes the upper stack 304 to contact the lower stack 308. In some cases, even a slight touch from the user will be sufficient (eg, the user is not considered to be "pressing" the touch on the cover).

3E illustrates the assembly 300 after the force input has caused the lower stack 308 to deflect enough to completely collapse the air gap 310, thus contacting the lower stack 308 with the deformable element 314 and at least partially deforming the deformable element 314.

As used herein, the term "collapse" may mean that one of the layers is partially collapsed (eg, corresponding to any thickness of a material or an air gap at any location), or one of the layers is fully collapsed (eg, corresponding) The opposing surfaces defining an air gap at any location contact each other or reach a maximum deformation of one of the deformable materials.

4 is an example force versus deflection curve showing how a user input surface (eg, cover member 303) of one of the assemblies 300 of FIGS. 3C-3E is deflected in response to the force input. In particular, as the force increases from zero to a force threshold (eg, corresponding to point 402), the deflection increases along a first amount curve 406. In some cases, the first amount of variation curve 406 corresponds to the deflection of the assembly 300 until all of the air gaps in the assembly 300 (eg, the air gap 306 and the air gap 310) have completely collapsed. As the force increases beyond the force threshold (eg, point 402) and the deformable element 314 compresses, the deflection increases along a second amount curve 408 that extends from point 402 to point 404. Accordingly, the force threshold corresponds to the force that has changed from the collapse of only the air gap to the deformation of the deformable element.

The first amount of variation curve 406 can be substantially linear such that at any point in the first amount of variation curve 406, an incremental increase in force produces a substantially identical incremental increase in deformation of the cover member 303. In contrast, the second amount of variation curve 408 can be non-linear and can be plateau as the force increases. For example, an incremental increase in one of the forces at the beginning of the second amount of variation curve 408 may result in a greater amount of deformation of the cover member 303 than the same incremental increase in force at the end of the second amount of variation curve 408. . However, these quantitative curves are merely illustrative, and the force sensing devices described herein can exhibit any other force versus deflection or quantitative curve.

The systems and methods described herein, including the force sensing devices 500, 700, 900, and 1100 described below, facilitate detecting whether a force sensing device operates according to a first amount of variation curve 406 such that only the air gap collapses, or Operating according to the second amount varying curve 408 causes a deformable element to deform. Accurate force measurements can be provided by detecting different volume curves.

Although FIGS. 3A through 4 relate to the assembly 300 of the device 100, the components, structures, and operating principles of the assembly 300 can also be applied to other devices, such as the display 202 or track of the device 200 (or any other suitable device). Board 206. In the event that one of the displays is not present, some components of the assembly 300, such as the trackpad 206, may be omitted, replaced, or reconfigured. For example, upper stack 304 and lower stack 308 may include components other than display elements, or may be omitted or replaced with spacers or other components.

5 is a partial cross-sectional view of an example force sensing device 500 that can be incorporated into an electronic device (eg, device 100, 200) depicting a region similar to region 301 in FIG. 3A. The cover member 303 and the housing 104 are omitted for clarity.

The force sensing device 500 includes an upper stack 504, similar to the upper stack 304, which may include one or more layers or components of a display including a liquid crystal matrix, light emitting diodes (LEDs), light guides, filters An optical device, (eg, a polarizing filter), a diffuser, an electrode, or the like. The upper stack 504 can be configured to flex or flex in response to a force applied by one of the force sensing devices 500.

A first sensing element 505 is coupled to the upper stack 504 (for example, coupled to a cover 303 or to a component coupled to the cover 303, such as a filter) and is attached to one of the electronic devices Within the internal volume. The first sensing component 505 can be a capacitive sensing component that is configured to capacitively couple with another capacitive sensing component. For example, the first sensing component 505 can be capacitively coupled to a driving layer of a sensing layer (eg, the second sensing component 512, hereinafter) that facilitates the use of mutual capacitance to detect the sensing layer One distance from the drive layer. As another example, the first sensing element 505 can be a sensing layer rather than a driving layer. In yet another example, the first sensing element 505 can be configured to capacitively couple to a ground plane to facilitate the use of self-capacitance to detect a distance between itself and the ground plane. In yet another example, the first sensing element 505 can be capacitively coupled to a ground plane of a separate sensing layer.

In the examples of the description, the sensing elements are described as elements for capacitive sensing. However, other types of sensors (and sensor assemblies) can be used in place of or in addition to capacitive sensors. In fact, other types of sensors or sensing techniques can be used that can detect distance changes or absolute distances between components, or otherwise detect forces. For example, an inductive sensor, an optical sensor, a sonic or ultrasonic sensor, or a magnetic sensor can be used. Additionally, components of the sensor can be integrated into a force sensor as shown herein (eg, wherein the sensing elements are separated from one another by one or more layers, including air gaps, deformable layers, other components, Or similar, or the components of the sensor may be integrated in any other manner suitable for use with this type of sensor (eg, an optical sensor may include one or more light emitters instead of one sensing) Floor).

The first sensing element 505 can be coupled to the upper stack 504 in any suitable manner, such as with a pressure sensitive adhesive (PSA), a thermal adhesive (HSA), or the like. The first sensing element 505 can also be patterned on the upper stack 504, such as by physical vapor deposition, electron beam evaporation, sputter deposition, or any other suitable technique. The first sensing element 505 can be formed of any suitable material disposed on a substrate or include any suitable material disposed on a substrate, such as indium tin oxide (ITO).

A lower stack 508 can be disposed under the first sensing element 505 and separated from the first sensing element 505 by an air gap 506. Like air gap 306, air gap 506 can be any suitable thickness, such as from about 25 microns to about 100 microns.

The lower stack 508 can include any suitable components or layers, such as those described above with respect to the lower stack 308 (eg, LEDs, an optical stack, backlight, reflector, or light guide), and can be coupled to the upper stack 504 and/or The housing 104 is as described with respect to the lower stack 308 of Figure 3A (e.g., via the frame member 309). In embodiments where the force sensing device 500 does not include a display or does not provide display functionality, the lower stack 508 (and the upper stack 504) may include different components or be omitted.

The lower stack 508 can be coupled to and/or supported by a frame member, which can be similar to the frame member 309 in Figure 3A. The frame member can include a stiffening member 509 similar to the stiffening member 312 in Figure 3A. The stiffening member 509 can be formed from a dielectric material or include a dielectric material to facilitate or improve electrical, capacitive, and/or electromagnetic interaction between the sensing elements (eg, between the first sensing element 505 and the second sensing) Electrical, capacitive, and/or electromagnetic interaction between elements 512).

The frame member, and in particular the stiffening member 509, can support the lower stack 508 in a spaced configuration relative to the upper stack of the electronic device, a base structure 516, a deformable element 514, or one of the other components. FIG. 5 shows a second sensing element 512 coupled to a deformable element 514. However, in some cases, the second sensing element 512 can be coupled to the lower stack 508. In such cases, the second sensing element 512 can be coupled to the frame member, such as to one of the stiffening member 509 or the lower stack 508.

An air gap 510 separates the lower stack 508 from a second sensing element 512. Air gap 510 can be any suitable thickness, such as from about 0.5 mm to 1.0 mm.

The second sensing component 512 can be used in one of the sensing layers of a capacitive sensor and can be capacitively coupled to the first sensing component 505. The second sensing component 512 can include an array of discrete capacitive sensing regions that facilitate detecting a location (and/or a magnitude) of one of the force inputs on the upper stack 504. The second sensing element 512 can be formed of any suitable material or include any suitable material, such as ITO traces disposed on a substrate. The second sensing element 512 can be coupled to the deformable element 514, the stiffening member 509 (or other component or lower stack 508 of the frame member), or any other component or structure in the internal volume of the electronic device such that the second Sensing element 512 is between first sensing element 505 and a third sensing element 515 (discussed below).

An optional anti-adhesion layer 511 can be disposed on a surface defining one side of the air gap 510 to prevent temporary or permanent adhesion of the opposite sides of the air gap when they are in contact with each other. Thus, when an applied force is removed from a user input surface, the components of force sensing device 500 can be returned to or near their original orientation. The anti-adhesion layer 511 can be formed of any suitable material or include any suitable material, and can have any suitable shape or structure. For example, the anti-adhesion layer 511 can include pillars, protrusions, channels, or other structures that permit airflow therethrough to reduce or prevent the formation of a sealed region between the surfaces of the air gap 510 when the air gap 510 is completely collapsed. . In the absence of the anti-adhesion layer 511, such a sealed region may result in a negative pressure zone that acts similarly to the "suction cup", which prevents side separation of the air gap 510. The anti-adhesion layer 511 also prevents adhesion by other mechanisms or forces such as van der Waals forces, electrostatic forces, or the like.

The force sensing device 500 includes a deformable element 514 between the second sensing element 512 and a third sensing element 515. Similar to the deformable element 314, the deformable element 514 can comprise any suitable material (such as polyfluorene oxide, polyurethane foam, rubber, gel, or the like) and can have any suitable structure, Such as a plurality of flexible cylinders (as shown), beams, pyramids, cones, undulations, open or closed pockets, or the like. The deformable element 514 can deflect non-linearly with respect to an applied force, as described above.

The deformable element 514 is shown in FIG. 5 below the air gap 510 and between the second sensing element 512 and the third sensing element 515. However, the relative position of the air gap 510 and the deformable element 514 can be adjusted. For example, the deformable element 514 can be coupled to the lower stack 508.

The third sensing element 515 disposed between the deformable element 514 and a base structure 516 can be used for one of the capacitive sensing layers and can be capacitively coupled to the second sensing element 512. For example, the second sensing element 512 can be a sensing layer, and the third sensing element 515 can be a driving layer, thus forming a capacitive sensor across the deformable element 514.

The base structure 516 can be a frame, bracket, or support structure of one of the force sensing devices. In some cases, the base structure 516 is an assembly of an electronic device below a user input surface, such as a circuit board, a battery pack, a housing or an inner wall of the housing, or the like. The base structure 516 can be stiff or otherwise more resistant to deflection in response to an applied force than components above the base structure 516. Thus, once the air gap 510 has completely collapsed, the additional force can primarily deform the deformable element 514 rather than deflecting the base structure 516.

The first sensing element 505, the second sensing element 512, and the third sensing element 515 can form two capacitive sensors. For example, as described above, the first sensing element 505 and the third sensing element 515 can each function as a distinct driving layer, and the second sensing element 512 can be capacitively coupled to the first sensing element 505 And a sensing layer of both the third sensing element 515 (and sensing a change in distance to both the first sensing element 505 and the third sensing element 515).

The second sensing component 512 is a shared sensing layer, which may include a first group of sensors for detecting the distance to the first sensing component 505 and for detecting to the third sensing component 515. A second set of sensors at a distance. The second sensing element 512 can also or alternatively use the same sensor to detect the distance to both the first sensing element 505 and the third sensing element 515. In the latter case, the first sensing element 505 and the third sensing element 515 can be driven with different electrical signals, thus allowing the second sensing element 512 (and/or the sensing circuitry coupled to the second sensing element 512) The change in capacitance caused by the change in the size of one of the air gaps 510 and the change in capacitance caused by the change in the size of one of the deformable elements 514 are distinguished. In another embodiment (not shown), the second sensing element 512 can be replaced with two discrete sensing elements, each sensing element being used as the first sensing element 505 and the third sensing element 515. A sensing layer of one of the different ones.

6 is an example force versus deflection curve showing how the force sensing device 500 of FIG. 5 is deflected in response to (directly or indirectly) applying a force input to the upper stack 504. The force response is similar to that shown in Figure 4, wherein a first quantity curve is from point 401 to point 402 (corresponding to the collapse of air gaps 506 and 510) and a second quantity curve is from point 402 to point. 404 (corresponding to the deformation of the deformable element 514).

As mentioned above, the force sensing device 500 has two capacitive sensors: a first capacitive sensor 518 formed by the first sensing element 505 and the second sensing element 512; and a second A capacitive sensor 519 is formed by the second sensing element 512 and the third sensing element 515. The first capacitive sensor 518 spans the air gaps 506 and 510, and the second capacitive sensor 519 spans the deformable element 514. Accordingly, the first capacitive sensor 518 is positioned within the force sensing device 500 to detect deformation of the upper stack 504 along the line 602 in FIG. 6, and the second capacitive sensor 519 is positioned at the force sensing device 500. Internally, the deformation of the upper stack 504 along line 604 in FIG. 6 is detected. By detecting the deformation of the air gaps with a sensor and deforming the deformable elements with a different sensor, the sensing circuitry can process the signals according to different force deflection correlations. For example, the deflection from the first capacitive sensor 518 can be cross-correlated with an applied force based on a substantially linear magnitude curve between point 401 and point 402, and can be based on point 402 and point 404. The non-linear magnitude curve between the two causes the deflection from the second capacitive sensor 519 to be cross-correlated with an applied force. Of course, the linear quantity change curve and the non-linear quantity change curve shown in FIG. 6 are merely examples, and the deformation of a force sensing device may follow or exhibit different quantitative curves.

The sensing circuitry can apply the force deflection correlation in any suitable manner. For example, the force deflection correlation can be implemented in accordance with a mathematical function that outputs a particular force value for a particular determined deflection amount (which can then be based on a measured or detected capacitance value, or any other electrical measurement or value). Determined). As another example, a force deflection correlation can be implemented using a lookup table in which a particular deflection value is correlated with a particular force value. Other techniques are also possible, and these examples do not limit the mathematical or programming techniques that can be used to generate force values from measured or detected electrical properties (eg, capacitance, resistance, current, signal, etc.).

7 is a developed view of sensing elements 505, 512, and 515 of force sensing device 500 of FIG. 5, showing an example configuration of sensing elements in one embodiment of force sensing device 500, Capacitive sensing is used to detect changes in the distance between the sensing elements. FIG. 7 omits the components of the force sensing device 500 and the electronic device in which the force sensing device is configured. For example, FIG. 7 omits the deformable element 514 shown between the second sensing element 512 and the third sensing element 515. Additionally, for clarity, Figure 7 omits some details of the sensing elements 505, 512, 515, such as conductive traces or leads to couple the sensing elements (or portions thereof) to other electrical circuitry.

As mentioned above, in the force sensing device 500, the first sensing element 505 and the third sensing element 515 can be used in a driving layer of a capacitive sensing solution, and the second sensing element 512 can be connected to the first sensing element 512. Sensing layer. In operation, an electrical signal (such as a substantially sinusoidal signal, a square or edge signal (eg, a substantially instantaneous transition from a first voltage to a second voltage), or any other suitable signal) may be used to excite the first A sensing element 505 and a third sensing element 515 (also referred to as driving layers 505, 515). The nature of the signal, such as frequency, voltage, or amplitude, can be selected to avoid or minimize other electronic circuitry that interferes with a device, such as display circuitry, processors, antennas, and the like. Because the second sensing component 512 (also referred to as a sensing layer) is capacitively coupled to a driving layer, a corresponding electrical signal can be induced (or otherwise detected by the sensing layer) in the sensing layer. . For a given electrical signal to be applied to the drive layer, the induced electrical signal in the sense layer may differ depending on the distance between the drive layer and the sense layer. Thus, force sensing device 500 (or associated sensing circuitry) can determine the distance between the drive layer and the sensing layer by analyzing the signals induced in the sensing layer.

