WO2017074925A1 - Architecture for achieving stable wave propagation through a soft material - Google Patents

Architecture for achieving stable wave propagation through a soft material Download PDF

Info

Publication number
WO2017074925A1
WO2017074925A1 PCT/US2016/058639 US2016058639W WO2017074925A1 WO 2017074925 A1 WO2017074925 A1 WO 2017074925A1 US 2016058639 W US2016058639 W US 2016058639W WO 2017074925 A1 WO2017074925 A1 WO 2017074925A1
Authority
WO
WIPO (PCT)
Prior art keywords
bistable
architecture
elements
mechanical
series
Prior art date
Application number
PCT/US2016/058639
Other languages
French (fr)
Inventor
Jennifer A. Lewis
Jordan R. RANEY
Katia Bertoldi
Chiara Daraio
Dennis KOCHMANN
Neel NADKARNI
Original Assignee
President And Fellows Of Harvard College
California Institute Of Technology
Eth Zurich
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by President And Fellows Of Harvard College, California Institute Of Technology, Eth Zurich filed Critical President And Fellows Of Harvard College
Publication of WO2017074925A1 publication Critical patent/WO2017074925A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F3/00Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic
    • F16F3/08Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic with springs made of a material having high internal friction, e.g. rubber
    • F16F3/087Units comprising several springs made of plastics or the like material
    • F16F3/0873Units comprising several springs made of plastics or the like material of the same material or the material not being specified
    • F16F3/0876Units comprising several springs made of plastics or the like material of the same material or the material not being specified and of the same shape
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00Springs
    • F16F1/36Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/373Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by having a particular shape