The first drive layer 505 can include a conductive material that is coupled or otherwise applied to one of the substrates. For example, the first drive layer 505 can include a layer of ITO, nanowires (eg, a metal nanowire that includes silver or gold nanowires), or any other suitable material. As shown in FIG. 5, the drive layer 505 is disposed in the light path of the display 102 (eg, the drive layer 505 is above the lower stack 508 and the lower stack 508 is generated to illuminate the display 102). Thus, the conductive material can be substantially transparent. Even when a substantially transparent material is used, the material is visible on display 102 if it is configured in a regular pattern, such as by a grid or row. Accordingly, the conductive material of the first drive layer 505 can be substantially evenly distributed (eg, as a layer, sheet, coating, or other continuous element) on the first drive layer 505 rather than in a regular pattern. In some cases, the conductive material can be a continuous layer that covers or extends over the entire surface of one of the substrates of the first drive layer 505 (or substantially an entire surface, such as the surface area of the substrate) 80% or more). The layer of conductive material can be configured such that the border or edge of the layer is not positioned within the boundaries of a display into which the force sensing device 500 is incorporated.

The first drive layer 505 can also include a connection element 706 that is electrically coupled to the conductive material and that facilitates coupling of the conductive material to other electronic components or circuitry. Connecting element 706 can be formed of any material or include any material such as silver, copper, nickel vanadium, or any other suitable material. The connecting element 706 can form a continuous frame (as shown) along an outer portion of the first drive layer 505, or the connecting element 706 can be formed by discrete or distinct segments. In some cases, the connecting element 706 does not form a frame, but instead may be, for example, a strip along one side of the first drive layer 505. Other configuration systems are also available. Connecting elements 706 are discussed herein with respect to Figures 26-29 and 32-40, such as conductive strips (or any other conductive substrate, layer, coating, etc.) formed on one edge of a drive layer 505.

The sensing layer 512 can include a sensing region 702 formed of a conductive material (or including a conductive material) and configured in a regular pattern, such as a grid. Sensing region 702 can be formed from any suitable material or include any suitable material, such as ITO, metal nanowires, or the like.

Each of the sensing regions 702 can be used as a discrete region or pixel-like region that can be used to determine a distance between the first driving layer 505 and the particular sensing region. By analyzing all of the sensing regions 702, the force sensing device 500 can detect an amount of force applied to one of the covers 303. Additionally, pixelation of the sensing layer 512 as shown may allow the force sensing device 500 to more accurately detect force than if a single, uniform sensing layer were used. For example, if a single sensing layer is used, it may be difficult or impossible to tell the difference between one of the forces exerted near an edge cover 303 and a small force applied near a center cover 303. By using a pixelated sensing layer 512, the force sensing device 500 can account for differences in stiffness of different regions of the cover member 303. The use of a pixelated sensing layer 512 may also allow the force sensing device 500 to determine the position of an applied force, detecting a multi-touch input (eg, corresponding to multiple fingers or stylus applied to the cover 303) Or similar.

The second drive layer 515 can include a plurality of drive regions 704. Like the first drive layer 505 and the sense region 702 of the sense layer 512, the drive region 704 can be formed of any suitable conductive material or include any suitable conductive material, such as ITO, metal nanowires, or the like.

Drive region 704 can be configured in any suitable pattern or orientation and can have any suitable size. For example, the drive region 704 can be a plurality of substantially rectangular regions of conductive material and can be substantially aligned with one of the sense regions 702 in the sense layer 512, as shown and described with respect to FIG. Accordingly, the drive regions 704 can each overlap with the sensing region 702 of the sensing layer 512.

As with the first drive layer 505, the drive region 704 can be excited by an electrical signal (eg, a substantially sinusoidal or edge signal) that induces a corresponding signal in the sense region 702 of the sense layer 512 (or can otherwise be The sensing layer 512 detects). Because a single sensing layer 512 is used to detect the distance between the sensing layer 512 and the two different driving layers 505, 515, the force sensing device 500 must distinguish between the first driving layer 505 and the second driving layer. Signal of 515. Accordingly, the signals from the first drive layer 505 and the second drive layer 515 can have different frequencies, amplitudes, phases, or other properties such that the signals can be induced differently from one another in the sense layer 512. More specifically, the signal applied to the first drive layer 505 can have a first frequency, and the signal applied to the second drive layer 515 can have a second frequency that is different from the first frequency. Alternatively or in addition, the first drive layer 505 and the second drive layer 515 can be excited at different times (eg, with an edge signal) such that signals induced in the sense layer 512 can be attributed to a drive layer or other drive layer . For example, the sensing circuitry can alternately excite the first drive layer 505 and the second drive layer 515. These (or other) techniques can be used such that the distance between the first drive layer 505 and the sense layer 512 and the distance between the second drive layer 515 and the sense layer 512 can be independently detected.

Drive regions 704 can be electrically isolated from one another or can be electrically coupled to each other. In embodiments in which the drive regions 704 are electrically coupled to one another, all of the drive regions 704 can be simultaneously activated by a single signal.

Alternatively, where the drive regions 704 are electrically isolated, the drive regions can be driven or fired independently of each other. This can be used when not all of the sensing regions 702 are analyzed at one time. More specifically, the circuitry associated with force sensing device 500 can cyclically poll a subset of sensing regions 702. Accordingly, drive region 704 can correspond to a polling group of sensing regions 702, and a signal can be provided to driving region 704 when a corresponding group of sensing regions 702 is being polled. This may help reduce the power consumption of the force sensing device 500 when a cyclic polling technique is used, since no energy is supplied to all of the driving regions 704 when the corresponding sensing region 702 is not polled.

The drive layers 505, 515 and the sense layer 512 can be separate layers or components, as shown in Figure 7, or the like can be incorporated into other layers or components. For example, the first driving layer 505 can be coated on a polarizing filter, applied to a polarizing filter, or otherwise combined with a polarizing filter. The polarizing filter is The components of stack 304 (Fig. 3A). In fact, the conductive material of any of the sensing layer and the driving layer can be incorporated on another component or layer of the electronic device in which the sensing layer and the driving layer are incorporated. Alternatively, the sensing layer and the driving layer may be formed separately, such as by applying a conductive material to the substrate, such as a flexible circuit material (eg, polyethylenimine, polyethylene terephthalate) ), polyetheretherketone, or transparent conductive polyester), and then, incorporating the substrate into an electronic device.

8 is a partial cross-sectional view of the first driving layer 505 and the second driving layer 515 and the sensing layer 512 taken along line CC of FIG. 7, illustrating the sensing region 702 and the driving region of the force sensing device 500. The relative size and location of 704. The first driving layer 505 includes a substrate 802, a conductive layer 804, and a connecting member 706. Substrate 802 can be any suitable material or component, such as a flexible circuit material, a polarizing filter, or any other material or component of an electronic device or display stack. Conductive layer 804 can be ITO, a layer of metal or conductive nanowire, or any other suitable material, as described above. Conductive layer 804 can be a continuous sheet of overlap with multiple sensing regions 702 (eg, having a single piece of conductive material rather than a segmented or pixelated configuration). Connection element 706 can be a conductive material such as copper, silver, nickel vanadium, or the like.

Sensing layer 512 can include a substrate 806 (which can be any suitable material or component, such as a flexible circuit material) and a sensing region 702. As described above, the sensing region 702 can be formed from any suitable material or include any suitable material, including ITO, conductive nanowires, or the like.

The second drive layer 515 can include a substrate 808 (which can be any suitable material or component, such as a flexible circuit material), and a drive region 704. The drive region 704 and the sense region 702 of the sense layer 512 can be sized and positioned relative to each other such that the sense region 702 shields the drive region 704 from interference sources, such as the first drive layer 505. For example, the width of the drive region 704 can be substantially the same or narrower than the sensing region 702, and the sensing region 702 can be vertically aligned (where the position is worded relative to the orientation of the layer in FIG. 8). In this manner, the conductive material of the sensing region 702 can substantially shield the drive region 704 from the first drive layer 505 or other potential sources of interference above the sensing layer 512. Portions of the drive region 704 may not be directly covered by a sense region 702. However, if the second drive layer 515 is a single continuous sheet of conductive material, the unshielded regions of the substantially rectangular drive region 704 are significantly smaller than, for example, would be present on the first drive layer 505.

Figure 8 shows the sensing region 702 and the driving region 704 extending away from the surface of their respective substrates. However, this is only an example configuration. In fact, the sensing region 702 and the driving region 704 can be substantially flush with or recessed in their respective substrates.

FIG. 9 shows a sensing layer 512 containing an example distribution of one of the sensing regions 702. FIG. 9 also shows a conductive path 902 that can electrically couple the sensing region 702 to other electronic components or circuits. Conductive path 902 can be any suitable material and can be formed in any suitable manner. For example, the conductive paths can be formed by ITO applied using a lithography technique. Other materials and technologies are also envisaged. In embodiments in which the sensing region 702 is independently polled to provide a unique force value for a particular display location (as shown in FIG. 9), each sensing region 702 can be coupled to a unique conductive path 902. In embodiments in which multiple sensing regions 702 are polled or monitored as a single unit, their sensing regions 702 can be shared or connected to a common conductive path 902 (not shown). The pattern of sensing regions 702 and conductive paths 902 shown in FIG. 9 is merely one example of a suitable configuration, and other configurations are contemplated, including the number and configuration of sensing regions 702 and conductive paths 902.

10A shows a first drive layer 505 showing an example of an electrical connection to one of the conductive layers 804 of the first drive layer 505 via a connection element 706 (eg, a strip or bezel around one of the first drive layers 505). configuration. In particular, FIG. 10A illustrates a pair of connector segments 1002 positioned proximate to the connecting element 706. Each connector segment 1002 can be formed from an electrical conductor or include an electrical conductor that is electrically coupled to a signal generator or other electronic circuitry. For example, connector segment 1002 can be formed from a flexible circuit material that contains a metal or conductive material (eg, copper, gold, ITO) disposed thereon. In some cases, connector segment 1002 can be formed substantially entirely of conductive material, such as when connector segment 1002 is a piece of copper, silver, or any other metal or conductive material.

A conductive bonding material 1004 can be deposited over the connector segment 1002 and a portion of the connecting component 706 such that an electrical connection is formed between the connector segment 1002 and the connecting component 706. The conductive material can be any suitable material such as silver, gold, copper, conductive adhesive, or the like.

As mentioned above, the connection element 706 is electrically connected to the conductive layer 804. Accordingly, a drive signal can be applied from the connector segment 1002 to the conductive layer 804. In some cases, more or fewer connector segments 1002 can be used to electrically couple the circuitry to the conductive layer 804, or the connector segments 1002 can be positioned at different locations around the drive layer 505, such as along the drive layer 505. The opposite edge.

FIG. 10B shows a first driving layer 505 showing another example configuration of electrical connection to one of the conductive layers 804 of the first driving layer 505. As shown, the first drive layer 505 does not include the connection element 706. In this example, connector segment 1006 is coupled to conductive layer 804 via a conductive adhesive 1008 rather than to conductive layer 804 via connection element 706 (as shown in FIG. 10A). As with connector segment 1002 (Fig. 10A), connector segment 1006 can be formed from an electrical conductor or include an electrical conductor that is electrically coupled to a signal generator or other electronic circuitry. Connector segment 1006 can be electrically and physically coupled to conductive layer 804 via conductive adhesive 1008, and conductive adhesive 1008 can be disposed between the overlapping portions of connector segment 1006 and conductive layer 804. FIG. 10B illustrates an example embodiment in which two connector segments 1006 are coupled to opposite sides of the first drive layer 505. Other configurations are also contemplated that include different numbers, sizes, shapes, and coupling locations of connector segments 1006. For example, in some cases, only one connector segment 1006 is used. In other cases, the four connector segments 1006 are configured to wrap around the first drive layer 505 (eg, one of the connector segments 1006 is on each side of the first drive layer 505).

FIG. 11 shows a second drive layer 515 containing an example distribution of one of the drive regions 704. Figure 11 also shows a conductive path 1102 that can electrically couple the drive region 704 to other electronic components or circuits. Conductive path 1102 can be any suitable material and can be formed in any suitable manner. For example, the conductive paths can be formed by ITO applied using a lithography technique. Other materials and technologies are also envisaged. In embodiments in which the drive region 704 is independently driven or fired, as discussed above with respect to FIG. 8, each drive region 704 can be coupled to a unique conductive path 1102. In embodiments in which multiple drive regions 704 are driven or excited together (eg, a signal is simultaneously applied to multiple drive regions 704), their drive regions 704 may share or be connected to a common conductive path (not shown). The pattern of drive region 704 and conductive path 1102 shown in FIG. 11 is merely one example of a suitable configuration, and other configurations are contemplated, including the number and configuration of drive region 704 and conductive path 1102.

12 is a partial cross-sectional view of an example force sensing device 1200 that can be incorporated into an electronic device (eg, device 100, 200) depicting a region similar to region 301 in FIG. 3A. The cover member 303 and the housing 104 are omitted for clarity. While the force sensing device 1200 is similar to the force sensing device 500, the force sensing device 1200 has different numbers and configurations of sensing elements within the electronic device, as described herein.

The force sensing device 1200 includes an upper stack 1204, similar to the upper stack 304. The upper stack 1204 can include one or more layers or components of a display including a liquid crystal matrix, light emitting diodes (LEDs), light guides, filters An optical device, (eg, a polarizing filter), a diffuser, an electrode, or the like. The upper stack 1204 can be configured to flex or flex in response to a force applied by one of the force sensing devices 1200.

A lower stack 1208 can be disposed below the upper stack 1204 and separated from the upper stack 1204 by an air gap 1206. The lower stack 1208 can include a frame member 1207 (similar to the frame member 309), an optical stack 1213 (similar to the optical stack 315 described above), and any other suitable components, such as a light source. As described with respect to assembly 300, air gap 1206 can be any suitable thickness, such as from 25 microns to 100 microns. In embodiments where the force sensing device 1200 does not include a display or does not provide display functionality, the lower stack 1208 (and the upper stack 1204) may include different components or be omitted.

A first sensing element 1209 is coupled to the lower stack 1208. The first sensing element 1209 can be a capacitive sensing element that is configured to capacitively couple with another capacitive sensing element. For example, the first sensing element 1209 can be capacitively coupled to a driving layer of a sensing layer (eg, the second sensing element 1215, described below) that facilitates the use of mutual capacitance to detect the sensing One distance between the layer and the drive layer. As another example, the first sensing element 1209 can be a sensing layer rather than a driving layer. As yet another example, the first sensing element 1209 can be configured to capacitively couple to a ground plane and facilitate detection using a self-capacitance to detect a distance between itself and the ground plane. In yet another example, the first sensing element 1209 can be capacitively coupled to a ground plane of a sensing layer.