Definitions

  • the present disclosure is related generally to soft architectures and more particularly to bistable structures formed from soft materials that may be useful for wave propagation.
  • Soft, highl deforrnable materials have enabled the desig of new classes of tunable and responsive systems and devices, including bioinspired soft robots, seif-rogul&tlng niicroflu dics, ada tive optics, reusable energy- absorbing systems, structures with highly programmable responses, and mofipbologicai computing paradigms.
  • bioinspired soft robots seif-rogul&tlng niicroflu dics
  • ada tive optics reusable energy- absorbing systems
  • structures with highly programmable responses and mofipbologicai computing paradigms.
  • An architecture for achieving stable wave propagation through a sof material Includes a plurality of bistable elements arranged In series.
  • Each bistable element comprises a soft .material and h s two stable configurations * a higher energy configuration and; a lower energy configuration.
  • the bistable elements are configu ed to snap from the igher energy configuration to the lower energy configuration sequentially when stimulated by a mechanical wave, thereb allowing the mechanical wave to propagate therethrough.
  • a mechanical logic device comprises a first input chain comprising a first plurality of bistable elements arranged in series, a second input chain comprising a second plurality of bistable elements arranged in series, and an output chain connected to the first and second Input chains and comprising a third plurality of bistable elements arranged in series.
  • Each bistable element comprises a soft material and has two stable configuratio s * a higher energy configuration and a lower energy configuration.
  • the bistable elements are configured to snap from the highe energy configu ation to the lower energy configuration sequentially when stimulated by a mechanical wave, thereby allowing fie mechanical wave to propagate therethrough.
  • the mechanical logic device may be configured as a mecha ical OR gate or a mechanical AMD gate, £0097
  • bistable element comprises a soft material nd has two stable
  • the first bistable element Is simulated by a mechanical wave and Induced to snap from the hig er to the tower e e g configuration.
  • the mechanical wave thereby passes through the first bistable element and stimulates arc adjacent bistable element.
  • the stimulation of adjacent bistable elements continues until the mechanical wave has propagated through ail of the plurality of bistable elements.
  • a method of fabricating an architecture for achieving stable wave propagation through a soft material includes extruding an ink formulation from deposition o zle moving relative to a substrate, wher the ink formulation comprises an unaired polymer.
  • One or mom continuous filaments comprising the ink formulation are deposited In a predetermined pattern on the substrate.
  • an as-printed architecture comprising a plurality of printed structures arranged In series is formed, where each printed structure comprises the uncured polymer. The uncured polymer is cured so as to form, from the printed
  • bistable elements arranged i aeries, where each bistable element is In a km energy configuration and comprises a soft material...
  • the bistable elements are then deformed to have a deformed geometry, such that each bistable element adopts a higher energy configuration ⁇
  • the bistable elements are configured to snap from the higher energy configuration to the low energy configuration sequentially when stimulated by a mechanical wave, thereby allowing the mechanic l wave to propagate therein rough.
  • Fie. 1 A shows an exemplary soft architecture for achieving wave propagation that includes a plurality of bistable elements arranged in series.
  • the bistable elements have two stable configurations * a lower energy configuration and a higher energy configuration.
  • the bistable elements are in the lower energy configuration in FIG. 1 A..
  • FIG. 1 B shows a close-up view of three of the bistable elements of FIG. 1A
  • the bistable elements are physically connected fey coupling, elements having the form of linear springs.
  • FIG, 1 C shows a ciose-u vie® of t ree of the bistable elements of FIG. 1A in a higher energy, deformed configuration
  • FIG. 2A shows force F and potential energy V versus d splacement 3 ⁇ 4 for the coupling elements of RGs ⁇ 1A ⁇ 1C,
  • FIG, 28 shows a portion of an exemplary soft architecture Including a plurality of bistable elements in series, where the linea coupling elements have a different geometry than the springs shown in FIGs, 1A-1C.
  • FIG, 2C shows a plot of force F versus displacement * for linear coupling elements of various sizes and geometries.
  • FIG. 3 shows force F and potential energy V versus displacement x for the bistable elements of FIGs,. 1 A-1G.
  • FIGs, 4A and 4B show force F and potential energy V as a function of displacement* and end-fo-end distance dfor bistable elements ha ing the geometry shown in FIGs. 1A-1C.
  • FIGs, 5A-5B show simulated values of pulse velocity and puls width, respectively, as a function ofend-to-end distance d a d coupling element stiffness
  • FIG. 5C shows an approximate ene gy barrier E m for an entire propagating pulse, which is a function of both d and k, by combining the
  • FIG, 6 is a contour map showing normalized displacement For eac bistable unit of a sertes having a variation I d along the lengt , from distance dt TM 14,5 mm at one end to a distance d2 TM 19.0 mm at the other end, A wave propagating through such an accelerator may exhibit a ⁇ -fold increase in wave p ed moving from the first end to the second end of the series,
  • FI , ? shows n exemplary soft mechanical diode co structed from a heterogeneous chain (series) of bistable elements, where a first region of the series Includes soft coupling: elements (e.g., k - 60 Ni m) inking adjacent bistable elements, and a second region of the series includes stiff coupling elements (e.g., k - 2,100 N/m) linking adjacent bistable elements.
  • FiGs. 8A and SB show optical images and a contour map, res ectively, of fie behavior of amodul ⁇ oliated in the soft region of the mechanical diode of FIG, ? when i! encounters the soft-stiff boundary.. (Propagation is halted).
  • FIGs, 9A and 98 show optical images and a contour map, respectively, of the behavior of a pulse foliated in the stiff region of the mechanical diode of FIG., 7 when It encounters the stiff-soft boundary. (Propagation continues).
  • FIG. 10 shows an exemplary soft mechanical logic device that includes a first input chain comprising a first plurality of bistable elements arranged in series, a second input chain comprising a second plurality of bistable elements arranged in series, and an output chain connected to the first and second: input chains, where the output chain comprises a third plurality of bistable elements, arranged in series,
  • FiGs.. 11 A and 118 show the soft mechanical logic device of FIG, 10 configured as an AND gate.
  • [O025J F!Gs. 12A and 12B show t e soft mechanical logic device of FIG. 10 configured as an OR gate.
  • FIG, 3 Is a schematic of a 3D printing process in which a filament comprising a viscoeiastlc ink composition is extruded through a moving deposition i ozzl and deposited on an underlying substrate,
  • FIG,. 14 illustrates propagation of a stable nonlinear transition ave through an exemplary architecture, with each bistable element undergoing a displac ment from x ⁇ x to x « x*
  • the instability 3 ⁇ 4 may propagate with constant velocity and geometry,; enabled by both ⁇ the balance of nonlinear and dispersive effects and ) the balance of dissipation and energy release.
  • FIGs, 15A and 158 sho contour maps of an exemplary architecture during wave propagation, where the wave pulse Is in compression (FIG. 1SA) or tension (FIG. 158).
  • FIGs. ISC and ISO show optical Images obtained from a high-speed camera during wave propagation, corresponding to the experimental data in
  • FIGs, 151 and 15F show simulated compression-initiated nd tension- initiated pulses, respectively:, which sho excellent agreement with the experimental data shown In FIGs. 15 arsd 15B,
  • bistable elements comprising a sot material that are capable of storing elastic energy in the form of deformation are used. When stimulated by the wave-front, the bistable elements release the energy as the wave propagates, without the need of any externa! stimulus. Dissipation allows stable wave propagation by balancing the elastic energy release.
  • the damping intrinsic to the soft materials may remove all signals except the desired transition wave, which therefore can propagate with high fidelity, predictability, and controllability.
  • Such architectures may serve as the ack one of functional devices, such as soft mechanical logic devices,
  • FIG. 1A shows an exemplary architecture 100 fo achieving stable wave propagation through a soft material
  • the architecture 100 includes a plurality of bistable elements 102 arranged in series,.
  • Each bistable element 102 comprises a soft material, such as an elasto eric material or other polymer, and has two stable- configurations, higher energy configuration 106, as shown in FIG,. 1C S and a lower energy configuration 104,.
  • FIG. B When simulated by a mechanical wave, the istable elements 102 snap torn the higher energy configuration 106 to the lower energy configuration 104 in a sequential fashion, thereby allowing the mechanical wave to propagate th ough the
  • each: bistable element 102 includes a first beam portion 110 attached to a second be m portion 112, thereby defining a junction or node 114 in a mldportfon of the bistable element 102, as described further below,
  • Adjacent bistable elements 102 may be coupled together by a physical connection or by a force fi d (e.g.,, a magnetic -field), in the architecture of FIGs, 1A-1C, coupling elements 108 exte d between and physically connect adjacent bistable elements 102, Th functions or nodes 114 e ween the first and second beam portions 110,112 can serve as connection points for the coupling elements 08,
  • a ⁇ G include small metallic cylinders press fit into the soft material to add a mass concentration; at each node and to provide optical contrast for tracking wave propagation during eriments.
  • the bistable elements 102 may be arranged in series along a longitudinal axis U, as shown, but generally speaking the serial arrangement of bistable elements need not: follow a straight line.
  • the bistable elements 102 may be seriall arranged along a curved line,
  • Each bistable element includes at least one constrained portion that is constrained from motion, while an unconstrained portion of the bistable element is free to snap (transition) from the higher to the lower energy configuration when stimulated by a mechanical w ve. As shown in FIGs, 1 -1C, both ends
  • each bistable element 102a, 102b of the bistable elements 102 may be constrained from, motion while mtdportions 102m thereof (which Include the junctions 4 ⁇ are free to transition from the higher energy configuration 06 to the lower energy configuration 104,
  • the ends 1 : G2a,1Q2b of each bistable element 102 may be fixedly or translatably secured to constraints 1 6 positioned adjacent to fie plurality of bistable
  • the constraints 116 may be attached to or may be pari of longitudinally oriented bars 118, as shown In FIG. 1A.
  • the constraints 116 may be spaced apart a. distance as illustrated In Fie, 18, The distance tf may be constant or variable along the series,, depending on the desired behavior of the wave.. T us, the longitudinally oriented bars 1 18 may e oriented either substantially parallel to or nonp ra!lel to the longitudinal axis L s ,
  • the first and second beam portions 110,112 re substantially straight a d have opposing life with respect to he longitudinal axis L s .
  • the first beam portion 110 has a negative till with respect to the longitudinal axis L 3 ⁇ 4 and the second beam portion 112 has a positive tilt with respect to the longitudinal axis L*
  • the first, and second beam portion 110,112 of this example have a teng!tvto- thickness aspect ratio of 18, where the length is J mm, in the higher energ configuration 106 sh wn
  • the first and second team portions 110,112 have a deformed (e.g., non-straight) geometry, which Is capable of storing energy.
  • Other geometries are possible also, as long as each bistable element i cludes stable higher and lower energy configurations that allow energy to be stored In the architecture,
  • the coupling elements 108 of FIGs. 1A*1C take the form of springs having a zigzag geometry.
  • the springs xhibit a linear relationship between force F and displacement ⁇ ( m shown in FIG, 2A,. where the slope of the line represents the stiffness k
  • the coupling elements 108 may be referred to as linear coupling elements.
  • the springs have a length of 0 mm :f a width of 5 m, a thickness of 5,4 mm, and a stiffness k of 80 N/m
  • suitable linear coupling elements 108 may have any geometry that exhibits linear behavior in respon e to an applied force, such as the cellular structures show in FIG, 2B.
  • FIG. 2C shows force versu s displace men! data for exemplary linea r coupling elements 108 of different sizes and geometries (springs and cellular structures).
  • the measured 1 stiffness values range from about 30 N/m to about 2,100 N/m.
  • the coupling elements 108 may alternative ⁇ be designed to e ibi a nonlinear relationship between force and displacement Such coupling eiements may be referred to as nonl near coupling elements, Exemplary nonlinear coupling elements Include spheres Sr Hertzian contact, where force F ⁇ x)
  • the coupling element 108 may comprise a soft material
  • tie soft material may comprise one or more polymers, such as an elastomer (&.g ,, a silicone, polyuret ane, palybutadiene, or neoprene).
  • elastomers include poiydimeti ylsHoxane PDMS) and Dragon Skin® .
  • the soft material may also or alternatively comprise a *smarf material, such as a shap memory polymer, that can return to a previous "remembered" shape when triggered by a stimulus, such as a temperature change or light exposure.
  • the soft material of the coupling eiements 108 may he the same as or different f om that of the bistable elements 102, It is also contemplated that the cou ling elements 108 may co ise a hard material ⁇ e.g», a non-polymeric solid) such as a metal, alloy or semiconductor. Hard materials may exhibit elastic moduli much higher than the elastic moduli of soft materials.
  • the bistable elements 102 and the coupling elements 1 8 are each formed of a material that may be 3D printed, a discussed further below.
  • Toe stiffness k may be nfluenced by the geometry of the coupling elements 1 8 and also by their chemical composition (e.g., hard or soft material), in the case of 3D i ted architectures, process conditions ( .g extrusion/print speed) also may play a role in determining the stiffness t
  • the stiffness k of th (linear) coupling elements 108 is in the range from about 1 Him to out 3,00 Him, or from about 33 Him to about 2,100 Him, £O041
  • FIG. 3 shows force F and potential ene gy F as a function of displace merit x for the bistable elements W2 of FfGs.
  • bistable elements 102 exhibit a highly nonlin ar response when a fore ⁇ fs applied, with a region of negative in emeriia! stiffness (negative slope ⁇ :.
  • the associated instability can lead to a rapid shape change that has been studied In the context of both natural and synthetic stems.