The first sensing element 1209 can be formed of any suitable material or include any suitable material, such as ITO traces disposed on a flexible substrate, and can be coupled to the lower portion in any suitable manner, such as with a PSA or HSA. Stack 1208, or directly patterned onto lower stack 1208. Because the first sensing element 1209 is below the lower stack 1208, the frame member 1207 of the lower stack 1208 can be formed from a conductive material, such as a metal. More specifically, because the frame member 1207 is not tied between the first sensing element 1209 and a second sensing element 1215 (discussed below), the frame member 1207 may be unshielded or otherwise negatively interfered with the first Capacitive coupling between sensing element 1209 and second sensing element 1215. Accordingly, more material can be suitably used in the frame member 1207, and the frame member 1207 can define a continuous layer or panel instead of having one of the openings to avoid undesired shielding or interference.

An air gap 1210 and a deformable element 1214 can be disposed between the first sensing element 1209 and a second sensing element 1215. Air gap 1210 and deformable element 1214 correspond to air gap 510 and deformable element 514 and may have similar compositions, structures, dimensions, and functions.

The second sensing component 1215 can be capacitively coupled to the first sensing component 1209, and the components together can form a capacitive sensor 1218 across the air gap 1210 and the deformable component 1214 to detect distortion of the layers. Depending on the operating principle of the capacitive sensor 1218 and/or the configuration of the first sensing element 1209, the second sensing element 1215 can be a sensing layer, a driving layer, or a ground plane.

The second sensing element 1215 can be coupled to a base structure 1216 that can be a frame, a bracket, a circuit board, a battery pack, an inner wall of a housing or housing, or the like, as above This is described with respect to the base structure 516 of FIG.

13 is an example force versus deflection curve illustrating how the force sensing device 1200 of FIG. 12 is deflected in response to (directly or indirectly) applying a force input to the upper stack 1204. The force response is similar to that shown in Figure 4, wherein a first quantity curve extends from point 401 to point 402 (corresponding to the collapse of air gaps 1206 and 1210) and a second quantity curve extends from point 402 to point 404 (corresponding to the deformation of the deformable element 1214).

As mentioned above, the force sensing device 1200 has a capacitive sensor 1218 formed by a first sensing element 1209 and a second sensing element 1215. The first sensing element 1209 and the second sensing element 1215 span the air gap 1210 and the deformable element 1214, but do not span the air gap 1206. Therefore, the capacitive sensor 1218 does not detect the deflection of the upper stack 1204 that causes the air gap 1206 to collapse (corresponding to line 1302 in FIG. 13), but detects the deflection that causes the air gap 1210 to collapse and the deformable element 1214 to deform. (corresponding to line 1304 in Figure 13). Accordingly, the collapse of the air gap 1206 is decoupled from the collapse of the air gap 1210, and one of the forces detected by the capacitive sensor 1218 using the force sensing device 1200 corresponds to the force required to collapse the air gap 1210.

Because the capacitive sensor 1218 spans the air gap 1210 and the deformable element 1214, the sensing circuitry coupled to the first sensing element 1209 and the second sensing element 1215 can be configured to determine when to algorithmize The air gap 1210 has completely collapsed. For example, the sensing circuitry can monitor a rate of change of deformation (eg, a slope of the force relative to the deflection curve) when a force is applied. If the slope satisfies a first condition (eg, the slope is constant or is below a threshold value), the sensing circuitry can determine that only the air gap 1210 is collapsing or collapsed, and one can be applied The first force deflection correlation. If the slope satisfies a second condition (eg, the slope increases or is above the threshold), the sensing circuitry can determine that the air gap 1210 has collapsed completely and the deformable element 1214 is about to deform or has been at least partially Deformation. In the latter case, the sensing circuitry can apply a second force deflection correlation to determine a value of the applied force.

14 is a partial cross-sectional view of an example force sensing device 1400 that can be incorporated into an electronic device (eg, device 100, 200) depicting a region similar to region 301 in FIG. 3A. In this example, the force sensing device 1400 is the same as the force sensing device 1200, but the first sensing element 1209 is coupled to the upper stack 1204 such that the capacitance formed by the first sensing element 1209 and the second sensing element 1215 is sexy. The detector 1402 is excluded from both the air gap 1206 and the air gap 1210. Accordingly, capacitive force detector 1402 detects deflection of upper stack 1204 from point 401 to point 404 (corresponding to line 1502) as depicted in FIG. 15 relative to the deflection curve. Additionally, as described herein, the sensing circuitry can be configured to determine, in the form of an algorithm, when the air gap 1210 and optionally the air gap 1206 have completely collapsed to apply a suitable force deflection correlation.

In FIG. 12, although the frame member 1207 is not between the first sensing element 1209 and the second sensing element 1215, the frame member 1207 in FIG. 14 is attached to the first sensing element 1209 and the second sensing element. Between 1215. Accordingly, the frame member 1207 can be formed from a dielectric material or can have a dielectric material positioned in one of the openings such that the frame member 1207 does not shield or otherwise interfere with the sensing elements 1209, 1215.

16 is a partial cross-sectional view of an example force sensing device 1600 that can be incorporated into an electronic device (eg, device 100, 200) depicting a region similar to region 301 in FIG. 3A. In this example, the force sensing device 1600 includes an upper stack 1604 (corresponding to the upper stack 1204), a first sensing element 1605 (corresponding to the first sensing element 1209), and an air gap 1606 (corresponding to Air gap 1206), lower stack 1608 (corresponding to lower stack 1208), a deformable element 1610, an air gap 1615, a second sensing element 1614, and a base structure 1620 (corresponding to base structure 1216). The lower stack 1608 can include an optical stack 1617 and a frame member 1607 that supports the optical stack 1617 and couples the lower stack 1608 to the upper stack 1604. Because the frame member 1607 is between the first sensing element 1605 and the second sensing element 1614 (similar to the configuration in the force sensing device 500, Figure 5), the frame member 1607 can be formed from a dielectric material. Or a dielectric material, such as one of the dielectric members disposed in one of the openings in the frame member 1607.

The first sensing element 1605 and the second sensing element 1614 form a capacitive sensor 1619 that spans both the air gap 1606 and the air gap 1615. Thus, as in force sensing device 1400, capacitive sensor 1619 detects collapse corresponding to both air gaps 1606, 1615 and deformation of deformable element 1610. Accordingly, capacitive force detector 1619 detects the deflection of upper stack 1604 from point 401 to point 404 (corresponding to line 1702) as illustrated in force in FIG. 17 relative to the deflection curve.

The force sensing device 1600 also includes a touch sensor configured to detect contact between the upper stack and the lower stack. As shown in FIG. 16, the touch sensor is integrated with the deformable element 1610 and the second sensing element 1614. For example, the deformable element 1610 can include a protrusion 1611 that extends from a base portion of the deformable element 1610. The protrusion 1611 can include a sensing element 1612 that is configured to sense or otherwise detect when the air gap 1615 is detected by a contact sensing area (eg, a contact sensing area 1616, discussed herein). The fully deformed component and the deformable element 1610 contact the second sensing element 1614. As shown in FIG. 16, sensing element 1612 is disposed at the free end of protrusion 1611.

Sensing element 1612 can be formed from any suitable material and can have any suitable size and shape. These properties of the sensing element 1612, as well as any other properties, can be selected based on the operating principles of the touch sensor. For example, if a contact sensing region 1616 is a capacitive sensor, the sensing component 1612 can be a conductive material, and/or a dielectric material. A suitable dielectric material can have a dielectric constant (or relative dielectric constant) greater than about 3.9 (eg, a high-k dielectric material). The contact sensing area 1616 is a continuous sensor, and the sensing element 1612 can be a conductive material such as carbon, metal, or the like.

The sensing element 1612 can be incorporated into the deformable element 1610 in any suitable manner. For example, the sensing element 1612 can be co-molded with the deformable element 1610. In another example, sensing element 1612 can be deposited on deformable element 1610. For example, one or more layers of metal (or any other suitable material) may be deposited on the free ends of the protrusions 1611. In yet another example, the deformable element 1610 can be formed from a material that is itself configured to be sensed by a corresponding contact sensing region 1616, and thus the discrete sensing element 1612 can be eliminated. For example, the material can be polyoxygenated or other elastomers containing conductive particles (such as carbon) embedded therein. Other materials and techniques for integrating the material with the deformable element 1610 are also contemplated.

The force sensing device of the touch sensor 1600 also includes a contact sensing region 1616 that is configured to detect the sensing element 1612 to determine when the air gap 1615 has completely collapsed and the deformable element 1610 has begun to be compressed. The contact sensing area 1616 can be configured to detect the sensing element 1612 in any suitable manner. For example, the contact sensing region 1616 can include a capacitive sensing component configured to detect a change in capacitance caused by the proximity of the sensing component 1612 to the contact sensing region 1616. . As another example, the contact sensing region 1616 can include an electrical switch configured to detect a closed circuit when a conductive sensing component 1612 contacts the electrical switch.

Contact sensing region 1616 can be integrated with second sensing element 1614. For example, the contact sensing region 1616 for contact sensing and the sensing region for the capacitive force sensor 1619 can be patterned on the same substrate or otherwise incorporated into the same substrate in. As another example, the contact sensing region 1616 can be disposed on top of the second sensing element 1614. For example, a contact sensing region 1616 including an electrical contact, a capacitive sensing component, or the like can be placed on top of the second sensing component 1614 and selectively adhered to the second sensing component 1614.

Similar to the force sensing device 1400 of FIG. 14, the force sensing device 1600 forms a capacitive sensor 1619 that spans both the air gap 1615 and the deformable element 1610, and thus the capacitive sensor 1619 exhibits an extension from point 401. A force to point 404 (corresponding to line 1702) is in response to the curve (shown in Figure 17). However, when the force sensing device 1600 is operated according to a first force curve (eg, from point 401 to point 402) or a second force curve (eg, from point 402 to point 404), the capacitive sensor 1619 may not provide A discrete indication. The force sensing device of the touch sensor 1600 provides this indication, allowing the sensing circuitry to apply a suitable force deflection correlation. For example, the sensing circuitry can be applied to the air gap 1615 before the air gap 1615 is completely collapsed and before the contact sensor indicates a contact event (corresponding to point 1704 in FIG. 17). A first force deflection correlation of collapse (from point 401 to point 402). After the air gap 1615 has completely collapsed, as detected and indicated by a signal from one of the contact sensors (at point 1704), the sensing circuitry can apply compression corresponding to the deformable element 1610 (eg, A second force deflection correlation from point 402 to point 404).

Although FIG. 16 illustrates an embodiment in which the first sensing element 1605 is disposed on the upper stack 1604, and thus includes an air gap 1606 in a space between the first sensing element 1605 and the second sensing element 1614. , but other configurations are possible. For example, the first sensing element 1605 can be disposed on the lower stack 1608 on the opposite side of the air gap 1606, or can be disposed between the lower stack 1608 and the deformable element 1610. No matter where the first sensing component 1605 and the second sensing component 1614 are located in the force sensing device 1600, an air gap, a deformable component, and a contact sensor may be disposed on the first sensing component 1605 and Between the second sensing elements 1614. In addition, FIG. 16 illustrates that the deformable element 1610 is positioned on the lower stack 1608 with the protrusion 1611 extending toward the base structure 1620 and the contact sensing region 1616 being illustrated on the base structure 1620. In other embodiments, the relative positioning of the components can be swapped such that the deformable element 1610 is positioned on the base structure 1620 with the protrusions 1611 extending toward the lower stack 1608 and the sensing regions 1616 positioned on the lower stack 1608. It will be appreciated that this modification can produce at least an equivalent result with respect to the operation of the deformable element 1610 and the contact sensing region 1616.

18A is an expanded view of region 1800 of FIG. 16 showing an example configuration of a protrusion 1611, a sensing element 1612, and a contact sensing region 1616 that can form the contact sensor of FIG. . The second sensing element 1614 can include a sensing region 1810 (such as a capacitive plate or lead capacitively coupled to a ground or drive layer), and a contact sensing region 1616. The contact sensing region 1616 in FIG. 18A includes leads 1802, 1804, 1806, and 1808. The leads can be of any suitable material (such as traces, wiring, plates, pads, or the like of conductive materials (eg, metal, carbon, ITO)) and can be coupled for detecting contact with sensing element 1612 or Suitable circuitry to the proximity of sensing component 1612. For example, the leads can be capacitive elements that facilitate detecting a change in capacitance caused by the sensing element 1612 being in contact with the lead or the proximity lead. By way of another example, the leads can be electrical contacts that facilitate detecting a closed circuit between one or more of the contacts.

FIG. 18B illustrates region 1800 in FIG. 16 when air gap 1615 has completely collapsed and deformable element 1610 is in contact with second sensing element 1614. As shown, the proximity or contact between the sensing element 1612 and the leads 1802, 1804, 1806, and 1808 results in detection by the corresponding pair of leads 1802, 1804, 1806, and 1808. Although FIGS. 18A-18B illustrate four leads, this is merely an example, and more or fewer leads may be used. Additionally, the relative sizes of contact sensing region 1616, sensing element 1612, and leads 1802, 1804, 1806, and 1808 are merely exemplary and may be selected based on various factors and considerations. For example, the contact sensing region 1616 can be large enough to accommodate under-alignment between the deformable element 1610 and the contact sensing region 1616. Thus, even if the centers of the protrusions 1611 and the contact sensing regions 1616 are not exactly aligned, the contact sensor will still effectively detect when the air gap 1615 has completely collapsed.

Figure 19 shows an example of a deformable element 1610 or a portion thereof. The deformable element 1610 includes an array of protrusions 1611 extending from a substrate surface 1900. The protrusion 1611 may be integrally formed with the base surface 1900. For example, the deformable element 1610 can be molded (eg, injection molded) into a monolithic, monolithic assembly of substantially uniform composition. As mentioned above, after forming the deformable element 1610, the sensing element 1612 can be co-molded with the deformable element 1610 or the like can be applied (eg, adhered, coated, or deposited) to the protrusion 1611 or in the protrusion Part 1611. In either case, the sensing element 1612 can be at least partially embedded in the protrusion 1611. Other techniques for fastening the sensing element 1612 to the protrusion 1611 are also contemplated. It will be appreciated that the protrusions 1611 are for illustrative purposes and are not necessarily drawn to scale relative to the size of the substrate surface 1900 or any other component depicted in the drawings.

20 shows an example of a second sensing element 1614, or a portion thereof, the second sensing element 1614 includes a sensing region 1810 (indicated by a solid square) and a contact sensing region 1616 (indicated by a cross-hatched square) Both, and can be used in conjunction with the deformable element 1610 shown in FIG. Both the sensing region 1810 and the contact sensing region 1616 can be formed on the same substrate 2000 (eg, a flexible circuit material) and can include conductive traces such as metal, carbon, ITO, or the like.

In the example shown in FIGS. 19 and 20, each protrusion 1611 includes a sensing element 1612 and corresponds to one of the contact sensing regions 1616 on the second sensing element 1614. This may not be the case, however, because the considerations for determining the amount, configuration, and distribution of the protrusions 1611 that provide a suitable compression resistance are different from the considerations for pushing the amount, configuration, and distribution of the contact sensing regions. For example, in some embodiments, some of the protrusions 1611 do not correspond to the contact sensing area 1616. In such cases, the protrusions 1611 that do not correspond to the contact-sensing regions 1616 can omit the sensing elements 1612, but can be formed or shaped to ensure that all of the protrusions 1611 have substantially the same height. Alternatively, all of the protrusions 1611 can include a sensing element 1612, whether or not the protrusions correspond to a contact sensing area 1616. This ensures that all of the protrusions have the same height and substantially simultaneously contact an opposing surface.

21A is a cross-sectional view of an example contact sensor 2100 showing a section similar to that shown in FIGS. 18A-18B. Although the contact sensor formed by the protrusion 1611 and the contact sensing region 1616 shown in FIGS. 18A to 18B places the sensing component and the sensed component on opposite sides of the air gap 1615. However, the touch sensor 2100 is configured such that both the sense component and the sense component can be disposed on one side of an air gap.

The touch sensor 2100 includes a deformable protrusion 2102 that can be made of any suitable deformable material (such as polyfluorene oxide, polyurethane foam, rubber, gel, or the like). ) formed. A sensing element 2104 can be merged with the protrusion 2102. For example, the sensing element 2104 can be placed in one of the cavities 2106 or other interior regions of the protrusion 2102. Sensing element 2104 can also be embedded in the material of protrusion 2102 (eg, via co-molding or insert molding). As with sensing element 1612, sensing element 2104 can be formed of any suitable material or include any suitable material, such as a dielectric material and/or a conductive material.

Contact sensor 2100 also includes leads 2110 in an adjacent layer 2108. Adjacent layer 2108 can be a sensing element, such as sensing element 1614, in which lead 2110 is incorporated. Alternatively, adjacent layer 2108 can be dedicated to contain leads 2110. As with leads 1802, 1804, 1806, and 1808 in FIGS. 18A-18B, lead 2110 can be configured to function as a capacitive component (eg, capacitively coupled to sensing component 2104 and detecting proximity of sensing component 2104) Capacitance plate), contact for a continuous sensor, or the like. Additionally, the leads 2110 can be formed of any suitable material or include any suitable material, such as traces, wiring, plates, pads, or the like of conductive materials (eg, metal, carbon, ITO). Lead 2110 can be coupled to a suitable circuitry for detecting contact with sensing element 2104 or proximity to sensing element 2104.

In the case where the contact sensor 2100 is a capacitive sensor, physical contact between the lead 2110 and the sensing element 2104 may not be required to detect contact between the protrusion 2102 and another component. Rather, when the protrusion 2102 contacts another component (eg, because an adjacent air gap has completely collapsed), the lead 2110, along with associated circuitry, can detect the distance between the sensing element 2104 and the lead 2110. The change thereby triggers the touch sensor 2100. In such cases, the aperture 2106 can be filled with a deformable material, such as polyfluorene, thereby encapsulating the sensing element 2104.

21B illustrates the contact sensor 2100 after the protrusion 2102 has been deformed by a layer 2112, the layer 2112 forming an opposite side of one of the air gaps in which the protrusion 2102 has been disposed. As shown, the sensing element 2104 has been brought into contact with the lead 2110, thus triggering the touch sensor 2100. However, the sensing element 2104 need not actually contact the lead 2110 to trigger the touch sensor 2100. For example, in the case where the lead 2110 is configured as a capacitive sensor (or any other type of sensor capable of detecting a change in distance between the lead and another object), the layer 2112 can be utilized The touch sensor 2100 is triggered by any other detectable distance change between the sensing element 2104 and the lead 2110 caused by deformation or otherwise contacting the protrusion 2102.

22A is a cross-sectional view of an example contact sensor 2200 showing a section similar to that shown in FIGS. 18A-18B. Although the contact sensor formed by the protrusion 1611 and the contact sensing region 1616 shown in FIGS. 18A to 18B places the sensing component and the sensed component on opposite sides of the air gap 1615. However, the touch sensor 2200 is configured such that both the sense component and the sense component can be disposed on one side of an air gap.

The touch sensor 2200 includes a deformable protrusion 2202 that can be made of any suitable deformable material (such as polyfluorene oxide, polyurethane foam, rubber, gel, or the like). ) formed. A sensing element 2204 can be disposed over the protrusion 2202. For example, a material can be disposed over at least a portion of the protrusions 2202, such as by coating, deposition (eg, physical vapor deposition or chemical vapor deposition), or any other suitable mechanism. Contact sensor 2200 also includes leads 2208 that are proximate to protrusions 2202 in layer 2206.

Lead 2208 can be configured to act as a capacitive element capacitively coupled to sensing element 2204, thereby sensing a change in distance from lead 2208 to sensing element 2204. Accordingly, the sensing element 2204 can be formed of a conductive material, a dielectric material (eg, a high-k dielectric material), or any other suitable material that can be capacitively coupled to the lead 2208 and sensed by the lead 2208, or A conductive material, a dielectric material (eg, a high-k dielectric material), or any other suitable material that can be capacitively coupled to lead 2208 and sensed by lead 2208 is included.

FIG. 22B illustrates the contact sensor 2200 after the protrusion 2202 has been deformed by a layer 2210 formed on the opposite side of one of the air gaps in which the protrusion 2202 is disposed. As shown, the sensing element 2204 has been brought closer to the lead 2208, thus triggering the touch sensor 2200.

Contact sensors 2100, 2200 can be used instead of or in conjunction with the touch sensors described with respect to Figures 18A-20. For example, the deformable element 1610 can include a plurality of contact sensors 2100 or 2200 that provide the same or similar functions, rather than forming a contact sensor together to detect the protrusion 1611 of the contact and deformable element 1610. And sensing area 1616.

The contact sensing system described herein can be applied between any of the layers or components of a force sensing device. For example, while FIG. 16 depicts a touch sensor to detect when the air gap 1615 has collapsed, a touch sensor can alternatively or alternatively be configured to detect when the air gap 1606 has collapsed. In some cases, a plurality of air gaps in a stack of force sensing devices can include a contact sensor. By providing an additional contact sensor in this manner, an electronic device can determine which layers have been deflected or are deflecting, and thus can apply a force deflection correlation that is adapted to deflect one or more particular layers. By providing a different force deflection correlation for each of the multiple layers, one of the forces applied to one surface can be determined with high precision.

When the deformable elements described in each of the foregoing examples are in an undeformed state, the deformable elements can have different thicknesses and/or different protrusion heights in different zones. For example, the base structure of the force sensing device and/or the upper stack or the lower stack (or any other layer of any force sensing device) may not have a uniform flat surface. Accordingly, in order to provide a relatively constant air gap size across one of the air gaps, the deformable elements can have different thicknesses in different zones. For example, the protrusions may be larger in some regions to account for a greater distance between one layer or stack (eg, lower stack 308) and a substrate structure (eg, base structure or layer 316).

In some cases, the input surface may not be evenly deflected across the entire input surface area. For example, one of the forces applied near one edge of the cover 303 (eg, near the junction between the housing 104 and the cover 303) can cause the cover 303 (and thus the upper stack 304 and the lower stack) The deflection of 308) is less than the deflection caused by one of the same magnitudes applied to the central cover member 303. Accordingly, the deformable element can be thicker in areas where less deformation is desired (eg, around the edge or perimeter of the cover 303) such that the deformable element begins to compress with substantially the same magnitude of force, regardless of the input surface. Where the force is applied.

23A is a cross-sectional view of one embodiment of the device 100 of FIG. 1 taken along line AA of FIG. 1, showing an assembly 2300 that provides display, touch sensing, and force/or sensing. Functionality to device 100, or may be integrated with other components to provide such functionality. As shown in FIG. 23A, device 100 includes a force sensing system (similar to the sensor described above with respect to FIGS. 5-22) in assembly 2300, and is positioned between housing 104 and cover member 303. One of the sensors 2302 (Fig. 23B). The sensor 2302 operates in conjunction with the sensing element in the assembly 2300 to determine the amount of deflection of one of the covers 303, and thus the force applied to the cover 303.

Assembly 2300 includes upper stack 304 and lower stack 308, air gaps 306, 310, and deformable elements 314, all of which are described above with respect to Figures 3A-3E. The assembly 2300 also includes a first sensing element 2304 positioned on a first side (eg, above) of one of the deformable elements 314 and positioned on a second side of one of the deformable elements 314 (eg, below) One of the second sensing elements 2306. The first sensing element 2304 and the second sensing element 2306 can be collectively referred to as a force sensor.

The first sensing element 2304 and the second sensing element 2306 can be similar to any of the sensing elements described herein. For example, the first sensing component 2304 can be a capacitive driving layer, and the second sensing component 2306 can be capacitively coupled to one of the driving layers. The first sensing element 2304 and the second sensing element 2306 and associated circuitry can detect a deformation or deflection of the deformable element 314 and thus determine a force applied to the cover member 303. While the assembly 2300 shows that the first sensing element 2304 and the second sensing element 2306 are positioned on opposite sides of the deformable element 314, other configurations are possible. For example, the first sensing element 2304 can be disposed on the bottom of the frame member 309, on the upper stack (or in), or the like. In some cases, any of the force sensing devices described herein can be used in assembly 2300, such as shown and described with respect to FIG. 5, FIG. 12, FIG. 14, or FIG.

In addition to the force sensor included in the assembly 2300, the device 100 can also include a sensor 2302 disposed between the housing 104 and the cover member 303. The sensor 2302 can include a flexible material that can deflect or deform in response to a force applied by one of the covers 303. The sensor 2302, along with the associated sensing circuitry, can detect the amount of deflection of the cover member 303 in response to an applied force, and the sensing elements 2304, 2306 incorporated in the assembly 2300 determine the application to the cover. One of the strengths of piece 303.

Figure 23B shows an expanded view of area 2308 in Figure 23A, showing details of sensor 2302. The sensor 2302 can be positioned between the lug 307 of the housing 104 and a portion of the cover member 303 such that when a force is applied to the cover member 303, the sensor 2302 is pressed against the lug 307 and the cover member 303. Between the parts, the sensor 2302 is thus deformed. The geometry of lug 307 and cover member 303 in Figure 23B is merely exemplary, and different embodiments of housing 104 and cover member 303 can have different shapes, geometries, and/or variations than those shown in Figure 23B. feature.

The sensor 2302 includes a deformable portion 2310. The deformable portion 2310 can be formed from any suitable material or include any suitable material, such as polyfluorene oxide, polyurethane foam, rubber, gel, elastomer, or the like. In some cases, the deformable portion 2310 can have adhesive properties such that the sensor 2302 holds the cover 303 to the housing 104.

The sensor 2302 also includes a first sensing component 2312 and a second sensing component 2314. The first sensing element 2312 and the second sensing element 2314 can be positioned on opposite sides (eg, a top and bottom, as shown in FIG. 23B) of the deformable portion 2310. The first sensing component 2312 and the second sensing component 2314 can form a capacitive sensor. In this case, one of the first sensing component 2312 and the second sensing component 2314 can be a capacitive driving layer. And the other can be a capacitive sensing layer. The capacitive sensor detects a amount of deformation of the deformable portion 2310 and thus facilitates detecting an applied force, as discussed herein. In some cases, the sensor 2302 can be a resistive sensor (or any other suitable sensor), in which case the first sensing element 2312 and the second sensing element 2314 can be omitted, or Other components replace the first sensing element 2312 and the second sensing element 2314.

When a force is applied to the cover member 303, the deformable portion 2310 of the sensor 2302 can be deflected or deformed such that the first sensing element 2312 and the second sensing element 2314 are closer together. The first sensing element 2312 and the second sensing element 2314 and associated circuitry can determine the amount of deformation and correlate the amount of deformation with a force applied to the cover member 303. However, as a certain amount of force is applied, the deformable portion 2310 can reach a maximum deformation, wherein a larger applied force may not cause further deformation of the deformable portion 2310. However, in some cases, it is desirable to detect that the applied force is greater than this amount. Accordingly, the sensor 2302 and the sensing elements in the assembly 2300 can sense different ranges of applied forces.

For example, the sensor 2302 can be configured to determine a force that spans from one of the unapplied forces to one of the forces that cause the air gaps 306 and 310 in FIG. 23A to collapse. Up to this point, the sensors in the assembly 2300 (formed by the first sensing element 2304 and the second sensing element 2306) may not detect any force, since the lower stack 308 and the deformable element 314 have not been made yet. contact. Once the lower stack 308 contacts the deformable element 314, the increased force can be determined by the sensing elements 2304, 2306 in the assembly 2300.

The first sensing element 2312 and the second sensing element 2314 can be formed of any suitable material or include any suitable material, such as metal, ITO, or the like. Additionally, the first sensing element 2312 and the second sensing element 2314 can be applied to the deformable portion 2310 or otherwise combined with the deformable portion 2310 in any suitable manner. For example, the first sensing element 2312 and the second sensing element 2314 can be or can be embedded in the deformable portion 2310, positioned on the deformable portion 2310, or otherwise integrated with the deformable portion 2310 Conductive sheet (for example, copper, silver, or gold). As another example, the first sensing element 2312 and the second sensing element 2314 can be ITO deposited on the deformable portion 2310.

In some cases, either or both of the first sensing element 2312 and the second sensing element 2314 may not be integrated with the deformable material 2310, but may be separate components. For example, the first sensing element 2312 and/or the second sensing element 2314 can be a layer of a material (eg, a flexible circuit material) that is provided with a conductive material disposed thereon. The layers can be positioned between the deformable portion 2310 and the cover 303 and/or between the deformable portion 2310 and the housing 104 and can be joined or otherwise adhered to their components. As another example, the first sensing element 2312 and/or the second sensing element 2314 can be directly patterned on the cover member 303 and/or the housing 104. For example, when the device 100 is in its assembled configuration, ITO, conductive nanowires, or any other suitable material may be formed directly on the opposing portions of the cover member 303 and the housing 104. Any combination of the foregoing examples can be used to integrate first sensing element 2312 and/or second sensing element 2314 with device 100.

Figure 24 is an example force versus deflection curve showing how the cover member 303 of the device illustrated in Figure 23A deflects in response to a force input applied thereto. The force response is similar to that shown in Figure 4, wherein a first quantity curve is from point 401 to point 402 (corresponding to the collapse of air gaps 306 and 310) and a second quantity curve is from point 402 to point. 404 (corresponding to the deformation of the deformable element 314). The sensor 2302 can detect the deformation of the air gaps 306, 310 as indicated by line 2402 in FIG. 24, and the force sensor in the assembly 2300 detects the deformation of the deformable element 314, such as by the line. Indicated by 2404. Although lines 2402, 2404 are shown as non-overlapping, this may not be the case. For example, even after the air gaps 306, 310 have collapsed, the sensor 2302 can continue to deflect and thus provide meaningful force information. In such cases, the sensing circuitry associated with the sensor can process information from both of the sensors to determine an applied force.