  • Th potential energy r"( v) Is characterised by two local minima at x TM * ! ⁇ 0 and ,* - corresponding to the two stable configurations shown in FIGs. 1 B a d 1C.
  • the potential energy is defined such that d ⁇ 8x ⁇ -Fand is calculated by first itiing a fifth-degree polynomial io the measured force-displacement data and then integrating.
  • the stable conjuration at x* (corresponding to the higher energy configuration 108) Is characterised by an energ state higher than that of the stable configuration at x*' ⁇ 0 (corresponding to the lower energy configuration 104). Therefore, similar to a. phase transition, the transition ⁇ or snapping) between the two stable states involves a net change in stored potential energy. Depending on the director! of the tra sition energy is either absorbed or released.
  • the architecture 100 typically includes at least six bistable elements and may include- as many as (or more than) 100 bistable elements.
  • the bistable etemenis may in some cases be myfiistabie elements that have more than two stabl
  • the architecture may not enable propagation of small-amplitude elastic waves over long distances; however, moderate* and large* amplitude excitation can lead to a very different response, if the bistable elements are initially set to thei lower*energy
  • a method of propagating mechanical signals In a soft material may entail: providing a plurality of bistable elements arranged in series, where each bistable element comprises a soft material and has two stable configurations, a higher energy configuration and a lower energy configuration; and stimulating: a first bistable element by a mechanical wave, causing the first bistable element to snap (transition) from the higher to the lower energy configuration.
  • the transition allows the mechanical wave to pass through the first bistable element and to stimulate an adjacent bistable element, which also snaps (transitions) to the lower energy configuration .
  • the stimulation of adjacent bistable elements continues until the mechanical wave has propagated through all of the bistable elements.
  • the bistable elements may be coupled together by a physical connection or by a force field (e.g., a magnetic Held), as described above.
  • first bistable lement m y be positioned at an end of the ply r lly of bistable elements, and the mechanical wave may propagate In a single direction (e.g., toward the other end).
  • first bistable element may be positioned at an intermediate location in the plurality of bistable elements, and the mechanical wave may propagate in more than one direction simultaneously ⁇ &.g, f tow rd both ends),
  • the mechanical wave may propagate as a compressive wave pulse in one direction and as a ra refraction wave pulse In the other direction.
  • the soft material may comprise a smart mater al, such as a s pe memory polymer, either alone or in combination with another polymer.
  • the smart material may e ogr mmed to return to a "mmembered" configuration upon exposure to a suitable stimulus, as kno n: n the art and discussed in, for example, M, Be hi and A. Lendleln, "Sh e Memory Polymers " terials Toda , 10, 4, 200?, pp. 20-28.
  • the method may further include, after propagation of Hie mechanical wave through tie plurality of bistable elements, exposure of the smart material to a stimulus In order to activate the smart, material, thereby retumsng each bistable element from the lower energy configuration to the higher energy configuration.
  • the stimulus m y be a change in temperature or exposure to ultraviolet f : UV) radiation, for example.
  • the soft architecture may be reset and used again for wave propagation
  • the width of the pulse and it propagation velocity can be greatly changed by manipulating the nonlinear response of the .bistable elements: 102 and/or (in the case of linear coupling elements) the stiffness k.
  • changes in k require fabrication, of new units with different morphology, as shown by the data of FIG, 20, it is possible to exploit the high doformabi ty of soft materials to tune the nonlinear response of the bistable elements.
  • the application of small lateral loads can change the ertd-to*end distance d
  • FfG. SO provides an a rox m te energy barrier i3 ⁇ 4 ; for an .entire propagating poise, which is a function of both d and k, by combining the measu ed energy landscape- of the individual bistable elements (FIG,. 48) with fit simulated puts ⁇ widths of FIG, SB.
  • an accelerator can be designed by applying different values of d spatially along the length of the architecture to achieve a controlled variation In wave velocity. This can be done without fabricating a specifically graded system because the deformable architecture allows different values of d to he applied as a function of length.
  • the bistable elements may be arranged In series along a longitudinal axis and each bistable element may be secured
  • longitudinally oriented constraints positioned adjacent to the plurality of bistable elements.
  • the distance of between the longitudinally oriented constraints may be varied: as desired along the longitudinal axis (®.g tf linear Increase or decrease, exponential increase or decrease, ste wise change, etc).
  • a mechanical diode is designed as a
  • heterogeneous chain or series of bistable elements where a first region Includes soft coupling elements linking adjacent bistable elements and a second region includes stiff coupling elements linking adjacent bistable elements.
  • t e coupling elements n the first region of the aeries have a stiffness k d the coupling elements In a second region of the series have a stiffness A3 ⁇ 4 where 3 ⁇ 4 >
  • FIG. 7 shows an example of such an architecture
  • Stat Includes 25 bistable elements wi h soft coupling elements (ki ⁇ 80 N/m) and 25 bistable elements with stiff coupling elements (!3 ⁇ 4 ⁇ 2,100 N/m), with d - 17.5 mm.
  • SC t propagating poises In these two distinct portions of the architecture encounter very different energy barriers. Consequently, the architecture can functiono as a mechanical diode,
  • the pulse freezes indefinitely at the soft-stiff boundary, with the wave energy that has not already been dissipated being stored In the elastic deformation of tie local structure, pOSSl
  • a pulse initiated in the stiff region readily propagates through the sot region as well, although a kink in wave velocit is observed at the transition between stiff and soft, as a result of ihe change in L
  • the fact that the wave velocity rapidly changes at the boundary is a manifestation of the system's insertsi!ivity to initial conditions.
  • the large* amplitude wave appears to be essenti lly Insensitive to any fabrication-induced imperfections i the architecture.
  • SSSJ A mom complex logic device is shown in FIG. 10.
  • This device includes a first Input chain comprising a first plurality of bistable elements arranged in series, a second Input chain comprising a second plurality of bistable elements arranged in series, and an output chain connected to the first and second Input chains, where the output chain comprises a third plurality of bistable elements arranged In series.
  • Each bistable element comprises a soft material and has two stable configurations, a higher energy configuration and a lower energy configuration:.
  • the bistable elements are configured to snap from the higher energy configuration to the lower energy configuration sequentially when stimulated by a mechanical wav , thereby allowing the mechanical wav to propagate therethrough.
  • the logic device may be configured as an AND gate or an OR gate,
  • the logic device may f urther comprise a first set of constraints positioned along both sides of the first input chain adjacent to the first plurality of bistable elements; a second set of constraints positioned along both sides of the second input chain adjacent to the second plurality of bistable elements; and a third set of constraints positioned along both sides of the output chain adjacent to the third plurality of bistable elements.
  • Ends of eac bistable element may be fixedly secured to trie respective adjacent constraints, and a distance d between the first set of constraints may be substantially the same as the distance d between the second set of constraints.: if a distance between the third set of constraints is less lhan the distance d, then the logic device may function as a mechanical AND gate. Alternatively, if the distanc d m between the third set of constraints is greater than the distance d, then the logic device may function as a mechanical OR gate.
  • the logic gate of FIG. 10 includes coupling elements ail having the same value of k (80 N/m i this example), with the first and second Input chains having d « 17,5 mm.
  • d &ll 3 ⁇ 4 when the end-to-end distance, d &ll 3 ⁇ 4, of the bistable elements In the output chain is small in comparison to d (e.g., o s ⁇ 16,? mm), the energy barrier is sufficiently igh fiat both Input chains need to be activated by propagating: transition waves n order to achieve wave propagation through t e output chain.
  • Such a configuration yields a soft mechanical logical AND gate
  • the architecture can become a logical OR gate when is increased sufficiently relative to d to ⁇ 18.6 mm), as shown in FiGs, 12A and 12B. in this case, because the energy barrier of the outpot chain is smaller (less than 0,1 mJ), if either of the input chains has propagated the transition wave, the wave can propagate through the output chain. Similar behavio can be obtained by other combinations of bistable element geometries and linear cooping eleme ts, using FIG, 5C as a guide.
  • Ail of the architectures described in this disclosure may be fo med by 3D printing, an extrusion-based printing process that may also be referred to as direct ink writing or direct write fabrication. Referring to FIG, 13, 3D printing:
  • the deposition nozzle may be moved at: a constant or variable print speed V while the substrate remains stationary, as shown In FIG, 13, Alternatively the substrate may be moved while the deposition nozzle remains stationary * or both the deposition noz le and the substrate may be moved. While the substrate is typically a solid, 3D printing may be carried out using a gel or liquid as a substrate.
  • the ink formulation extruded through the deposition nozzle is viseoelastic with a strain-rate dependent viscosity
  • the ink formulation ma also be said to be shear-th inning.
  • deposited on the substrate may have a sufficient stiffness to retain its shape and a h 3 ⁇ 4ht h.
  • An exemplary ink formulation and 3D printing process is described below. Further descriptions of 3D printing may he found in U.S. Patent
  • a soft: material includes extruding an ink formulation from a deposition nozzle moving relative to a substrate, where the ink formulation comprises an uncured polymer, One or mom continuous filaments comprising the ink formulation are deposited in a predetermined pattern on the substrate, as illustrated in FIG, 13.
  • an as-printed architecture comprising a plurality of printed structures arranged in series s formed, where each printed structure comprises the unoured polymer.
  • the uncured polymer is cured to form (from the printed structures) a plurality of bistable elements arranged in series, where each bistable element Is in a low energy configuration and comprises a soft material (e.g., a polymer as described previously),
  • the bistable elements are deformed to have a deformed geometry, such that each bistable element adopts a higher energy configuration.
  • the bistable elements are configured to snap from the higher energy configuration to the low (lower) energy configuration
  • bistable elements formed as described above may have any of the features described elsewhere in this disclosure, Including, for example, coupling elements, constraints, etc.
  • the exemplary architectures ma b produced using direct ink: writing, an extrusion -based 3D printing method, which may be followed by an Infilling step.
  • a visooeiastic poiydimethyisiioxane (POMS) ink formulation is used for 3D printing.
  • This ink formulation includes a she -thinning POMS material, Dow Coming SE-1700 (85 wt.%), with a Sower-viscosity POMS additive, Dow Coming Sylgard 184 (IS wt.% ⁇ .
  • the viscoelaatio yield properties are theologically tailored to ensure that the uncured ink lows readily during printing yet maintains its shape until it is permanently cross-linked In a subsequent curing step ⁇ e,g, s 100 * G for 30 rain).
  • the ink formulation Is extruded through a tapered noz ⁇ e (e.g?,, 20 ⁇ ⁇ ⁇ inner diameter, obtained from Nordson EFD) during programmed translation; of the nozzle over a fixed substrate ⁇ e.g., PTFE-coated aluminum), as shown schematically in FIG. 13.
  • Ink extrusion may be controlled via. fixed pressure (Nordson EFD Ultimus V pressure box), with the ozzle precisely positioned using a custom 3D positioning stage (Aerotech).
  • a cylindrical copper rod $.g, t 3. 75 mm diameter is cut to pieces (e.g., 5,1 ? mm length, giving; a mass of -0.4? gj, which can be press fit Into the printed bistable elements to enable optical tracking of portions of the architecture during wave propagation.
  • top surfaces of the copper cylinders are painted with flat white paint to m&xirnke light contrast for visualization of the transition wave propagation.
  • stiffness values range from 30 to 2 * 100 N/m (as measured with a commercial quastsfatic test system, Instron 5586, in displacement control at a displacement rale of 2
  • Additional intermediate values can fee obtained by varying the translation speed of the printbead during the printing process.
  • FIG * 14 illustrates the propagation of the nonlinear wave by showing for each unit lis
  • the pulse width for any time can be extracted from the ma by taking a. horizontal slice of the plot ( e, s a fixed time) and measuring the number of bistable elements in the midst of transitioning between the solid dark and solid Sight regions (approximately four elements in width).
  • Another uni ue aspect of this system is that the propagation velocity and pu!se shape are the same (w thin the margin of error) whether the wave is initiated in compression or tension, as revealed S y comparison of tri contour plots reported in FIG, 15 A.
  • FIGs. ISC and 5D show optical images obtained during wave propagation from a high-speed camera * corresponding to the data in FIOs. 15A and 158, respectively,
  • Transition wave propagation is also characterized using a 1D mechanical model, in which the position of the middle of the - bistable element
  • the bistable potential V is numerically computed by nonlinear flnite-eiernent simulations of a qyasisfaticsl!y deforming, co- rofafional, linear elastic beam;
  • 2D The numerical force-displacement curves are validated tsy comparison with the experimental data shown in FIG, 3,
  • All nodes are placed in the high-energ configuration.-
  • the first node is then excited by displacing: it from the high-energy stable point to the low-energy one, and the system response In time Is solved using a Newmark- ⁇ scheme..
  • model parameter ⁇ is determined by fling experimental wave speed data for a particular combination of geometric parameters (k TM 80 Him and ⁇ ⁇ 17.5 mm). With all model parameters thereby determined, architectures with different combinations of geometric parameters c n he examined ' .
  • FIGs. 15E and 1SF show simulated compression-initiated and tension- initiated pulses, respectively, which show excellent agreement with the