Figure 25 shows a portion of sensor 2302 as viewed by cover member 303 of the transmissive device. The depicted portion of sensor 2302 corresponds to one of the corner portions of sensor 2302. The sensor 2302 includes a first drive region 2502 that is electrically coupled together (eg, via conductors 2503) and a second drive region 2504 that is electrically coupled together (eg, via conductor 2505). The first drive region 2502 and the second drive region 2504 can be formed together in the second sensing element 2314 shown in Figure 23B and can be driven or energized with a signal. As shown, the first drive region 2502 and the second drive region 2504 are shown in an alternating, interdigitated pattern, however this is only for one instance configuration of the first drive region 2502 and the second drive region 2504.

The sensor 2302 also includes a sensing region 2506. Sensing region 2506 is capacitively coupled to drive regions 2502, 2504 and can be coupled to circuitry that detects and analyzes signals induced by drive regions 2502, 2504 in sense region 2506. Each of the sensing regions 2506 can overlap with a first driving region 2502 and a second driving region 2504. Since the driving regions can be driven at different times and/or with different signals (eg, signals having different frequencies), a single sensing region can provide two different capacitive measurements, each capacitive measurement corresponding to the sense of the sensation One of the detectors 2302 is in a different position. In this manner, the sensor 2302 is pixelated, allowing for more precise force measurements and for detecting one of the forces exerted by one of the covers 303.

26 is a cross-sectional view of an embodiment of the apparatus 100 taken along line A-A of FIG. 1, showing a display stack 2600 positioned below the cover member 110. The force and/or touch sensing system or components thereof can be combined with the display stack 2600 to facilitate touch and force input detection on the device 100. As described herein, device 100 can include a conductive sheet (such as first drive layer 505, FIG. 5) that can facilitate sensing force and/or touch input on device 100.

Display stack 2600 can include a touch sensor 2602 positioned between cover member 110 and a display layer 2604. The touch sensor 2602 can include a sensor, each sensor configured to detect user input (eg, touch and/or force input) on the cover member 110 and the location of the user input . Any suitable touch sensor 2602 can be used. For example, in one embodiment, the touch sensor 2602 is formed with a dielectric substrate positioned between two electrode layers. The electrode layers can be made of any suitable optically transparent material. For example, in one embodiment, the electrode layers are made of indium tin oxide (ITO). Other suitable materials include, but are not limited to, a nanowire or nanowire grid, a transparent conductive film (eg, a polymeric film), a carbon nanotube, and an ultra-thin metal film.

Each of the electrode layers in the touch sensor 2602 can include one or more electrodes. The (equal) electrode in one layer is aligned with at least one direction (eg, vertical) of the respective electrodes in the other electrode layers to form one or more capacitive sensors. The user input and the location of the user input are detected by a change in capacitance of one or more capacitive sensors. As will be described in more detail below, touch and sense circuitry 2632 is coupled to the electrode layers and configured to receive an output signal from each of the capacitive sensors, the output signals representing the capacitance of each capacitive sensor.

One or both of the electrode layers in touch sensor 2602 can be patterned. For example, in one embodiment, one electrode layer is patterned into strips that are positioned along a first axis (eg, columns), and other electrode layers are patterned to be positioned along a second axis (eg, rows) a strip, the second axis being transverse to the first axis. A capacitive sensor is formed at the intersection of the strips in the two electrode layers. The user input, and the location of the user input, can be determined based on the capacitance (or capacitance change) of one or more capacitive sensors.

Display layer 2604 can include a front polarizer 2606; a display element 2608 attached to a rear surface of one of the front polarizers 2606; and a rear polarizer 2610 attached to a rear surface of one of the display elements 2608. Any suitable display element 2608 can be used. Example display component 2608 includes, but is not limited to, an LCD component, an LED component, an OLED component, or an OEL component. In the illustrated embodiment, display element 2608 is an LCD element.

In some cases, the noise signal generated by display element 2608 can be electrically coupled to touch sensor 2602. This coupling can adversely affect the detection of user input by touch sensor 2602. To reduce or eliminate display noise from coupling with touch sensor 2602, a conductive layer 2612 can be positioned between touch sensor 2602 and front polarizer 2606. Conductive layer 2612 can be made of any suitable optically transparent material. For example, in one embodiment, the conductive layer 2612 is made of ITO.

A sheet of conductive material 2614 is formed or coated on the surface behind the rear polarizer 2610. The sheet of conductive material 2614 can be made of any suitable conductive material. For example, in one embodiment, the sheet of conductive material 2614 is made from a silver nanowire film.

The rear polarizer 2610 can be made of an electrically insulating material. The sheet of conductive material 2614 enables the surface behind the rear polarizer 2610 to function as a conductive surface. As will be described in more detail below, the conductive surface of the rear polarizer 2610 is used to transmit a drive signal for a force sensor that includes one of the conductive surfaces.

A conductive bezel 2616 is attached to the rear surface of the rear polarizer 2610 (the structure, material, function, etc. of the conductive bezel 2616 can be the same or similar to the connecting element 706, Figures 7, 10A). The conductive bezel 2616 is positioned along at least a portion of a perimeter or edge of the rear polarizer 2610. As will be described in greater detail in connection with Figures 27-29, conductive bezel 2616 can extend around one continuous frame of the entire perimeter, or conductive bezel 2616 can include one or more discrete conductive strips, with each conductive strip positioned to be rearwardly polarized Each of the peripheral portions of the device 2610.

In the illustrated embodiment, display stack 2600 extends across user viewable area 108 (FIG. 1) of display 102 and to non-viewable area 2618 (which does not correspond to one viewable output from display 102). Alternatively, in some embodiments, only a subset of the layers in display stack 2600 extend into non-viewable area 2618. For example, portions of display layer 2604 can extend into non-viewable area 2618, while other layers in display stack 2600 do not extend into non-viewable area 2618.

In some embodiments, the conductive bezel 2616 can be positioned on a portion of the rear polarizer 2610 that resides in the non-viewable region 2618, which allows for any suitable material or materials (eg, opaque or transparent) Material) forms a conductive bezel 2616. For example, a conductive bezel 2616 can be formed from a metal or metal alloy such as copper, aluminum, molybdenum, and nickel vanadium. Other embodiments may form at least a portion of the conductive bezel 2616 within the user viewable area 108. In such embodiments, at least portions of the conductive bezel 2616 in the user viewable area 108 may be formed from an optically transparent material such as ITO.

In the illustrated embodiment, a backlight unit 2620 is positioned below the rear polarizer 2610 and the conductive bezel 2616. Display layer 2604, along with backlight unit 2620, is used to output an image on display 102. In some implementations, backlight unit 2620 can be omitted.

A first electrode layer 2622 is positioned below the backlight unit 2620 and attached to the backlight unit 2620. In some embodiments, the first electrode layer 2622 represents an array of electrodes (eg, two or more electrodes). In other embodiments, the first electrode layer 2622 is a single electrode. The first electrode layer 2622 can be formed from any suitable (opaque or transparent) conductive material such as a metal or metal alloy. Example metals and metal alloys include, but are not limited to, copper, aluminum, titanium, niobium, nickel, chromium, zirconium, molybdenum niobium, and nickel vanadium.

The conductive material sheet 2614 and the first electrode layer 2622 on the surface after the rear polarizer 2610 together form a force sensor. The force sensor can be used to detect a force value or a force applied to the cover member 110. When the first electrode layer 2622 is implemented as an electrode array, the conductive material sheet 2614 and the first electrode layer 2622 form a capacitive sensor array. Each of the capacitive sensors includes an electrode formed of a sheet 26 of conductive material and a respective electrode in the first electrode layer 2622. When a user input is applied to the cover member 110, the cover member 110 deflects and changes a distance between the electrodes in at least one of the capacitive sensors, which changes the capacitance of the capacitive sensor. For example, in the illustrated embodiment, the gap 2623 is changed based on a user input applied to the cover member 110, which in turn changes the capacitance of at least one capacitive sensor.

In some embodiments, the first electrode layer 2622 can be used to detect one or more touches on the cover member 110. In such an embodiment, the touch sensing layer 2602 can be omitted because the first electrode layer 2622 has dual functions for detecting both touch input and force input.

The device 100 can also include a support structure 2624 (the structure, materials, functions, etc. can be the same or similar to the frame members 309, 1207 discussed above). In the illustrated embodiment, the support structure 2624 is made of a conductive material (e.g., a metal), but other embodiments may form the support structure 2624 from a different material, such as plastic, ceramic, or a composite. In the illustrated embodiment, the support structure 2624 extends along one of the lengths and a width of the display stack 2600, but this is not necessary. In other embodiments, the support structure 2624 can have any shape and/or size. For example, the support structure 2624 can have an opening in which a stiffening member can be positioned (as described with respect to the frame member 309 and the stiffening member 312 of FIG. 3A).

In the illustrated embodiment, the support structure 2624 has a U-shaped cross section and is attached to the cover member 110 such that the support structure 2624 is suspended from the cover member 110. In other embodiments, the support structure 2624 can be coupled to one of the components other than the cover member 110. For example, the support structure 2624 can be attached to one of the devices 100 (eg, the housing 104 in FIG. 1) or attached to one of the frames or other support components in the housing.

In some embodiments, the support structure 2624 can be constructed and attached to the cover member 110 to define a gap 2626 between the support structure 2624 and the first electrode layer 2622. The gap 2626 allows the display stack 2600 to flex or move in response to a force applied by one of the covers 110. In some embodiments, the first electrode layer 2622 can be attached to the support structure 2624 instead of the backlight unit 2620.

Device 100 can also include a battery pack 2628. Battery pack 2628 provides power to various components of device 100. As shown in FIG. 26, a second electrode layer 2630 can be disposed on a top surface of one of the battery packs 2628. In some embodiments, the force applied to the cover member 110 may be sufficient to cause the display stack 2600 to deflect such that the rear polarizer 2610 contacts the first electrode layer 2622. When the display stack 2600 is deflected to a point where the rear polarizer 2610 contacts the backlight unit 2620 (or contacts the first electrode layer 2622 if the backlight unit 2620 does not exist), the force detected by the force sensor reaches a maximum Level (for example, a first power). The force sensor cannot detect the force exceeding the maximum level. The display stack 2600 is deflected to a point in which the rear polarizer 2610 contacts the backlight unit 2620 or the first electrode layer 2622, which may correspond to the first amount curve 406 of the force in FIG. 4 relative to the deflection curve. For example, the maximum level of force detected by the force sensor including the first electrode layer 2622 and the conductive material 2614 may correspond to point 402 in FIG.

In such an embodiment, the second electrode layer 2630 (in combination with the first electrode layer 2622 or other components) can form a second force sensor by being interposed between the first electrode layer 2622 A force exceeding the first force is detected in association with a deflection amount (eg, a second force) between the second electrode layer 2630. For example, in some embodiments, the second electrode layer 2630 can be used to measure a change in capacitance between the first electrode layer 2622 and the second electrode layer 2630. Alternatively, the second electrode layer 2630 can be used to detect a change in capacitance between the surface 2627 and the second electrode layer 2630 between the support structure 2624. This deflection between the first electrode layer 2622 and the second electrode layer 2630 (or between the support structure rear surface 2627 and the second electrode layer 2630) may correspond to the second amount curve 408 in FIG.

Drive and sense circuitry 2632 is coupled to touch sensor 2602 as previously described. Drive and sense circuitry 2632 can be positioned at any suitable location in device 100. The drive and sense circuitry 2632 is configured to provide a drive signal to the touch sensor 2602 and to receive an output signal from the touch sensor 2602. For example, when the touch sensor 2602 includes a capacitive sensor array, the drive and sense circuitry 2632 is coupled to each of the capacitive sensors and configured to sense or measure the capacitance of each capacitive sensor. . A processing device can be coupled to the drive and sense circuitry 2632 and configured to receive signals indicative of the measured capacitance of each of the capacitive sensors. The processing device can be configured to correlate the measured capacitances with a force.

Similarly, drive circuitry 2634 is coupled to conductive material sheet 2614 and is configured to provide a drive signal to the rear surface of rear polarizer 2610 (eg, to provide a drive signal to conductive material sheet 2614). In some embodiments, drive circuitry 2634 is coupled to conductive bezel 2616.

Sensing circuitry 2636 is coupled to first electrode layer 2622 and is configured to receive one or more output signals from first electrode layer 2622. For example, when the first force sensor includes a capacitive sensor array, drive and sense circuitry 2634, 2636 are coupled to each of the capacitive sensors and configured to sense or measure each capacitive sensing Capacitor. A processing device can be coupled to the drive and sense circuitry 2634, 2636 and configured to receive an output signal representative of the measured capacitance of each capacitive sensor. The processing device can be configured to correlate the measured capacitances with a force. As with the drive and sense circuitry 2632, the drive circuitry 2634 and the sense circuitry 2636 can be located at any suitable location in the device 100.

The drive signal transmitted on the surface after the rear polarizer 2610 (e.g., on the conductive material sheet 2614) can be decoupled from the noise generated by the display element 2608 (e.g., a TFT layer) because of the insulation The rear polarizer 2610 physically separates the sheet of conductive material 2614 from the display element 2608. In addition, the conductive bezel 2616 can reduce the contact resistance between the rear polarizer 2610 and the conductive material sheet 2614, as well as reduce the sheet resistance of the conductive material sheet 2614. Reducing the contact resistance and/or the sheet resistance increases the suppression of display noise generated by display element 2608.

Regarding the second electrode layer 2630, the drive circuitry 2638 is coupled to the second electrode layer 2630 and is configured to provide a drive signal to the second electrode layer 2630. Drive circuitry 2638 can be located at any suitable location in device 100. In some embodiments, sensing circuitry 2636 can be configured to receive one or more output signals from first electrode layer 2622. A processing device coupled to the sensing circuitry 2636 can be configured to receive the output signals and correlate the measured capacitances with a force.

27 through 29 depict an example configuration of a conductive bezel on the polarizer 2610 shown in FIG. As shown in FIG. 27, the conductive bezel can include four discrete conductive strips 2702, 2704, 2706, 2708 formed on one of the sheets of conductive material 2710 coated on a polarizer 2700. Each of the conductive strips 2702, 2704, 2706, 2708 is formed along a respective edge of one of the polarizers 2700. Although FIG. 27 depicts four conductive strips, other embodiments are not limited to this configuration. Other embodiments may include one or more conductive strips. The embodiment shown in Figures 27-29 can represent an embodiment of conductive material 2614 and conductive bezel 2616 on polarizer 2610 in Figure 26.

In some embodiments, the sheet of conductive material 2710 can be formed from an anisotropic material that conducts more in one direction than the other. In such embodiments, the discrete conductive strips or strips 2702, 2704, 2706, 2708 can more effectively reduce the sheet resistance and/or contact resistance of the sheet of conductive material 2710.

28 depicts a discrete L-shaped conductive strip 2802 positioned on a sheet of conductive material 2804 on a polarizer 2800. In the illustrated embodiment, conductive strips 2802 are formed along both edges of polarizer 2800. Other embodiments may include two "L" shaped conductive strips configured to position a conductive strip along each edge of polarizer 2800.

FIG. 29 illustrates a continuous conductive bezel 2902 positioned along the entire edge of the polarizer 2900. In some cases, the continuous conductive bezel 2902 can reduce the sheet conductivity and/or contact resistivity of the sheet of conductive material 2904 more efficiently than one or more of the conductive strips. Conductive strips 2702, 2704, 2706, 2708 and/or conductive bezels 2802, 2902 can form the connecting elements 706 described above with respect to Figures 7 and 10A.

While the embodiments shown in Figures 26-29 are described in connection with one display stack in an electronic device, other embodiments are not limited to displays. A force sensor can be formed under any suitable cover member, such as a housing of an electronic device (e.g., housing 104 in Figure 1, track plate 206 in Figure 2). An insulating substrate can be positioned below the cover member. A sheet of conductive material is formed over a rear surface of one of the insulating substrates to create a conductive surface on the rear surface of the insulating substrate. In other words, the sheet of conductive material converts the back surface of the insulating substrate into a conductive surface. A conductive bezel is formed along at least one edge of the sheet of conductive material, and an electrode layer is positioned below the insulating substrate. The electrically conductive surface of the insulative substrate and the electrode layer together form a force sensor configured to detect a force input on the cover layer.

Throughout the foregoing, the force sensing device and the contact sensor are described with respect to various examples. However, these examples are not intended to limit the particular elements, layers, or components described. For example, components described herein as separate and/or dissimilar components (eg, layers of force sensing devices) can be combined, and components described herein as being combined or integrated can be separated. In addition, some components may be substituted, added or removed without departing from the scope of the disclosure. For example, as mentioned above, if a force sensing device is not integrated with a display device or is not a component of a display device, a display structure can be omitted from the force sensing device. Additionally, any individual layer or structure described herein can include one or more sub-layers. For example, a cover member can include a plurality of sub-layers including glass, coatings, adhesives, filters, and the like. By way of another example, any layer or component of the force sensing device and contact sensor described herein can be secured to an adjacent layer or structure with an adhesive, tie layer, or the like, however such adhesion The agent and tie layer are not necessarily those described herein.

FIG. 30 depicts example components of an electronic device in accordance with an embodiment described herein. The schematic depicted in FIG. 30 may correspond to the components of the device depicted in FIGS. 1-2, and in fact corresponds to any device in which the force sensing described herein may be incorporated.

As shown in FIG. 30, a device 3000 includes a processing unit 3002 operatively coupled to computer memory 3004 and/or computer readable medium 3006. The processing unit 3002 can be operatively coupled to the memory 3004 and the computer readable medium 3006 component via an electronic bus or bridge. Processing unit 3002 can include one or more computer processors or microcontrollers configured to perform operations in response to computer readable instructions. Processing unit 3002 can include a central processing unit (CPU) of the device. Additionally or alternatively, processing unit 3002 can include other processors within the device, including special application integrated circuits (ASICs) and other microcontroller devices.

The memory 3004 can include a wide variety of non-transitory computer readable storage media including, by way of example, random access memory (RAM), read only memory (ROM), erasable programmable memory. (for example, EPROM and EEPROM), or flash memory. Memory 3004 is configured to store computer readable instructions, sensor values, and other resiliency software components. The computer readable medium 3006 also includes a wide variety of non-transitory computer readable storage media including, for example, a hard disk storage device, a solid state storage device, a portable magnetic storage device, or the like. Device. Computer readable medium 3006 can also be configured to store computer readable commands, sensor values, force deflection correlations, and other resiliency software components.

In this example, processing unit 3002 is operative to read computer readable instructions stored on memory 3004 and/or computer readable medium 3006. The computer readable instruction adaptable processing unit 3002 performs the operations or functions described above with respect to FIGS. 1 through 25 or the example programs described below with respect to FIG. In particular, processing unit 3002, memory 3004, and/or computer readable medium 3006 can be configured to cooperate with force sensor 3022, described below, based on whether one of the user input surfaces is deflecting The air gap is collapsed in a force sensor or a deformable element is compressed, and a force applied to the user input surface is determined by applying different force deflection correlations. The computer readable instructions can be provided as a computer program product, a software application, or the like.

As shown in FIG. 30, device 3000 also includes a display 3008. Display 3008 can include a liquid crystal display (LCD), an organic light emitting diode (OLED) display, an LED display, or the like. If display 3008 is an LCD, display 3008 can also include a backlight assembly that can be controlled to provide a variable level of display brightness. If display 3008 is an OLED or LED type display, the brightness of display 3008 can be controlled by modifying the electrical signals provided to the display elements. Display 3008 can correspond to the upper and lower stacks described above.

Device 3000 may also include a battery pack 3009 configured to provide power to components of device 3000. Battery pack 3009 can include one or more storage batteries that are coupled together to provide an internal power supply. Battery pack 3009 is operatively coupled to a power management circuitry that is configured to provide suitable voltage and power levels for individual components or groups of components within device 3000. Battery pack 3009 can be configured via power management circuitry to receive power from an external source, such as an AC power outlet. The battery pack 3009 can store the received power such that the device 3000 can operate for an extended period of time, not counting the range of fractions to days, when not connected to an external power source.

In some embodiments, device 3000 includes one or more input devices 3010. Input device 3010 is configured to receive a device input by a user. Input device 3010 can include, for example, a button, a touch activation button, a keyboard, a keypad, or the like. In some embodiments, input device 3010 can provide a dedicated or primary function including, for example, a power button, a volume button, a home button, a scroll wheel, and a camera button. In general, a touch sensor (eg, a touch screen) or a force sensor can also be classified as an input device. However, for this illustrative example use, touch sensor 3020 and force sensor 3022 are depicted as distinct components within device 3000.

Device 3000 can also include a touch sensor 3020 (eg, touch sensor 2602, FIG. 26) configured to determine a position of a touch on one of the touch-sensitive surfaces of device 3000. Touch sensor 3020 can include an array of capacitive electrodes or nodes that operate in accordance with a mutual capacitance or self capacitance scheme. As described herein, the touch sensor 3020 can be integrated with one or a plurality of layers of a display stack or a force sensing device to provide touch sensing functionality of a touch screen. The capacitive arrays of touch sensors 3020 can be integrated with the force sensing devices described above and can provide force sensing functionality in addition to capacitive sensing elements.

Device 3000 can also include a force sensor 3022 configured to receive and/or detect a force input applied to a user input surface of device 3000. The force sensor 3022 can correspond to any of the force sensing devices or force sensors described herein, and can include or be coupled to a capacitive sensing component that facilitates detecting the force sensor The relative positional change of the components (e.g., the deflection caused by a force input).

As described herein, the force sensor 3022 can include a touch sensor that is configured to signal when an air gap has completely collapsed by a force input. A force sensor 3022 (including the contact sensors) is operatively coupled to the processing unit 3002, which can process signals from the force sensor 3022 to determine one of the user input surfaces Apply force as described above.

Device 3000 can also include one or more sensors 3024 that can be used to detect one of the environmental conditions, orientations, locations, or some other aspect of device 3000. Example sensors 3024 that may be included in device 3000 include, but are not limited to, one or more accelerometers, gyroscopes, inclinometers, goniometers, or magnetometers. The sensor 3024 can also include one or more proximity sensors, such as a magnetic Hall effect sensor, an inductive sensor, a capacitive sensor, a continuous sensor, and the like.

The sensor 3024 can also be generally defined to include wireless positioning devices including, but not limited to, global positioning system (GP) circuitry, Wi-Fi circuitry, cellular communication circuitry, and the like. Device 3000 can also include one or more optical sensors including, but not limited to, photodetectors, light sensors, image sensors, infrared sensors, and the like. Although the camera 3026 is depicted in FIG. 30 as a separate component, the generally defined sensor 3024 can also include a camera 3026 with or without an accompanying light source or flash. The sensor 3024 can also include one or more acoustic elements, such as one of the microphones used alone or in combination with a single speaker element. The sensors may also include a temperature sensor, a barometer, a pressure sensor, an altimeter, a humidity sensor, or other similar environmental sensor.

Device 3000 can also include a camera 3026 configured to capture a digital image or other optical material. Camera 3026 can include a charge coupled device, a complementary metal oxide semiconductor (CMOS) device, or other device configured to convert light into an electrical signal. Camera 3026 can also include one or more light sources, such as a strobe light, flash, or other illumination device. As discussed above, camera 3026 can be broadly classified as a sensor for detecting optical conditions and/or objects in the vicinity of device 3000. However, camera 3026 can also be used to create realistic images that can be stored in an electronic format, such as JPG, GIF, TIFF, PNG, pure image archives, or other similar file types.

Apparatus 3000 can also include a communication port 3028 configured to transmit and/or receive signals or electrical communications from an external or separate device. Communication port 3028 can be configured to couple to an external device via a cable, adapter, or other type of electrical connector. In some embodiments, the communication port 3028 can be used to couple the device 3000 to an accessory, such as a smart case, a smart cover, a smart stand, a keyboard, or configured to transmit And/or other devices that receive electrical signals.

Device 3000 can use any suitable technique or algorithm to determine the force applied to a user input surface. For example, device 3000 can use data, readings, or other information from the force sensing device, and then apply a mathematical formula or consulting model or lookup table to determine a based on the information from the force sensing device. Apply strength. More specifically, an example technique for determining a force applied to a structure including a force sensing device includes consulting to cause a sensor value (eg, a detected capacitance value) to interact with a particular known force A related lookup table or other data structure. The lookup table can be populated by a calibration procedure whereby a known force is applied to various locations on the user input surface. For each location, the resulting sensor values (which may be referred to as calibration values) for each pixel or sensing region of the sensor are stored in the lookup table (or other data structure). Accordingly, there is a set of calibration values for each user input location in the lookup table, the calibration values representing the sensor values of all pixels or sensing regions of the sensor when the sensor is subjected to a known force. . In some cases, there are multiple sets of calibration values for each location, such as values associated with forces of different known magnitudes.

To determine a force applied to the user input surface during normal operation, (eg, with touch sensor 3020) determine one of the touch events on the input surface and use the calibration value for the position The actual applied force is determined in conjunction with the detected sensor value. For example, if the detected sensor value corresponding to one of the touch events at a given location is approximately three times the calibration value associated with one of the touch events at that location, then Device 3000 can determine that the applied force is approximately three times greater than the calibration force.

Another technique for determining an applied force includes determining a force applied to each pixel or sensing region of a sensor, and then applying a sum of the forces from each pixel or sensing region to the determination The total strength of the sensor. In the case of using this technique, a change in distance between two sensing elements can be used in combination with one of the materials of one of the two sensing elements, to determine the force applied to the pixel or region. . For a particular example, a deformable element (eg, deformable element 514, Figure 5) can be positioned between the capacitive sensing elements. The capacitive sensing elements can correspond to the second sensing element 512 and the third sensing element 515, which are respectively the capacitive sensing layer and the driving layer in FIG. The capacitive sensing elements may also correspond to the first electrode layer 2622 and the conductive material 2614 in FIG. By measuring the capacitance of one of the capacitive sensing elements, device 3000 can determine a distance (or a change in distance) between the sensing elements caused by a force applied to the deformable element. The change in distance can be multiplied by a stiffness of the deformable element (e.g., a constant that causes one of the materials to be deflected or deformed to correlate with a given force) to determine the force corresponding to the detected distance change. As mentioned above, the second sensing element 512 and the third sensing element 515 can define a number of different pixels or sensing regions (eg, region 702, Figure 7). Accordingly, the foregoing techniques can be used to determine the force applied to individual pixels or sensing regions, and can combine (eg, add) the forces to determine the total applied to the user input surface and/or the sensor. power.

In some cases, the stiffness of the deformable element (eg, a stiffness constant) can be determined for each sensing region. Thus, the distance measurement for each region can be multiplied by a specific stiffness constant for that region, which can improve the accuracy of force measurements for each pixel or region, and thus can improve the overall accuracy of the force sensor. The stiffness constant for each pixel or sensing region can be manually determined, for example, by applying a known force to each region of the deformable element (corresponding to a pixel or sensing region), and measuring the deformable The amount or distance that the component has been deflected. In some cases, multiple measurements may be made according to different forces to determine an average stiffness constant or a constant metric curve for the one of the deformable materials. This can increase the accuracy of a sensor as compared to using the same stiffness constant for each sensing region, since the stiffness varies with the region.

Any of the foregoing techniques (eg, consulting a lookup table or calculating a force based on a stiffness constant) can be used to determine the force applied to a given sensor or sensing device described herein. In embodiments where one device includes multiple sensors, a different technique can be used for each sensor. For example, for force sensing device 500 (which includes first capacitive sensor 518 and second capacitive sensor 519 (FIG. 5)), a look-up table can be used to determine the application to first capacitive sensor 518. The force, and a stiffness-based force calculation can be used to determine the force applied to the second capacitive sensor 519. As another example, the device of Figures 23A-23B includes a sensor 2302 positioned between a housing and a cover, and a sensor within the housing (eg, the housing includes First sensing element 2304 and second sensing element 2306, together with one deformable element 314) between first sensing element 2304 and second sensing element 2306. In this case, a lookup table can be used to determine the force applied to the sensor 2303, and a stiffness based calculation can be used to determine the sensor applied to the housing (eg, the first sensing element) The force of 2304 and second sensing element 2306). Alternatively, a look-up table technique can be used for both sensors.

Where two or more sensors are used, the force values determined for each sensor can be combined to produce a single value representative of the force applied to the user input surface. For example, referring to the force sensing device 500 (FIG. 5), the first capacitive sensor 518 and the second capacitive sensor 519 can be deflected in response to different applied forces. More specifically, the air gaps 506 and 510 (between the first sensing element 505 and the second sensing element 512) may collapse in response to a force applied by one of a particular value. Because the air gaps 506, 510 are between the first sensing element 505 and the second sensing element 512, the first capacitive sensor 518 defined by the sensing elements can be used to determine the force up to a particular value. However, since the distance between the first sensing element 505 and the second sensing element 512 cannot be further reduced, the first capacitive sensor 518 will not detect the value of the applied force exceeding the specific value. However, after collapse of the air gaps 506, 510, the second capacitive sensor 519 can detect the force. Accordingly, in the case where both the first capacitive sensor 518 and the second capacitive sensor 519 generate a force value, the values may be added to determine the total force applied to the force sensing device 500. The same or a similar procedure can be used in conjunction with the force sensor described with respect to FIG. 26, wherein the conductive material 2614 and the first electrode layer 2622 form a first force sensor, and the first electrode layer 2622 and the second electrode layer 2630 A second force sensor is formed.