Abstract

An architecture for achieving stable wave propagation through a soft material comprises a plurality of bistable elements arranged in series. Each bistable element comprises a soft material and has two stable configurations, a higher energy configuration and a lower energy configuration, The bistable elements are configured to snap from the higher energy configuration to the lower energy configuration sequentially when simulated by a mechanical wave, thereby allowing the mechanical wave to propagate therethrough. Adjacent bistable elements may be coupled together by a physical: connection or by a force laid.

Description

ARCHITECTURE FOR ACHIEVING STABLE WAVE PROPAGATION
THROUGH A SOFT MATERIAL
RELATED APPLICATION
[0001] The present patent document claims the benefit of priority under 35 iiS.C. 119(e) to U,S. Provisional Patent Application No. 62/246,433, filed on October 2§!: 2015, which Is hereby incorporated by reference in its entirety.
TECHNICAL FIELD
[ 082] The present disclosure is related generally to soft architectures and more particularly to bistable structures formed from soft materials that may be useful for wave propagation.
BACKGROUND
[0003] Soft, highl deforrnable materials have enabled the desig of new classes of tunable and responsive systems and devices, including bioinspired soft robots, seif-rogul&tlng niicroflu dics, ada tive optics, reusable energy- absorbing systems, structures with highly programmable responses, and mofipbologicai computing paradigms. However, their highly deformabls and dissfpatlve nature also oses unique challenges. Although It has been
demonstrated that the nonlinear response of soft structures can be exploited to design machine capable of performing surprisingly sophisticated functions on actuation, their hig intrinsic dissipation has prevented the design of completely soft machi es. Se sing and control functionalities, which require transmission of a signal over a distance, still typically rely on the Integration of stiff electronic components within the so material, introducing interfaces that are often a source of mechanical failure*
[0004] The design of soft control and sensing systems {and, consequently, completely sot machines) requlms the ability to ropagate: a stable signal without distortion through soft media. There are two limiting factors intrinsic to materials that work against this: dispersion (signal distortion doe to frequency-dependent phase velocity) and dissipation (loss of energ over time as the wave propagates through the medium). Dispersion can be controlled or eliminated through nonlinear effects produced via the control of structure in th medium. For example, periodic systems based on Hertzian contact, tensegrlty structures, rigid bars and linkages, and bistable elastic elements can behave as nondispersive media, with the nonlfneartty of their local mechanical response canceling out the tendency for the signal to disperse at sufficiently large amplitudes. However, dissipation m still an overarching problem. Structures designed to propagate elastic waves are typically built from stiff materials with low intrinsic dissipation (e.g., metals) and excited with small-amplitud excitation (to avoid plastic energy loss). This approach minimizes, but does not eliminate, dissipation., in soft, highly dlsslpattve media, the problem is farther exacerbated, and there is no robust strategy currentl available to propagat signal© in these systems,
BRIEF SUMMARY
£09Θ5| An architecture for achieving stable wave propagation through a sof material Includes a plurality of bistable elements arranged In series. Each bistable element comprises a soft .material and h s two stable configurations* a higher energy configuration and; a lower energy configuration.. The bistable elements are configu ed to snap from the igher energy configuration to the lower energy configuration sequentially when stimulated by a mechanical wave, thereb allowing the mechanical wave to propagate therethrough.
ΪΟ0093 A mechanical logic device comprises a first input chain comprising a first plurality of bistable elements arranged in series, a second input chain comprising a second plurality of bistable elements arranged in series, and an output chain connected to the first and second Input chains and comprising a third plurality of bistable elements arranged in series. Each bistable element comprises a soft material and has two stable configuratio s* a higher energy configuration and a lower energy configuration. The bistable elements are configured to snap from the highe energy configu ation to the lower energy configuration sequentially when stimulated by a mechanical wave, thereby allowing fie mechanical wave to propagate therethrough. The mechanical logic device may be configured as a mecha ical OR gate or a mechanical AMD gate, £0097| A method of propagating mechanical signals m a soft material
comprises providing a plurality of bistable elements arranged in series,, where each: bistable element comprises a soft material nd has two stable
configurations, a higher energy configuration and a lower ene gy configuration. The first bistable element Is simulated by a mechanical wave and Induced to snap from the hig er to the tower e e g configuration. The mechanical wave thereby passes through the first bistable element and stimulates arc adjacent bistable element. The stimulation of adjacent bistable elements continues until the mechanical wave has propagated through ail of the plurality of bistable elements.
£00383 A method of fabricating an architecture for achieving stable wave propagation through a soft material includes extruding an ink formulation from deposition o zle moving relative to a substrate, wher the ink formulation comprises an unaired polymer. One or mom continuous filaments comprising the ink formulation are deposited In a predetermined pattern on the substrate. Thus, an as-printed architecture comprising a plurality of printed structures arranged In series is formed,, where each printed structure comprises the uncured polymer. The uncured polymer is cured so as to form, from the printed
structures* a plurality of bistable elements arranged i aeries, where each bistable element is In a km energy configuration and comprises a soft material... The bistable elements are then deformed to have a deformed geometry, such that each bistable element adopts a higher energy configuration► The bistable elements are configured to snap from the higher energy configuration to the low energy configuration sequentially when stimulated by a mechanical wave, thereby allowing the mechanic l wave to propagate therein rough.
BRIEF DESCRIPTION OF THE DRAWINGS
0i | Fie. 1 A shows an exemplary soft architecture for achieving wave propagation that includes a plurality of bistable elements arranged in series. The bistable elements have two stable configurations* a lower energy configuration and a higher energy configuration. The bistable elements are in the lower energy configuration in FIG. 1 A..
(0010| FIG. 1 B shows a close-up view of three of the bistable elements of FIG. 1A The bistable elements are physically connected fey coupling, elements having the form of linear springs. £0011! FIG, 1 C shows a ciose-u vie® of t ree of the bistable elements of FIG. 1A in a higher energy, deformed configuration,
[0012] FIG. 2A shows force F and potential energy V versus d splacement ¾ for the coupling elements of RGs< 1A~1C,
[0013] FIG, 28 shows a portion of an exemplary soft architecture Including a plurality of bistable elements in series, where the linea coupling elements have a different geometry than the springs shown in FIGs, 1A-1C.
[001 ] FIG, 2C shows a plot of force F versus displacement * for linear coupling elements of various sizes and geometries.
[001 S] FIG. 3 shows force F and potential energy V versus displacement x for the bistable elements of FIGs,. 1 A-1G.
£ 0 0 FIGs, 4A and 4B show force F and potential energy V as a function of displacement* and end-fo-end distance dfor bistable elements ha ing the geometry shown in FIGs. 1A-1C.
£0017! FIGs, 5A-5B show simulated values of pulse velocity and puls width, respectively, as a function ofend-to-end distance d a d coupling element stiffness
[0010] FIG. 5C shows an approximate ene gy barrier Em for an entire propagating pulse, which is a function of both d and k, by combining the
measured energy landscape of the individual bistable elements (FIG. 40) with tie simulated pulse- widths of FIG, 58,
£0019] FIG, 6 is a contour map showing normalized displacement For eac bistable unit of a sertes having a variation I d along the lengt , from distance dt14,5 mm at one end to a distance d219.0 mm at the other end, A wave propagating through such an accelerator may exhibit a β-fold increase in wave p ed moving from the first end to the second end of the series,
[0020] FI , ? shows n exemplary soft mechanical diode co structed from a heterogeneous chain (series) of bistable elements, where a first region of the series Includes soft coupling: elements (e.g., k - 60 Ni m) inking adjacent bistable elements, and a second region of the series includes stiff coupling elements (e.g., k - 2,100 N/m) linking adjacent bistable elements. |0 21| FiGs. 8A and SB show optical images and a contour map, res ectively, of fie behavior of a puis© oliated in the soft region of the mechanical diode of FIG, ? when i! encounters the soft-stiff boundary.. (Propagation is halted).
[0022] FIGs, 9A and 98 show optical images and a contour map, respectively, of the behavior of a pulse foliated in the stiff region of the mechanical diode of FIG., 7 when It encounters the stiff-soft boundary. (Propagation continues).
[0023] FIG. 10 shows an exemplary soft mechanical logic device that includes a first input chain comprising a first plurality of bistable elements arranged in series, a second input chain comprising a second plurality of bistable elements arranged in series, and an output chain connected to the first and second: input chains, where the output chain comprises a third plurality of bistable elements, arranged in series,
[0024] FiGs.. 11 A and 118 show the soft mechanical logic device of FIG, 10 configured as an AND gate.
[O025J F!Gs. 12A and 12B show t e soft mechanical logic device of FIG. 10 configured as an OR gate.
[002$] FIG, 3 Is a schematic of a 3D printing process in which a filament comprising a viscoeiastlc ink composition is extruded through a moving deposition i ozzl and deposited on an underlying substrate,
[ 027] FIG,. 14 illustrates propagation of a stable nonlinear transition ave through an exemplary architecture, with each bistable element undergoing a displac ment from x ^ x to x « x* The instability ¾ may propagate with constant velocity and geometry,; enabled by both {ή the balance of nonlinear and dispersive effects and ) the balance of dissipation and energy release.
Snapshots of the evolving state of She ch in are shown, ith: |.t ~ 0.128 s, ~ 0.194 s, and ™ 0.252 s relative to the start of the experiment, in this case wlh « 18.8 mm,
[0020] FIGs, 15A and 158 sho contour maps of an exemplary architecture during wave propagation, where the wave pulse Is in compression (FIG. 1SA) or tension (FIG. 158). 029] FIGs. ISC and ISO show optical Images obtained from a high-speed camera during wave propagation, corresponding to the experimental data in
F!Gs. ISA a d SB, respectively,
03393 FIGs, 151 and 15F show simulated compression-initiated nd tension- initiated pulses, respectively:, which sho excellent agreement with the experimental data shown In FIGs. 15 arsd 15B,
DETAILED DESCRIPTION
[00313 Described herein is an architected mediom. made of a highly
dlssipat!ve, soft material that can overcome both dispersive nd d!ssi ative effects and enable the propagation of a mechanical signal over arbitrary distances without distortion., A stable mechanical signal can be transmitted over long distances through a dissipative medium only If additional energy is continuously suppled during its propagation. To achieve such behavior, bistable elements comprising a sot material that are capable of storing elastic energy in the form of deformation are used. When stimulated by the wave-front, the bistable elements release the energy as the wave propagates, without the need of any externa! stimulus. Dissipation allows stable wave propagation by balancing the elastic energy release. The damping intrinsic to the soft materials may remove all signals except the desired transition wave, which therefore can propagate with high fidelity, predictability, and controllability.
[§032] The architectures described herein, which can be fabricated and customized by 30 printing, ar capable of propagating stable waves with constant velocity over arbitrary distances, overcoming both dissipative and dispersive effects, despite th soft, dissipailve material of which they are
composed. Such architectures may serve as the ack one of functional devices, such as soft mechanical logic devices,
[00333 FIG. 1A shows an exemplary architecture 100 fo achieving stable wave propagation through a soft material The architecture 100 includes a plurality of bistable elements 102 arranged in series,. Each bistable element 102 comprises a soft material, such as an elasto eric material or other polymer, and has two stable- configurations, higher energy configuration 106, as shown in FIG,. 1CS and a lower energy configuration 104,. as shown In FIG. B, When simulated by a mechanical wave, the istable elements 102 snap torn the higher energy configuration 106 to the lower energy configuration 104 in a sequential fashion, thereby allowing the mechanical wave to propagate th ough the
architecture Thus, energy issipation in the soft material may fee countered by the energy released as each testable element 102 transitions to the tower energy configuration 104, n this exemplary architecture 100, each: bistable element 102 includes a first beam portion 110 attached to a second be m portion 112, thereby defining a junction or node 114 in a mldportfon of the bistable element 102, as described further below,
[00343 Adjacent bistable elements 102 may be coupled together by a physical connection or by a force fi d (e.g.,, a magnetic -field), in the architecture of FIGs, 1A-1C, coupling elements 108 exte d between and physically connect adjacent bistable elements 102, Th functions or nodes 114 e ween the first and second beam portions 110,112 can serve as connection points for the coupling elements 08, The nodes 114 in the architecture of FIGs. A~ G include small metallic cylinders press fit into the soft material to add a mass concentration; at each node and to provide optical contrast for tracking wave propagation during eriments. The bistable elements 102 may be arranged in series along a longitudinal axis U, as shown, but generally speaking the serial arrangement of bistable elements need not: follow a straight line. For example, the bistable elements 102 may be seriall arranged along a curved line,
[00353 Each bistable element includes at least one constrained portion that is constrained from motion, while an unconstrained portion of the bistable element is free to snap (transition) from the higher to the lower energy configuration when stimulated by a mechanical w ve. As shown in FIGs, 1 -1C, both ends
102a, 102b of the bistable elements 102 may be constrained from, motion while mtdportions 102m thereof (which Include the junctions 4} are free to transition from the higher energy configuration 06 to the lower energy configuration 104, The ends 1:G2a,1Q2b of each bistable element 102 may be fixedly or translatably secured to constraints 1 6 positioned adjacent to fie plurality of bistable
elements 102 in both the lower and higher energy configurations 104,106, The constraints 116 may be attached to or may be pari of longitudinally oriented bars 118, as shown In FIG. 1A. The constraints 116 may be spaced apart a. distance as illustrated In Fie, 18, The distance tf may be constant or variable along the series,, depending on the desired behavior of the wave.. T us, the longitudinally oriented bars 1 18 may e oriented either substantially parallel to or nonp ra!lel to the longitudinal axis Ls,
|δ038] Irt the lower energy configuration 104 shown In FIG. 1 Bs the first and second beam portions 110,112 re substantially straight a d have opposing life with respect to he longitudinal axis Ls. In this exam e, the first beam portion 110 has a negative till with respect to the longitudinal axis L¾ and the second beam portion 112 has a positive tilt with respect to the longitudinal axis L* The first, and second beam portion 110,112 of this example have a teng!tvto- thickness aspect ratio of 18, where the length is J mm, in the higher energ configuration 106 sh wn In FIG, 1Ct the first and second team portions 110,112 have a deformed (e.g., non-straight) geometry, which Is capable of storing energy. Other geometries are possible also, as long as each bistable element i cludes stable higher and lower energy configurations that allow energy to be stored In the architecture,
[0037 The coupling elements 108 of FIGs. 1A*1C take the form of springs having a zigzag geometry. The springs xhibit a linear relationship between force F and displacement χ( m shown in FIG, 2A,. where the slope of the line represents the stiffness k Thus, the coupling elements 108 may be referred to as linear coupling elements. In this example, the springs have a length of 0 mm:f a width of 5 m, a thickness of 5,4 mm, and a stiffness k of 80 N/m, it should be noted that suitable linear coupling elements 108 may have any geometry that exhibits linear behavior in respon e to an applied force,, such as the cellular structures show in FIG, 2B. Using different geometries for the linear coupling elements 108 may lead to different effective stiffnesses, which can influence the characteristics of the propagating mechanical wave, as discussed below. FIG, 2C shows force versu s displace men! data for exemplary linea r coupling elements 108 of different sizes and geometries (springs and cellular structures). The measured1 stiffness values range from about 30 N/m to about 2,100 N/m. p038] The coupling elements 108 may alternative^ be designed to e ibi a nonlinear relationship between force and displacement Such coupling eiements may be referred to as nonl near coupling elements, Exemplary nonlinear coupling elements Include spheres Sr Hertzian contact, where force F{x)
Increases according to or magnets that couple the bistable elements via a magnetic fi ld, as discussed in Nadfcaml et at, Physical R tew Letters i 16, 244501 (2016),
Like the bistefeie eiements 102, the coupling element 108 may comprise a soft material As indicated above, tie soft material may comprise one or more polymers, such as an elastomer (&.g ,, a silicone, polyuret ane, palybutadiene, or neoprene). Specific examples of suitable elastomers include poiydimeti ylsHoxane PDMS) and Dragon Skin® . The soft material may also or alternatively comprise a *smarf material, such as a shap memory polymer, that can return to a previous "remembered" shape when triggered by a stimulus, such as a temperature change or light exposure. Use of such a material may permit the bistable element to be reset from the low energy configuration to the high energy configuration after transmission of a wave through the soft architecture. The soft material of the coupling eiements 108 may he the same as or different f om that of the bistable elements 102, It is also contemplated that the cou ling elements 108 may co ise a hard material {e.g», a non-polymeric solid) such as a metal, alloy or semiconductor. Hard materials may exhibit elastic moduli much higher than the elastic moduli of soft materials. Advantageously, the bistable elements 102 and the coupling elements 1 8 are each formed of a material that may be 3D printed, a discussed further below.
[00491 Toe stiffness k may be nfluenced by the geometry of the coupling elements 1 8 and also by their chemical composition (e.g., hard or soft material), in the case of 3D i ted architectures, process conditions ( .g extrusion/print speed) also may play a role in determining the stiffness t Typically, when soft materials ar utilized, the stiffness k of th (linear) coupling elements 108 is in the range from about 1 Him to out 3,00 Him, or from about 33 Him to about 2,100 Him, £O041| FIG. 3 shows force F and potential ene gy F as a function of displace merit x for the bistable elements W2 of FfGs. 1 It can be observed that the bistable elements 102 exhibit a highly nonlin ar response when a fore© fs applied, with a region of negative in emeriia! stiffness (negative slope}:. The associated instability can lead to a rapid shape change that has been studied In the context of both natural and synthetic stems. Th potential energy r"( v) Is characterised by two local minima at x *! ~ 0 and ,* - corresponding to the two stable configurations shown in FIGs. 1 B a d 1C. The potential energy is defined such that d¥~8x ~ -Fand is calculated by first itiing a fifth-degree polynomial io the measured force-displacement data and then integrating. The stable conjuration at x* (corresponding to the higher energy configuration 108) Is characterised by an energ state higher than that of the stable configuration at x*'∞ 0 (corresponding to the lower energy configuration 104). Therefore,, similar to a. phase transition, the transition {or snapping) between the two stable states involves a net change in stored potential energy. Depending on the director! of the tra sition energy is either absorbed or released. The release of energy associated with a transition from the higher to the lower energy state can be exploited to overcome dissipation: and propagate a mechanical signal over arbitrary distances, as Indicated above, enabling the design of soft and highly tunable devices, such as the mechanical logic elements described below; The architecture 100 typically includes at least six bistable elements and may include- as many as (or more than) 100 bistable elements. The bistable etemenis may in some cases be myfiistabie elements that have more than two stabl
configurations,
[0O42| Due to the intrinsic damping of the soft material, the architecture may not enable propagation of small-amplitude elastic waves over long distances; however, moderate* and large* amplitude excitation can lead to a very different response, if the bistable elements are initially set to thei lower*energy
(yndeformed) stable e»«f¾ymtlon (x ~ s*™ 0 In FIG. 3, corresponding to FIG. 18), even a large amplitude displacement may not lead to a transition wave due to the energetically unfavorable {energy-absorbing) transition of each bistable element. Small-amplitude linear modes may also disintegrate because of dissipation; fhus, there may be no stable modes of energy transport whan the elements are in the low-energy state. However, f the bistable elements are initially set to their higher-energy (deformed) stable configuration (a? - 9 in FIG, 3, corresponding to FIG, 1C)» a sufficiently large displacement applied to any of the bistable elements cam cause the displaced bistable element to transition states, producing a nonlinear transition wave that propagates Indefinitely outward from the paint of initiation with constant speed and shape. This can be attributed to both (0 an
Figure imgf000012_0001
between dispersive and nonlinear effects of the architecture and (« a release of energy that overcomes the effects of dissipation as each of the bistable elements, stimulated by th wsvefront, transitions from its higher- to lower-energy stable state (i,e,,: from x « xf to x « ¾f » G).
£0O43| Consequently, a method of propagating mechanical signals In a soft material may entail: providing a plurality of bistable elements arranged in series, where each bistable element comprises a soft material and has two stable configurations, a higher energy configuration and a lower energy configuration; and stimulating: a first bistable element by a mechanical wave, causing the first bistable element to snap (transition) from the higher to the lower energy configuration. The transition allows the mechanical wave to pass through the first bistable element and to stimulate an adjacent bistable element, which also snaps (transitions) to the lower energy configuration . The stimulation of adjacent bistable elements continues until the mechanical wave has propagated through all of the bistable elements. The bistable elements may be coupled together by a physical connection or by a force field (e.g., a magnetic Held), as described above.