Figure 31 depicts an example program 3100 for determining one of the forces applied to a user input surface of an electronic device. Program 3100 can be implemented on any of the example devices discussed herein. For example, program 3100 can be used to determine what action, if any, the electronic device should perform in response to the force input, and can be implemented using, for example, the processing unit and other hardware components described with respect to FIG. Program 3100 can be implemented as processor-executable instructions stored in the memory of the electronic device.

In operation 3102, it is determined whether a sensor signal corresponds to one of a first spacer layer (eg, an air gap, as described above) or a second spacer layer (eg, a deformable element, as described above) Description) One of the variants, or a combination of the two. For example, the device can monitor a rate of change of a sensor signal. If the rate of change of the sensor signal satisfies a first condition (e.g., constant or below a threshold within a particular range of deformation), then the device can determine that an air gap is collapsing or has collapsed. If the rate of change of the sensor signal satisfies a second condition (eg, increases or exceeds the threshold within a particular range of deformation), the device can determine that an air gap has completely collapsed and a deformable component has Compressed or will be at least partially compressed. By way of another example, the device can indicate that the first spacer layer has completely collapsed based on whether a contact sensor (eg, the touch sensor described with respect to Figures 16 and 18A-22B) It is determined whether a sensor signal corresponds to collapse of one of the first spacer layer or a second spacer layer.

In operation 3104, a force deflection correlation is selected. As described herein, depending on whether the deflection of the force sensor corresponds to a collapse of one of the first spacer layers (eg, an air gap) or a deformation of a second spacer layer (eg, a deformable element), A different force deflects the correlation to determine an applied force. Thus, if the device determines at operation 3102 that the sensor signal corresponds to a deformation of one of the first spacer layers (such as a collapse of an air gap), then the device can select a first force deflection correlation at operation 3104. If the device determines at operation 3102 that the sensor signal corresponds to a deformation of one of the second spacer layers (such as compression of a deformable element), the device may select a second force deflection correlation at operation 3104, the The two-force deflection correlation is different from the first force deflection correlation.

In embodiments where the device includes a plurality of sensors across different spacer layers, such as the first capacitive sensor 518 and the second capacitive sensor 519, FIG. 5, the device can select and use multiple Force deflection correlation. For example, if the device determines at operation 3102 that the deflection corresponds to at least partial collapse of one of the first spacer layer and the second spacer layer, the device can select a suitable force deflection correlation for each sensor. .

In operation 3106, an applied force is determined based on the selected force deflection correlation. For example, the apparatus utilizes a look-up table, a stiffness-based force calculation, or another technique for performing the selected force deflection correlation, such that the amount of deflection indicated by the sensor signal is The specific applied forces are cross-correlated. In embodiments in which the device includes a plurality of sensors, the device can correlate the amount of deflection indicated by each sensor with a force value, and then, the force values from the respective sensors Determine the total force exerted by the general.

Based on the determined force applied, the device may (or not perform) a certain action. For example, if the applied force is below a threshold, the device can perform an action, and if the applied force is above the threshold, the device can perform another action. For example, if the force is below the threshold, the device can move a cursor to a position corresponding to the position of the touch event, and if the force is higher than the threshold, the device can A selection is made at that location of the cursor (eg, a mouse click). However, this is merely an example, and the range of possible actions that the device can perform based on the determined applied force is limited only by the capabilities of the device.

As mentioned above, a force sensor sheet or layer containing a conductive bezel can be used. For example, as described with respect to Figures 7, 10A, and 26-29, a conductive sheet can be used as a drive layer for a capacitive force sensing system. A conductive bezel can be applied to or otherwise included in the conductive sheets. 32 shows a fabrication on the surface of one of the sheets, such as one of the polarizers described with respect to FIGS. 26-29 or one of the force sensing elements 505 described with respect to FIGS. 5, 7, and 10A. A flow chart of a method of conducting a bezel. FIG. 32 will be described with reference to FIGS. 33 to 37. This method is described in conjunction with a roll-to-volume production process. Although described in connection with a polarizer, the procedure can be used to create a conductive bezel on any suitable film or substrate. Further, the method is described in connection with forming a continuous conductive bezel (see, for example, FIGS. 7 and 29), but the embodiment is not limited to this type of conductive bezel.

In other embodiments, other manufacturing processes can be used to create a conductive bezel on a polarizer or substrate. Example fabrication procedures include, but are not limited to, physical or chemical vapor deposition, screen printing or inkjet coating techniques using a shadow mask, and film masks and lithography.

Initially, as shown in block 3200, a mask is applied to one of the surfaces of a film. In one embodiment, the film is a polarizer film comprising a sheet of conductive material formed or coated on one surface of the polarizer film. As previously described, the polarizer film will be attached (eg, laminated) to the back surface of a display element and used as a polarizer for the display (eg, display element 2608 and rear polarizer 2610 in FIG. 26) ).

Each mask defines the area that will be surrounded by or within the conductive bezel. For example, the masks can define a user viewable area of a display (eg, user viewable area 108). Although depicted as having a rectangular shape, a mask can have any given shape and/or size.

In some embodiments, each mask can be one of a plurality of masks. For example, when a plurality of conductive strips are formed on a film substrate (see, for example, Figure 27), a mask defines regions that will not include conductive strips.

Figures 33A-33B depict the application of a mask to one of the surfaces of a film. As shown in Figure 33A, the application program 3300 includes moving the film 3302 from a first roll 3304 toward a second roll 3306 in a roll-to-roll production system. This movement is indicated by arrows 3308 in Figures 33A and 33B. In one embodiment, the second roller 3306 includes the finished product of the method illustrated in Figure 32 (e.g., a collection of conductive bezel formed on the surface of the polarizer film). In another embodiment, the second roll 3306 includes a collection of masks formed on the surface of the film (eg, finished product of block 3200).

A third roller 3310 is positioned between the first roller 3304 and the second roller 3306. The third roller 3310 includes a collection of masks 3312 that are applied to the film 3302 as the film 3302 moves under the third roller 3310. FIG. 33B illustrates a top view film 3302 after the mask 3312 has been applied to the film 3302 by the third roller 3310.

Referring now to block 3202 of Figure 32, a conductive material is formed over the surfaces of the masks and the film. The conductive material is used to form the material of the conductive bezel. Figures 34A-B show the formation of the conductive material over the film and the masks. Forming process 3400 includes moving film 3302 from a fourth roller 3402 toward a fifth roller 3404 (represented by arrow 3406). In an embodiment, the fourth roller 3402 corresponds to the first roller 3304 and the fifth roller 3404 corresponds to the second roller 3306. In such an embodiment, the fifth roller 3404 includes a collection of conductive bezels formed on the surface of the polarizer film (e.g., the finished product of the method shown in Figure 32). In other embodiments, the fourth roller 3402 includes the finished product of the block 3200.

In the illustrated embodiment, the membrane 3302 containing the mask 3312 enters a deposition chamber 3408, wherein a nozzle 3410 deposits conductive material 3412 onto the membrane 3302 and the mask 3312. The deposit can be deposited as a blanket such that the entire film 3302 and mask 3312 have a conductive material deposited thereon. FIG. 34B illustrates a top view film 3302 after deposition of conductive material 3412 to film 3302 and mask 3312 by deposition chamber 3408.

Referring now to block 3204 of Figure 32, a mask is removed from the surface of the film after the conductive material has been formed over the mask and the film. 35A-35B show the removal of the mask 3312 from the film 3302. The removal procedure 3500 includes moving the film 3302 from a sixth roller 3502 toward a seventh roller 3504 (represented by arrow 3506). In an embodiment, the sixth roller 3502 corresponds to the first roller 3304 and the seventh roller 3504 corresponds to the second roller 3306. In such an embodiment, the seventh roller 3504 includes the finished product of the method shown in FIG. In other embodiments, the sixth roller 3502 includes the finished product of the block 3202.

An eighth roller 3508 is positioned between the sixth roller 3502 and the seventh roller 3504. The eighth roller 3508 removes the mask 3312 leaving an area 3514 that only includes the membrane 3302. The conductive material is disposed on the region around the region 3514. FIG. 35B illustrates a top view of the film 3302 after the mask 3312 has been removed by the eighth roller 3508.

Any suitable procedure can be used to remove the mask 3312. For example, in one embodiment, the eighth roller 3508 employs an electrostatic technique to remove the mask 3312.

In some embodiments, an imaging system (eg, a camera) can be positioned over the membrane 3302 between the eighth roller 3508 and the seventh roller 3504. After the masks have been removed by the eighth roller 3508, the imaging system or automated optical inspection system can be used to detect if the film is defective.

Referring now to block 3206 in Figure 32, a protective layer is formed over the surface of the film and over the conductive material. 36A-36B illustrate the formation of the protective layer over the film and the conductive material. Forming process 3600 includes moving film 3302 from a ninth roller 3602 toward a tenth roller 3604 (represented by arrow 3606). In an embodiment, the ninth roller 3602 corresponds to the first roller 3304 and the tenth roller 3604 corresponds to the second roller 3304. In such an embodiment, the tenth roller 3604 includes the finished product of the method shown in FIG. In other embodiments, the ninth roller 3602 includes the finished product of the block 3204.

An eleventh roller 3608 is positioned between the ninth roller 3602 and the tenth roller 3604. The eleventh roll 3608 applies a protective layer 3610 over the film 3302 and the conductive material 3412. FIG. 36B illustrates a top view of film 3302 after protective layer 3610 has been applied by eleventh roll 3608.

Referring now to block 3208 in Figure 32, the conductive bezels are cut (e.g., single cut) to create individual segments of the film each surrounded by a conductive bezel. Figures 37A-37B illustrate the creation of individual sections of a film surrounded by a conductive bezel. The cutting procedure 3700 includes moving the film 3302 from a twelfth roller 3702 toward a thirteenth roller 3704 (represented by arrow 3706). In an embodiment, the twelfth roller 3702 corresponds to the first roller 3304 and the thirteenth roller 3704 corresponds to the second roller 3306. In such an embodiment, the thirteenth roller 3704 includes the finished product of the method shown in FIG. In other embodiments, the twelfth roller 3702 includes the finished product of the block 3206.

In the illustrated embodiment, a single-cut system 3708 is positioned over the membrane 3302 between the twelfth roller 3702 and the thirteenth roller 3704. The single cut system 3708 includes a precision die cutting tool 3710 that is aligned by one or more alignment cameras 3712.

In one embodiment, the precision die cutting tool 3710 uses one or more corners of the region 3514 (FIG. 35) as a cutting reference 3714 to position the die cut pattern 3716. FIG. 37B illustrates a top view of film 3302 including cutting reference 3714 and die cut pattern 3716 prior to cutting individual segments by die cutting tool 3710. Two single cut sections 3718 are also depicted in Figure 37B. Each single cut section 3718 includes a section of film 3720 surrounded by a conductive bezel 3722. As previously described, this section of film 3720 includes a sheet of conductive material formed over a polarizer film (e.g., a sheet of conductive material 2614 coated on polarizer 2610 after FIG. 26).

Referring to block 3210 in Figure 32, each single cut section can then be attached to a display layer. In particular, each single cut section can be laminated to one of the rear surfaces of a rear polarizer in the display layer.

The geometry of the geometry and/or die cut pattern (e.g., the die cut pattern 3716 in Fig. 37B) of the mask (e.g., mask 3312 in Fig. 33B) can be varied to adjust the geometry of the conductive border. 38 through 40 illustrate example techniques for determining the geometry of a conductive bezel. In FIG. 38, the die cut pattern 3800 is such that the mask 3802 is centered in a rectangular shape at the center of the die cut pattern 3800. After performing the single-cut procedure, the membrane 3806 includes a continuous rectangular conductive bezel 3804 extending along the edge of the membrane 3806.

As shown in FIG. 39, the die cut pattern 3900 is offset from the mask 3902 such that one edge of the mask 3902 is outside the die cut pattern 3900. After performing the single cut procedure, the membrane 3906 includes a U-shaped conductive bezel 3904. In the illustrated embodiment, the top of edge mask 3902 is external to die cut pattern 3900 to create a U-shaped conductive bezel 3904 that extends along both side and bottom edges of film 3906. However, other embodiments are not limited to this presentation. The shape and orientation of the conductive bezel 3804 determines which edge (or edges) of the mask 3902 is outside of the die cut pattern 3900.

40 illustrates a die cut pattern 4000 of three of the four edges of the mask 4002 that are external to the die cut pattern 4000. After performing the single-cut process, film 4006 includes a linear conductive frame 4004 that extends along one edge of film 4006. In the illustrated embodiment, only a portion of the bottom edge of the mask 4002 is positioned within the die cut pattern 4000 to create a linear conductive bezel 4004 that extends along the bottom edge of the film 4006. However, other embodiments are not limited to this configuration. The shape and orientation of the conductive bezel determines which edge (or edges) of the mask 4002 is outside of the die cut pattern 4000.

For the purposes of this description, the foregoing descriptions are used to provide a thorough understanding of the described embodiments. However, it will be apparent to those skilled in the art that the specific details are not essential to the embodiments described. Therefore, the particular embodiments described herein are intended to be illustrative and illustrative, and are not intended to be It will be apparent to those skilled in the art that many modifications and variations are possible in light of the above teachings. Furthermore, as used herein, the terms "above" and "below" or "synonym" of the component are not necessarily referring to the absolute position relative to an external reference, but instead Refers to the relative position of the components in the reference schema.