[00443 Tlie first bistable lement m y be positioned at an end of the ply r lly of bistable elements, and the mechanical wave may propagate In a single direction (e.g., toward the other end). Alternatively, the first bistable element may be positioned at an intermediate location in the plurality of bistable elements, and the mechanical wave may propagate in more than one direction simultaneously {&.g,f tow rd both ends), The mechanical wave may propagate as a compressive wave pulse in one direction and as a ra refraction wave pulse In the other direction. P&4SJ As indicated abo e, the soft material may comprise a smart mater al, such as a s pe memory polymer, either alone or in combination with another polymer. By incorporating a smart material into the bistable elements, it ma be possible to reset each bistable element from the lower energy configuration to the higher energy configuration after propagation of t e mechanical wave. The smart material may e ogr mmed to return to a "mmembered" configuration upon exposure to a suitable stimulus, as kno n: n the art and discussed in, for example, M, Be hi and A. Lendleln, "Sh e Memory Polymers " terials Toda , 10, 4, 200?, pp. 20-28. Thus, the method may further include, after propagation of Hie mechanical wave through tie plurality of bistable elements, exposure of the smart material to a stimulus In order to activate the smart, material, thereby retumsng each bistable element from the lower energy configuration to the higher energy configuration. The stimulus m y be a change in temperature or exposure to ultraviolet f:UV) radiation, for example. In this way, the soft architecture may be reset and used again for wave propagation
£00463 The width of the pulse and it propagation velocity can be greatly changed by manipulating the nonlinear response of the .bistable elements: 102 and/or (in the case of linear coupling elements) the stiffness k. Although changes in k require fabrication, of new units with different morphology, as shown by the data of FIG, 20, it is possible to exploit the high doformabi ty of soft materials to tune the nonlinear response of the bistable elements. For example, the application of small lateral loads can change the ertd-to*end distance d
[004?] Simulations are used to systematically investigate the effects of the parameters d and k on the behavior of the propagating wave. The obtained force- displacement corves ere subsequently integrated to determine the on-site potential, and an eighth-order polynomial fit Is used as an approximation fo V(x), as shown for four representative values of d in FIGs, 4A and 48, It can be observed that d has a large effect on the energy harrier separating the two stable configurations, which is reflected also In changes in the peak forces during transition- Furthermore, d strongly affects the displacement necessary to obtain snap-through from the high-energy state to the low-energy state (and thus to initiate th transition during wave propagation). The effects of 4 and k on wave propagation velocity and pulse width are shown In P!Gs, BA and 5B and discussed further below. FfG. SO provides an a rox m te energy barrier i¾; for an .entire propagating poise, which is a function of both d and k, by combining the measu ed energy landscape- of the individual bistable elements (FIG,. 48) with fit simulated puts© widths of FIG, SB.
£06 81 Given that the energy barrier for propagation of a transition wave can be controlled by tuning; d and &, the inventors recognized that functional devices can be designed by carefully arranging the linear and nonlinear elements in the series (ί&,, along the chain). Since pulse propagation is substantially or entirely independent of initial conditions, the wave poise can be- manipulated through entirely local geometric changes. Dye to fee high damping of the system, only the specific signal compatible with the local geometric parameters may he able to propagate an appreciable distance.
00 13 Several exemplary mechanical devices based on soft architectures comprising series arrangements of bistable elements are described* including a wave accelerator, a mechanical diode and mechanical logic gates,
£60501 In a first example, an accelerator can be designed by applying different values of d spatially along the length of the architecture to achieve a controlled variation In wave velocity. This can be done without fabricating a specifically graded system because the deformable architecture allows different values of d to he applied as a function of length. The bistable elements may be arranged In series along a longitudinal axis and each bistable element may be secured
(fixedly or translaiabiv) to longitudinally oriented constraints positioned adjacent to the plurality of bistable elements. The distance of between the longitudinally oriented constraints may be varied: as desired along the longitudinal axis (®.gtf linear Increase or decrease, exponential increase or decrease, ste wise change, etc).
£60511 Experimental results are shown m FIG, 6 for a series of bistable elements, where d varies linearly from about 14.5 mm at one end to about 19 mm at the other end. The results show a change In siope of the interface between the pre-transitioned and post-transltfone states (dark and light regions,
respectively), indicating a variation in pulse velocity,, as the slope of the interface is Inversely proportional to the speed1. In this example, a change in the wave speed by more than a factor of 6 from the left: end of the series to the right end can be achieved (from 0.8 mis to 5.2 mis,). The velocity can he seen to
continually vary along the length of the chain, but at each location it {matches the expected velocities from: FIG, 5A,
£0652| *n another example, a mechanical diode is designed as a
heterogeneous chain or series of bistable elements, where a first region Includes soft coupling elements linking adjacent bistable elements and a second region includes stiff coupling elements linking adjacent bistable elements. Specifically, t e coupling elements n the first region of the aeries have a stiffness k d the coupling elements In a second region of the series have a stiffness A¾ where ¾ >
|0653! FIG. 7 shows an example of such an architecture Stat Includes 25 bistable elements wi h soft coupling elements (ki ~ 80 N/m) and 25 bistable elements with stiff coupling elements (!¾ ~ 2,100 N/m), with d - 17.5 mm. As shown in FIG. SC t propagating poises In these two distinct portions of the architecture encounter very different energy barriers. Consequently, the architecture can functio as a mechanical diode,
£0O54| Referring to FIGs, 8A and 8BS when a pulse is initiated in the soft region (k - 80 Him), where it possesses a small width -4 units) and a resulting tow energ barrier (Em 0.2-0,3 mJ < it is unable to continue propagating when it reaches the stiff region (k - 2.100 N/m), where a wide pulse {-2 units) and high- energy barrier are encountered (E * 1 md}.. As a result, the pulse freezes indefinitely at the soft-stiff boundary, with the wave energy that has not already been dissipated being stored In the elastic deformation of tie local structure, pOSSl In contrast, referring to FIGs, 9A and 9B, a pulse initiated in the stiff region readily propagates through the sot region as well, although a kink in wave velocit is observed at the transition between stiff and soft, as a result of ihe change in L The fact that the wave velocity rapidly changes at the boundary is a manifestation of the system's insertsi!ivity to initial conditions. Also, the large* amplitude wave appears to be essenti lly Insensitive to any fabrication-induced imperfections i the architecture. SSSJ A mom complex logic device is shown in FIG. 10. This device, a mechanical logic gate, includes a first Input chain comprising a first plurality of bistable elements arranged in series, a second Input chain comprising a second plurality of bistable elements arranged in series, and an output chain connected to the first and second Input chains, where the output chain comprises a third plurality of bistable elements arranged In series. Each bistable element comprises a soft material and has two stable configurations, a higher energy configuration and a lower energy configuration:. The bistable elements are configured to snap from the higher energy configuration to the lower energy configuration sequentially when stimulated by a mechanical wav , thereby allowing the mechanical wav to propagate therethrough.
iueSTJ One can define the high-energy state (e,g,., .x. * .r*9 in FIG. 3} of the bistable eleme ts as logical state 0 d the low-energy state ( ~ in FIG. 3) as logical stats 1 and then design systems that predictably control pulse propagation in accordance with the energy barrier relationships in FIG. SC. The logic device may be configured as an AND gate or an OR gate,
Cif 8] For example, the logic device may f urther comprise a first set of constraints positioned along both sides of the first input chain adjacent to the first plurality of bistable elements; a second set of constraints positioned along both sides of the second input chain adjacent to the second plurality of bistable elements; and a third set of constraints positioned along both sides of the output chain adjacent to the third plurality of bistable elements. Ends of eac bistable element may be fixedly secured to trie respective adjacent constraints, and a distance d between the first set of constraints may be substantially the same as the distance d between the second set of constraints.: if a distance between the third set of constraints is less lhan the distance d, then the logic device may function as a mechanical AND gate. Alternatively, if the distanc dm between the third set of constraints is greater than the distance d, then the logic device may function as a mechanical OR gate.
[0fK?9] The logic gate of FIG. 10 includes coupling elements ail having the same value of k (80 N/m i this example), with the first and second Input chains having d « 17,5 mm. Referring ow to FIGs, 11A and 118, when the end-to-end distance, d&ll¾, of the bistable elements In the output chain is small in comparison to d (e.g., o s ~ 16,? mm), the energy barrier is sufficiently igh fiat both Input chains need to be activated by propagating: transition waves n order to achieve wave propagation through t e output chain. Such a configuration yields a soft mechanical logical AND gate,
£06ββ| However, the architecture can become a logical OR gate when is increased sufficiently relative to d to ~ 18.6 mm), as shown in FiGs, 12A and 12B. in this case, because the energy barrier of the outpot chain is smaller (less than 0,1 mJ), if either of the input chains has propagated the transition wave, the wave can propagate through the output chain. Similar behavio can be obtained by other combinations of bistable element geometries and linear cooping eleme ts, using FIG, 5C as a guide.
[0661] Ail of the architectures described in this disclosure may be fo med by 3D printing, an extrusion-based printing process that may also be referred to as direct ink writing or direct write fabrication. Referring to FIG, 13, 3D printing:
entails flowing a rheoiogicaliy-iaiared ink formulation through a deposition nozzle that is moving relative to a substrate* such that a filament comprising the Ink composition may be deposited on the substrate in a. predetermined 2:0 or 3D pattern.. In this way 30 printing; may be employed to build up 3D structures layer by layer. During 30 printing, the deposition nozzle may be moved at: a constant or variable print speed V while the substrate remains stationary, as shown In FIG, 13, Alternatively the substrate may be moved while the deposition nozzle remains stationary* or both the deposition noz le and the substrate may be moved. While the substrate is typically a solid, 3D printing may be carried out using a gel or liquid as a substrate.
[fl0i.2| Advantageously, the ink formulation extruded through the deposition nozzle is viseoelastic with a strain-rate dependent viscosity, The ink formulation ma also be said to be shear-th inning. As shown in FIG. 13, the filament
deposited on the substrate may have a sufficient stiffness to retain its shape and a h ¾ht h. An exemplary ink formulation and 3D printing process is described below.. Further descriptions of 3D printing may he found in U.S. Patent
Application Serial No, 14/900,860, Hied December 22, 2015;;; US, Patent Application Serial No. 15/146,613* fi ed May 4, 2016: U,S. Patent Application Serial No. 16/036,937, fi ed M y 18, 2018,; and U.S. Patent Application Serial No. 15/117,623, filed August 9, 2018, ail of which are hereby incorporated by reference In their entirety,
§β§3] Generally speaking, a method of fabricating an architecture fo
achieving stable w ve propagation -through a soft: material includes extruding an ink formulation from a deposition nozzle moving relative to a substrate, where the ink formulation comprises an uncured polymer, One or mom continuous filaments comprising the ink formulation are deposited in a predetermined pattern on the substrate, as illustrated in FIG, 13. Thus, an as-printed architecture comprising a plurality of printed structures arranged in series s formed, where each printed structure comprises the unoured polymer. Typically after depositing the one or more continuous filaments, the uncured polymer is cured to form (from the printed structures) a plurality of bistable elements arranged in series, where each bistable element Is in a low energy configuration and comprises a soft material (e.g., a polymer as described previously), The bistable elements are deformed to have a deformed geometry, such that each bistable element adopts a higher energy configuration. The bistable elements are configured to snap from the higher energy configuration to the low (lower) energy configuration
sequentially when stimulated by a mechanical wave, thereby allowing the mechanical wave to propagat therethrough. The architecture and serially- arranged bistable elements formed as described above may have any of the features described elsewhere in this disclosure, Including, for example, coupling elements, constraints, etc.
£096 | The exemplary architectures ma b produced using direct ink: writing, an extrusion -based 3D printing method, which may be followed by an Infilling step. A visooeiastic poiydimethyisiioxane (POMS) ink formulation is used for 3D printing. This ink formulation includes a she -thinning POMS material, Dow Coming SE-1700 (85 wt.%), with a Sower-viscosity POMS additive, Dow Coming Sylgard 184 (IS wt.%}. The viscoelaatio yield properties are theologically tailored to ensure that the uncured ink lows readily during printing yet maintains its shape until it is permanently cross-linked In a subsequent curing step {e,g,s 100* G for 30 rain). The ink formulation Is extruded through a tapered noz^e (e.g?,, 20Ό μι ϊ inner diameter, obtained from Nordson EFD) during programmed translation; of the nozzle over a fixed substrate {e.g., PTFE-coated aluminum), as shown schematically in FIG. 13. Ink extrusion may be controlled via. fixed pressure (Nordson EFD Ultimus V pressure box), with the ozzle precisely positioned using a custom 3D positioning stage (Aerotech).
[iu6§] After printing and curing of the m formulation, two regions parallel with and adjacent to the functional region of wa e propagation may be infilled wit* epojcy (e.g., Momentiv© Epon 828) to prevent undesired structural; bending that could inhibit measurements.. The lateral distance, d, between* these longitudinal constraints or supports may be defined by acrylic braces of precise dimensions, which are made using an Epilog Laser Mini cutting s stem. The acrylic braces also serve to elevate the soft structure (via the longitudinal supports) without contacting to eliminate any interactions between the wave pulse and the table surface.
[i06S| A cylindrical copper rod $.g,t 3. 75 mm diameter) is cut to pieces (e.g., 5,1 ? mm length, giving; a mass of -0.4? gj, which can be press fit Into the printed bistable elements to enable optical tracking of portions of the architecture during wave propagation. For example, top surfaces of the copper cylinders are painted with flat white paint to m&xirnke light contrast for visualization of the transition wave propagation.
[0067] To achieve a range of effective stiffnesses I, several different
geometries are designed for the linear coupling elements that connect the individual bistable elements together. As- shown i FIG, 2C, stiffness values range from 30 to 2*100 N/m (as measured with a commercial quastsfatic test system, Instron 5586, in displacement control at a displacement rale of 2
mm min). Additional intermediate values can fee obtained by varying the translation speed of the printbead during the printing process.
0 haraste.ozgtio. . of Wave . Fro agaion
0068] To characterize the propagation of nonlinear waves experimentally, a high-speed; camera is used to track the location of ach bistable element In the series as a function of time. Because at the wavefronf the bistable elements tran ition from one stable configuration to the other, the d splacement of each unit is monitored relative to Its two stable configurations and For the unit two ced:
Figure imgf000020_0001
[00703 «, being the position of the P bistable element in the series, FIG* 14 illustrates the propagation of the nonlinear wave by showing for each unit lis
e nearest stable configuration
Figure imgf000020_0002
[ W2] at different times. If & » 0, the *¾' element ss In ether of its two stable configurations, whereas ·¾ > 0 indicates that the unit Is passing through the energy barrier separating them. The experimental data of FIG, 1 dearly show that at ie wavefront a few bistable units {in this case, about four) are
undergoing a change from one stable state to the other at any give time and that the transition sequentially propagates through the elements in the series* This transition wave is found to propagate with a constant shape, deafly indicating that both dispersive and dissipat effects are overcome in the architecture, 00733 The speed of fie nonlinear wave can he obtained by monitoring the evolution of the normalized distance a:sti; for each bist ble unit during the entire experiment:, as In IG* 15A< Because in th s contour map the dark and light regions indicate bistable units in the high-energy and iow-energ stable configurations, respectively, the sequential change of each of the elements along the chain from one stable state to the other is evident, Furthermore, the constant slope of the boundary between the pretransllon (dark) a d post-transition (light) regions reveals a constant propagation velocity (In this case, 3,4 ± 0>1 m/s). Note also that the pulse width for any time can be extracted from the ma by taking a. horizontal slice of the plot ( e,s a fixed time) and measuring the number of bistable elements in the midst of transitioning between the solid dark and solid Sight regions (approximately four elements in width). p074] Another uni ue aspect of this system is that the propagation velocity and pu!se shape are the same (w thin the margin of error) whether the wave is initiated in compression or tension, as revealed S y comparison of tri contour plots reported in FIG, 15 A. (for compression) and Fie, 158 (for tension}.,, in both cases, the transition wave propagates with a constant velocity (3,4 m s In this example) and pulse wtdlh (approximately four elements). The propagation: of rarefaction pulses Is rare find and thus a noteworthy feature of this system. Finally, It is noted1 that a wave can be initiated at any intermediate location in the series., in which case a compressive pulse travels in one direction d:
rarefaction pulse travels in the other direction, both propagating outward from the point of initiation.. FIGs. ISC and 5D show optical images obtained during wave propagation from a high-speed camera* corresponding to the data in FIOs. 15A and 158, respectively,
[0075J Transition wave propagation is also characterized using a 1D mechanical model, in which the position of the middle of the - bistable element
$0 SJ
Figure imgf000021_0001
(0077J where F is the quasi- 1 D on-site potential of each bistable element, γ is a linear damping parameter, and k is the coupling element (&.,g., spring) stiffness. The linear damping model is a leading-order approximation to the complex dsss!paflve nature of elastomers. The bistable potential V is numerically computed by nonlinear flnite-eiernent simulations of a qyasisfaticsl!y deforming, co- rofafional, linear elastic beam; In 2D, The numerical force-displacement curves are validated tsy comparison with the experimental data shown in FIG, 3, To simulate the response of the system under iarge÷ampiitude excitations, initially, all nodes are placed in the high-energ configuration.- The first node is then excited by displacing: it from the high-energy stable point to the low-energy one, and the system response In time Is solved using a Newmark-β scheme.. The only unknown model parameter, γ, is determined by fling experimental wave speed data for a particular combination of geometric parameters (k 80 Him and ά ~ 17.5 mm). With all model parameters thereby determined,, architectures with different combinations of geometric parameters c n he examined'. As an example, FIGs. 15E and 1SF show simulated compression-initiated and tension- initiated pulses, respectively, which show excellent agreement with the
experimental data discussed earlier in regard to FK3s> 15A and 15Β»
£00783 Using values obtained for the o -site potential !¾i, as shown in FIG, 48, simulations are performed to predict the wave characteristics for different coupling element stiffnesses, &, and ©ncMo-end distances, d The wave speed, which is computed by tracking the point of maximum particle velocity, increases monotonically with increasing ts shown in FIG,. SA, However, the effect of d on the wave velocity is more complicated. The wave velocity Is highly sensitive to changes In when d Is small but much less sensitive when is large. The associated width of the transition wave is also noted.,, defined as the number of nodes that simyiteneousiy have displacements between 10% and 90% of the transition displacement. The results reported in Fig. SB indicate that the pulse width increases with Increasing k, showing the same trend as t.he velocity. For constant coupling element stiffness value ks d does not have an effect on the pulse width fo lower stiffnesses but shows a similar variation as the velocity for higher stiffnesses. Experimental measurements of architectures wi h different values of d and k match these numerical results with excellent quantitative agreement, confirming the validity of our simulations.
[0079J The trends for velocity (FIG. 5A) and pulse width (FIG. 58) contours show a correlation with the energy barrier for different d values, as shown in FIG, 48, For a constant coupling element stiffness, the d values corresponding to high-energy barriers show lower velocity and width. This Is because when the energy barrier is high, each element need to absorb more energ to overcome the barrier, thereby causing a slower transition: rate and therefore a. lower wave speed and vice versa, Consequently, the energy barrier appears to be the most important criterion in determining the transition speed and width of the
displacement profile. £0080 Because tie N bistable elements that constitute a particular pulse are not simultaneously in morphologies that place them in the peak of their Individual energy barriers, the total pulse energy barrier, Ews is calculated as
Figure imgf000023_0001
[00821 where V and N are determined from the simulation results (FIGs. 48 and FIG. SB, respectively) and the .¾ values are a proximated by c islrlb ing them equally between and x5^ FIG, SC shows fie total potential energy barrier (Em), associated with: the tr nsition events of the individual bistable elements from their higher-energy slate (¾ - .¾ά to their Sower-energy stale {x ~ xe1). As expected, as the number of elements in the pulse (N) and the energy barrier for the Individual eiemeiits Increase, so does the total energy barrier required to Initiate tie pulse along a given portion of the series (or chain) because the tot l energy barrier is the sum of the transient barriers of the individual elements undergoing transition at a given time,
0 831 Although the present invention has bee described i considerable detail with reference to certain embodiments theieof, otser embodiments are possible without departing from the present invention. The spirit and scop© of the appended claims should not be limited, therefore, to the description of th preferred embodiments contained herein. Ail embodiments that come within the meaning of the claims, either literally or by equivalence, are Intended to be embr ced: therein. Furthermore, the advantages described above are not necessarily the on y advantages of the invention, and It Is not necessarily expected that all of the described advantages i! be achieved with every embodiment of the invention.