100‧‧‧Electronic devices

102‧‧‧ display

104‧‧‧Shell

106‧‧‧I/O devices

108‧‧‧Users can view the area

110‧‧‧Cleaning pieces

200‧‧‧ laptop computer; device

202‧‧‧ display

204‧‧‧ Shell

206‧‧‧track board

300‧‧‧assembly

301‧‧‧ District

302‧‧‧ Input force

303‧‧‧Cleaning pieces

304‧‧‧Upper stacking

305‧‧‧Intermediate components

306‧‧‧ Air gap

307‧‧‧ lugs

308‧‧‧Lower stacking

309‧‧‧Frame components

310‧‧‧ Air gap

311‧‧‧Combined components

312‧‧‧ stiffeners

313‧‧‧Light source

314‧‧‧Deformable components

315‧‧‧ Optical stacking

316‧‧‧Base structure or layer

317‧‧‧ District

401‧‧ points

402‧‧‧ points

404‧‧‧ points

406‧‧‧ first variable curve

408‧‧‧Second amount curve

500‧‧‧ force sensing device

504‧‧‧Upper stacking

505‧‧‧first sensing element; drive layer; first drive layer

506‧‧‧ Air gap

508‧‧‧Lower stacking

509‧‧‧ stiffening components

510‧‧‧ Air gap

511‧‧‧Selected anti-adhesion layer

512‧‧‧Second sensing element; sensing layer

514‧‧‧Deformable components

515‧‧‧ third sensing element; drive layer; second drive layer

516‧‧‧Base structure

518‧‧‧First Capacitive Sensor

519‧‧‧Second Capacitive Sensor

602‧‧‧ line

604‧‧‧ line

702‧‧‧Sensing area

704‧‧‧Drive area

706‧‧‧Connecting components

802‧‧‧Substrate

804‧‧‧Transmission layer

806‧‧‧Substrate

808‧‧‧Substrate

902‧‧‧Transmission path

1002‧‧‧Connector segmentation

1004‧‧‧ Conductive bonding materials

1006‧‧‧Connector segmentation

1008‧‧‧ Conductive Adhesive

1102‧‧‧ Conduction path

1200‧‧‧ force sensing device

1204‧‧‧Upper stacking

1206‧‧‧ Air gap

1207‧‧‧Frame components

1208‧‧‧Lower stacking

1209‧‧‧First sensing element

1210‧‧‧ Air gap

1213‧‧‧ Optical stacking

1214‧‧‧Deformable components

1215‧‧‧Second sensing element

1216‧‧‧Base structure

1218‧‧‧Capacitive sensor

Line 1302‧‧

Line 1304‧‧

1400‧‧‧ force sensing device

1402‧‧‧Capacitive sensor

Line 1502‧‧

1600‧‧‧ force sensing device

1604‧‧‧Upper stacking

1605‧‧‧First sensing element

1606‧‧‧ Air gap

1607‧‧‧Frame components

1608‧‧‧Lower stacking

1610‧‧‧Deformable components

1611‧‧‧Protruding

1612‧‧‧Sensor components

1614‧‧‧Second sensing element

1615‧‧‧ Air gap

1616‧‧‧Contact sensing area

1617‧‧‧ Optical stacking

1619‧‧‧Capacitive sensor

1620‧‧‧Base structure

1702‧‧‧ line

1704‧‧ points

1800‧‧‧ District

1802‧‧‧ lead

1804‧‧‧ lead

1806‧‧‧ lead

1808‧‧‧ lead

1810‧‧‧Sensing area

1900‧‧‧Base surface

2000‧‧‧Substrate

2100‧‧‧Contact Sensor

2102‧‧‧protrusion; deformable protrusion

2104‧‧‧Sensor components

2106‧‧‧ holes

2108‧‧‧layer; sensing element

2110‧‧‧Leader

2112‧‧ layer

2200‧‧‧Contact Sensor

2202‧‧‧Deformation protrusion

2204‧‧‧Sensor components

2206‧‧ layer

2208‧‧‧ lead

2210‧‧ layer

2300‧‧‧assembly

2302‧‧‧Sensor

2304‧‧‧First sensing element

2306‧‧‧Second sensing element

2308‧‧‧ District

2310‧‧‧Deformable part

2312‧‧‧First sensing element

2314‧‧‧Second sensing element

Line 2402‧‧

Line 2404‧‧

2502‧‧‧First drive area

2503‧‧‧Conductor

2504‧‧‧Second drive area

2505‧‧‧Conductor

2506‧‧‧Sensing area

2600‧‧‧Display stacking

2602‧‧‧Touch sensor

2604‧‧‧Display layer

2606‧‧‧Pre-polarizer

2608‧‧‧Display components

2610‧‧‧After polarizer

2612‧‧‧Transmission layer

2614‧‧‧Transmission material sheet

2616‧‧‧ Conductive border

2618‧‧‧Non-viewable area

2620‧‧‧Backlight unit

2622‧‧‧First electrode layer

2623‧‧‧ gap

2624‧‧‧Support structure

2626‧‧‧ gap

2627‧‧‧Back surface

2628‧‧‧Battery Pack

2630‧‧‧Second electrode layer

2632‧‧‧Touch and Sensing Circuitry

2634‧‧‧Drive Circuit System

2636‧‧‧Drive and sense circuitry

2638‧‧‧Drive Circuit System

2700‧‧‧Polarizer

2702‧‧‧Transmission strip

2704‧‧‧Transmission strip

2706‧‧‧Transmission strip

2708‧‧‧Transmission strip

2710‧‧‧Transmission material sheet

2800‧‧‧Polarizer

2802‧‧‧L-shaped conductive strip

2804‧‧‧Transmission material sheet

2900‧‧‧Polarizer

2902‧‧‧Continuous conduction border

2904‧‧‧Transmission material sheet

3000‧‧‧ device

3002‧‧‧Processing unit

3004‧‧‧ computer memory

3006‧‧‧Computer readable media

3008‧‧‧ display

3009‧‧‧Battery Pack

3010‧‧‧ Input device

3020‧‧‧Touch sensor

3022‧‧‧ force sensor

3024‧‧‧Sensor

3026‧‧‧ camera

3028‧‧‧Communication埠

3100‧‧‧Program operation

3102‧‧‧Operation

3104‧‧‧Operation

3106‧‧‧ operation

3200‧‧‧ Block

3202‧‧‧ Block

3204‧‧‧ Block

3206‧‧‧ Block

3208‧‧‧ Block

Block 3210‧‧‧

3300‧‧‧ application procedure

3302‧‧‧ film

3304‧‧‧First roll

3306‧‧‧Second roller

3308‧‧‧Arrows (moving)

3310‧‧‧third roll

3312‧‧‧ mask

3400‧‧‧ Formation procedure

3402‧‧‧fourth roller

3404‧‧‧ fifth roll

3406‧‧‧ arrow (mobile)

3408‧‧‧Deposition room

3410‧‧‧Nozzles

3412‧‧‧ mask

3500‧‧‧Remove procedures

3502‧‧‧6th roller

3504‧‧‧ seventh roller

3506‧‧‧Arrows (mobile)

3508‧‧‧8th roller

3514‧‧‧Area

3600‧‧‧ Formation procedure

3602‧‧‧9th roller

3604‧‧‧10th Roll

3606‧‧‧Arrows (moving)

3608‧‧‧11th Roll

3610‧‧‧Protective layer

3700‧‧‧ cutting procedure

3702‧‧‧12th Roll

3704‧‧‧13th Roll

3706‧‧‧Arrows (mobile)

3708‧‧‧Single system

3710‧‧‧Precision die cutting tools

3712‧‧‧Align the camera

3714‧‧‧ cutting reference

3716‧‧‧ die-cut pattern

3718‧‧‧Single section

3720‧‧‧ film

3722‧‧‧ Conductive border

3800‧‧‧ die-cut pattern

3802‧‧‧ mask

3804‧‧‧Continuous rectangular conductive border

3806‧‧‧film

3900‧‧‧ die-cut pattern

3902‧‧‧ mask

3904‧‧‧U-shaped conductive border

3906‧‧‧ Film

4000‧‧‧ die-cut pattern

4002‧‧‧ mask

4004‧‧‧ film

4006‧‧‧ film

The disclosure may be more readily understood by the following embodiments in conjunction with the accompanying drawings in which like reference numerals refer to similar structural components, wherein: FIG. 1 shows an example computing device incorporating one force sensing device. [Fig. 2] Another example arithmetic device incorporating a force sensing device is shown. 3A to 3E are partial cross-sectional views showing the apparatus of Fig. 1 taken along line A-A of Fig. 1. [Fig. 4] shows a deflection curve of a force with respect to the apparatus of Fig. 1. FIG. 5 is a cross-sectional view showing an example force sensing device taken along line A-A of FIG. 1. FIG. [Fig. 6] A deflection curve showing a force with respect to the force sensing device of Fig. 5. FIG. 7 is a developed view showing a sensing element of the force sensing device of FIG. 5. FIG. FIG. 8 is a partial cross-sectional view showing the sensing element of FIG. 7 taken along line C-C of FIG. 7. FIG. [Fig. 9] A sensing element showing one of the force sensing devices of Fig. 5. [Fig. 10A to 10B] An embodiment of another sensing element of the force sensing device of Fig. 5 is shown. [Fig. 11] Still another sensing element showing the force sensing device of Fig. 5. FIG. 12 is a cross-sectional view showing another example force sensing device taken along line A-A of FIG. 1. FIG. [Fig. 13] shows a deflection curve of a force with respect to the force sensing device of Fig. 12. Fig. 14 is a cross-sectional view showing still another example of the force sensing device taken along line A-A of Fig. 1. [Fig. 15] shows a deflection curve of a force with respect to the force sensing device of Fig. 14. Fig. 16 is a cross-sectional view showing still another example of the force sensing device taken along line A-A of Fig. 1. [Fig. 17] A deflection curve showing a force with respect to the force sensing device of Fig. 16. 18A to 18B are exploded cross-sectional views showing the force sensing device of Fig. 17. [Fig. 19] A perspective view showing a deformable member. [Fig. 20] A perspective view showing a sensing element. 21A-21B are cross-sectional views showing an example contact sensor. 22A-22B are cross-sectional views showing another example contact sensor. 23A-23B are partial cross-sectional views of the apparatus of Fig. 1 taken along line A-A of Fig. 1, showing an embodiment of integrating a force sensing system in the apparatus. [Fig. 24] A deflection curve showing a force with respect to the force sensing system of Figs. 23A to 23B. [Fig. 25] A sensor showing one of the force sensing systems of Figs. 23A to 23B. FIG. 26 is a cross-sectional view showing an example embodiment of the electronic device of FIG. 1 taken along line B-B of FIG. 1. FIG. [FIG. 27] A first example configuration depicting one of the conductive bezels on the polarizer shown in FIG. [Fig. 28] A second example configuration of one of the conductive bezels depicted on the polarizer shown in Fig. 26. [Fig. 29] A third example configuration depicting one of the conductive bezels on the polarizer shown in Fig. 26. [FIG. 30] An example component showing an electronic device. [Fig. 31] shows an example program for determining the force applied to a user input surface. [Fig. 32] shows an example program for manufacturing a conductive bezel on one surface of a polarizer. [Fig. 33A to Fig. 33B] depicting the application of a mask to one surface of a film. [Fig. 34A to Fig. 34B] showing formation of a conductive material over the film and the mask. [Fig. 35A to Fig. 35B] showing the removal of the mask from the film. [Fig. 36A-36B] shows the formation of a protective layer over the film and conductive material. [Fig. 37A-37B] shows various sections that produce a film surrounded by a conductive bezel. [Fig. 38] A first example technique for determining the geometry of a conductive bezel. [Fig. 39] shows a first example technique for determining the geometry of a conductive bezel. [Fig. 40] A first example technique for determining the geometry of a conductive bezel.

The cross-hatching or shading used in the figures is generally provided to clarify the boundaries between adjacent elements and also to aid in the identification of the drawings. Accordingly, the presence or absence of cross-hatching or shading is not an expression or indication of the particular material, material properties, component proportions, component dimensions, or versatility of similarly depicted components of any of the elements illustrated in the drawings, or A preference or requirement for any other characteristic, attribute or property.

Claims (20)

An electronic device comprising: a user input surface defining an outer surface of the electronic device; a first capacitive sensor comprising a first pair of sensing elements, between the first pair of sensing elements Having an air gap, and the first capacitive sensor is configured to determine a first applied force on the user input surface that causes one of the air gaps to collapse; and a second capacitive sensor Under the first capacitive sensor, the second capacitive sensor includes a second pair of sensing elements, the second pair of sensing elements have a deformable element therebetween, and the second capacitive sensor is Configuring to determine a second applied force on the user input surface that causes deformation of one of the deformable elements. The electronic device of claim 1, wherein: the first pair of sensing elements comprises: a common sensing element; and a first driving element spaced apart from the common sensing element and capacitively coupled to the common sensing element And the second pair of sensing elements comprise: the common sensing element; and a second driving element spaced apart from the common sensing element and capacitively coupled to the common sensing element. The electronic device of claim 2, further comprising: a display layer comprising: a display element positioned below the user input surface; and a rear polarizer positioned below the display element; a conductive material a sheet formed over a rear surface of one of the rear polarizers to create a conductive surface on the rear surface of the rear polarizer; and a conductive bezel formed along at least one edge of the sheet of conductive material. The electronic device of claim 3, wherein the conductive bezel is positioned outside of a user viewable area of the display layer. The electronic device of claim 3, wherein the sheet of conductive material comprises a silver nanowire. The electronic device of claim 2, further comprising: a display element coupled to the first drive element; and a base structure, wherein: the display element is configured to flex relative to the base structure; the deformable An element is coupled to the base structure; and the air gap is positioned between the deformable element and the display element. The electronic device of claim 6, wherein the common sensing element is coupled to the deformable element. A capacitive force sensor for an electronic device, comprising: a first driving layer; a second driving layer positioned relative to the first driving layer; a common sensing layer at the a driving layer and the second driving layer; a first spacer layer between the first driving layer and the common sensing layer; and a second spacer layer in the common sensing layer and the Between the second drive layers. The capacitive force sensor of claim 8, wherein: the first spacer layer comprises an air gap; and the capacitive force sensor further comprises: a pair of opposing surfaces that define the air gap; and an anti-adhesion A layer configured to prevent adhesion between the opposing surfaces. The capacitive force sensor of claim 9, wherein the second spacer layer comprises an array of deformable protrusions extending from a substrate layer. The capacitive force sensor of claim 8, further comprising a sensing circuit system operatively coupled to the first driving layer, the second driving layer, and the common sensing layer, and Configuring to determine: a first applied force that results in a change in thickness of one of the first spacer layers; and a second applied force that results in a change in thickness of one of the second spacer layers. The capacitive force sensor of claim 6, wherein the first driving layer comprises: an insulating substrate; a conductive material sheet formed on a rear surface of one of the insulating substrates to be in the insulating substrate a conductive surface is formed on the rear surface; and a conductive frame is formed along at least one edge of the conductive material sheet. The capacitive force sensor of claim 12, wherein the conductive bezel comprises a continuous conductive bezel extending along the edges of the sheet of conductive material. A capacitive force sensor according to claim 12, wherein the conductive bezel comprises one or more conductive strips formed along respective edges of one of the sheets of conductive material. An electronic device comprising: a cover member defining a user input surface of the electronic device; a first sensing element coupled to the cover member within an internal volume of the electronic device; a frame member, Coupled to the cover member and extending into the interior volume of the electronic device; a second sensing element coupled to the frame member; and a third sensing element coupled to a base structure and responsive thereto The layers are separated. The electronic device of claim 15, wherein: the frame member defines an opening; and the third sensing element is capacitively coupled to the second sensing element through the opening. The electronic device of claim 15 wherein the first sensing element comprises a layer of continuous transparent conductive material substantially covering an entire surface of one of the substrates. The electronic device of claim 17, wherein: the second sensing element comprises a plurality of sensing regions; and the continuous transparent conductive material layer overlaps the plurality of sensing regions of the plurality of sensing regions. The electronic device of claim 18, wherein: the third sensing component comprises a plurality of driving regions; and each of the driving regions overlaps the plurality of sensing regions of the plurality of sensing regions. The electronic device of claim 17, wherein: the first sensing element further comprises a connection element electrically coupled to the layer of continuous transparent conductive material; and the electronic device further comprises: sensing circuitry configured to provide An electrical signal to the first sensing element; and a connector segment electrically coupled to the sensing circuit to the connecting element.