Claims

1 ,. An architecture for achieving stable wave propagation through a sof material the architecture comprising;
a plurality of bistable elements arranged in series, each bistable element comprising a soft material and having two stable configurations, a higher energy configuration and a lower energy onfiguration:,
wherein the bistable elements are configured to snap from the higher energy configuration; ID the tower energy conflgu ation sequentially when stimulated by mechanical wave, thereby allowing the mechanical wave to propagat therethrough,
2, The architecture of data 1 , wherein the soft material comprises an eSastorneric material,
3, The architecture of claim 1 or 2, wherein the soft material comprises a smart material.
4, The architecture of any one of claims 1 -3, wherein adjacent bistable elements am coupled together by a physical connection or by a force field..
5,. The architecture of claim 4:( wherein coupling elements extend between and physically connect adjacent bistable elements,
8., The arch!tectuf© of claim S, wherein the coupling elements comprise the soft materi l,
?., The architecture of claim 5 or 8, wherein th coupling elements exhibit: a linear relationship between applied force and displacement, the coupling elements having a stiffness
8, The architecture of claim 7, wherein the stiffness £ is in the range from about 30 Him to about 2100 Him,
9. The architecture of any one of claims 1 -8, wherein at: feast one portion of the bistable element is constrained from motion and an unconstrained portion of the bistable e ement is free to sna from the higher en rgy
configuration to the lower energy configuration when stimulated by the
mechanical rave,
10. The architecture of arty one of claims 1 ~ „ wherein each bistable element comprises first beam portion attached to a second beam portion at a junction* the junction being in a midportion of the bistable element.
11. The architecture of claim 10, wherein the bistable elements ar arranged in series along a longitudinal axis, and
wherein, in the lower energy configuration , the first and second beam portions are substantially straight and have opposing tilts with respect to the iongftuidinai axis.
12. The architecture of claim 10 or 11 , wherein, in the higher energy configuration, the first and second beam potions comprise a deformed geometr capable of storing energy,
13. The architecture of any one of claims 1-12, wherein ends of each bistable element are fixedly or translstabiy secured to constraints positioned adjacent to the plurality of bistable elements.
14. The architecture of claim: 13, wherein a distance d between the constraints is constant along the series.
15. The architecture of claim 13, wherein a distance d between the constraints is variable along the series.
16. The architecture o any one of claims 13-15, wherein the constraints are attached to or part of longitudinally oriented bam oriented substantially parallel to or nonparatlei to the longitudinal axis,
17. The architecture of any one of claims 1 »18f he ein the plurality includes at least six bistable elements.
18. The architecture of claim 1 ?< wherein the plurality Includes at feast 100 bistable elements.
19. The architecture of any one of claims 1 -18, wherein each bistable element has more than two stable eonfigy ations,
20,. The architecture of any one of claims 1-19, wherein a mechanical wave propagates through the plurality of bistable elements at a constant velocity without distortion.
21. The architecture of any one of claims 1 -20 formed: by direct Ink writing,
22. A logic device comprising the architecture of any one of claims 1 -21 ,
23. The logic device of claim 22 being selected from among a
mechanical diode and a mechanical logic gate,
24. The logic device of claim 23 further comprising:
a plurality of coupling elements, each coupling element extending between and physically connecting adjacent bistable elements, wherein: the coupling elements in a first region of the series comprise a stiffness and the coupling elements in a second region of the series comprise a stiffness &2s where &2 > the logic device being a mechanical diode.
25. A logic device comprising
a first input chain comprising a first plurality of bistable elements arranged in series;
a second input chain comprising a second plurality of bistable elements arranged in series; and
an output chain connected to the first and second input chains, the output chain comprising a third plurality of bistable elements arranged in series,
wherein each bistable element comprises a soft material and has two stable configurations, a higher energy configuration and a lower energy
configuration, the bistable elements being configured to snap from the higher energy configuration to the tower energy configuration sequentially when
stimulated by mechanical wave, thereby allowing the mechanical wave to propagat therethrough,
20, The logic device of claim 25 being selected from a mechanical AMD gate and a mechanical OR gate,
27, The logic device of claim: 25 or 28 further comprising;
a first set of constraints positioned along both sides of the first input chain adjacent to the first plurality of bistable elements;
a second set of constraints positioned along both sides of the second input chain adjacent to the second plurality of bistable elements; and
s third set of constraints positioned along both: sides of the output chain adjacent to the third plurality of bistable elements,
wherein ends of each bistable element are fixedly secured to the respective adjacent constraints, and
wherein a distance d between the first set of constraints is substantially the same as the distance d between the second set of constr ints.
28. The logic device of lai : 27, wherein a distance d ii beiween the third set of constraints la less t an the distance d, the logic device being a mechanical AND gate.
28
29. The logic device of claim 27, wherein a distance d between the third set of constraints is greater than the distance dt the logic device being a mechanical OR gate.
30,. A. method of propagating mechanical sign ls in a soft material, the method comprising;
providing a plurality of bistable elements arranged so series, each bistable element comprising a soft material and having two stable oonigurationss a higher energy configuration and; a lower energy configuration;.
stimulating a first bistable element by a mechanical w ve, the mechanical wave inducing the first bistable element to snap f om the higher to the lower energy configuration, thereby allowing f e mechanical wave to pass through the first bistable element and to stimulate an adjacent blstabie element,
wherein the stimulation of adjacent bistable elements continues until the mechanical wave has propagated through all of the plurality of blstabie elements.
31 , The method of claim 30, wherein the first bistable element is positioned at m end of the series, and the mechanical wave propagates in a slngte direction,
32.. The method of claim 30, wherein the first bistable element I
positioned at an Intermedial© location in the series, and the mechanical wave propagates in two directions.
33, The method of any one of claims 30*32, wherein adjacent bistable elements are coupled together by a physical connection or by a force field.
34. The method of any one of claims 30-33 f wherein the soft material comprises a smart, material, and
further comprising, after the mechanical wave has propagated through, exposing the plurality of bistable elements to a stimulus to activate the smart material, thereby returning e ch bistable element from the lower nerg configuration to the higher ene gy configuration.
35, A method of fabricating an architecture for achieving stable wave propagation through a soft material, the method comprising:
extruding an ink formulation from a de ositon nozzle moving relative to a substrate, the Ink formulation comprising an uncured polymer:
depositing one or more continuous filaments comprising the ink formulation In a predetermined pattern on the substrate, thereby forming an as-printed architecture comprising a plurality of printed structures arranged in series, each printed structure comprising the yncured polymer;
curing the uncured polymer* thereby forming from the printed structures a plurality of bistable elements arranged in series and comprising a soft material, eac bistable element being in a low energ configuration, and
deforming the bistable elements to have a deformed geometry, each bistable element thereby adopting a higher energ configuration,
wherein the bistable elements are configured to snap from the higher energy configuration to the low enenjy configuration sequentially when stimulated by a mechanical wave, thereb allowing; the mechanical wave to propagate therethrough;.
PCT/US2016/058639 2015-10-26 2016-10-25 Architecture for achieving stable wave propagation through a soft material WO2017074925A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201562246433P 2015-10-26 2015-10-26
US62/246,433 2015-10-26

Publications (1)

Publication Number Publication Date
WO2017074925A1 true WO2017074925A1 (en) 2017-05-04

Family

ID=58631832

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2016/058639 WO2017074925A1 (en) 2015-10-26 2016-10-25 Architecture for achieving stable wave propagation through a soft material

Country Status (1)

Country Link
WO (1) WO2017074925A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180248552A1 (en) * 2017-02-28 2018-08-30 Lawrence Livermore National Security, Llc System and method for flexure based microstructural logic gates
WO2022250768A1 (en) * 2021-05-26 2022-12-01 Lawrence Livermore National Security, Llc System and method for micromechanical logical and gate
US11530621B2 (en) 2019-10-16 2022-12-20 General Electric Company Systems and method for use in servicing a machine

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6774391B1 (en) * 1999-10-25 2004-08-10 Cambridge University Technical Svcs. Magnetic logic element
US20100171393A1 (en) * 2008-12-10 2010-07-08 The Regents Of The University Of California Bistable electroactive polymers

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6774391B1 (en) * 1999-10-25 2004-08-10 Cambridge University Technical Svcs. Magnetic logic element
US20100171393A1 (en) * 2008-12-10 2010-07-08 The Regents Of The University Of California Bistable electroactive polymers

Non-Patent Citations (5)

* Cited by examiner, † Cited by third party
Title
GERSON ET AL.: "Design considerations of a large-displacement multistable micro actuator with serially connected bistable elements", FINITE ELEMENTS IN ANALYSIS AND DESIGN, vol. 49, no. 1, 23 September 2011 (2011-09-23), pages 58 - 69, XP028109000 *
NADKARNI ET AL.: "Dynamics of periodic mechanical structures containing bistable elastic elements: From elastic to solitary wave propagation", PHYSICAL REVIEW E, vol. 90, no. 2, 22 August 2014 (2014-08-22), pages 1 - 13, XP055379398 *
RANEY ET AL.: "Stable propagation of mechanical signals in soft media using stored elastic energy", PROCEEDINGS OF THE NATIONAL ACADEMY OF SCIENCES OF THE UNITED STATES OF AMERICA (PN AS, vol. 113, no. 35, 30 August 2016 (2016-08-30), pages 9722 - 9727, XP055379395 *
SHAN ET AL.: "Multistable Architected Materials for Trapping Elastic Strain Energy", ADVANCED MATERIALS, vol. 27, no. 29, 5 August 2015 (2015-08-05), pages 4296 - 4301, XP055379400 *
XIN ET AL.: "Tensional acoustomechanical soft metamaterials", SCIENTIFIC REPORTS, vol. 6, no. 1, 6 June 2016 (2016-06-06), pages 1 - 7, XP055379396 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180248552A1 (en) * 2017-02-28 2018-08-30 Lawrence Livermore National Security, Llc System and method for flexure based microstructural logic gates
US10122365B2 (en) * 2017-02-28 2018-11-06 Lawrence Livermore National Security, Llc System and method for flexure based microstructural logic gates
US11530621B2 (en) 2019-10-16 2022-12-20 General Electric Company Systems and method for use in servicing a machine
WO2022250768A1 (en) * 2021-05-26 2022-12-01 Lawrence Livermore National Security, Llc System and method for micromechanical logical and gate
US11604489B2 (en) 2021-05-26 2023-03-14 Lawrence Livermore National Security, Llc System and method for micromechanical logical and gate

Similar Documents

Publication Publication Date Title
WO2017074925A1 (en) Architecture for achieving stable wave propagation through a soft material
US8315499B1 (en) Functionally-graded three-dimensional ordered open-cellular microstructure and method of making same
Florian et al. Direct laser printing of tailored polymeric microlenses
Park et al. Mechanically tunable photonic crystal structure
Gruene et al. Dispensing pico to nanolitre of a natural hydrogel by laser-assisted bioprinting
Bae et al. High-performance PVC gel for adaptive micro-lenses with variable focal length
CN106324728B (en) Method and apparatus for reducing the fuel factor in compact adjustable optical lens
AU2018352982A1 (en) Methods and apparatuses for casting polymer products
KR20130060314A (en) Large area induced assembly of nanostructures
KR102341043B1 (en) Flexible liquid crystal cells and lenses
Xu et al. Fabrication of polymer microlens array with controllable focal length by modifying surface wettability
EP1843178A1 (en) Process for producing optical waveguide
CN110445534A (en) A kind of method, system and equipment that multi-core optical fiber crossfire value determines
Hsiao et al. Single-digit-micrometer-resolution continuous liquid interface production
KR100717851B1 (en) Microlens Array Sheet using MEMS and Manufacturing Method thereof
Dingeldein et al. Process characterization for direct dispense fabrication of polymer optical multi-mode waveguides
KR100955011B1 (en) Method of manufacturing an optical device by means of a replication method
DK103888A (en) extruder
US10795136B2 (en) Wafer level lens stack, optical system, electronic device and method
Yi et al. Fabricating method of SU-8 photoresist conical nozzle for inkjet printhead
De Pasquale et al. Experimental evaluation of mechanical properties repeatability of SLA polymers for labs-on-chip and bio-MEMS
JP2017516162A (en) Production of optical elements by duplication and corresponding duplication tools and optical devices
KR102337213B1 (en) Construction of Optical Layers with Imprint Lithography Process
US20200376720A1 (en) Method for producing mold, and method for producing molded article using same
US7136560B2 (en) Method of controlling optical characteristic of optical element and optical device

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 16860611

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 16860611

Country of ref document: EP

Kind code of ref document: A1