The present invention relates to structural connectors and methods of reinforcing connection between structural members, and more particularly, to structural connectors adapted for use with and methods of interconnecting a structural member comprising an shape memory wire.
Active material elements are conventionally utilized to effect reconfiguration and/or bias variance in structural assemblies, actuators or smart devices, when activated or deactivated. For example, shape memory alloy (SMA) wires are often used to transfer loads between and cause the displacements of structural members, upon activation. That is to say, once thermally activated, the crystal structure of the alloy reconfigures and in turn causes the wire to shrink; the actuating or reconfiguring force is transferred to the coupled members solely through their connection points. In promoting this function, it is appreciated that secure methods of joining (e.g., “connecting”) these wires to the structural members play a vital role.
Among conventional methods of joining, mechanical crimping is the most widely used method. This method, however, presents various concerns in the art. For example, failure, such as wire slipping or fatigue at or adjacent the crimp is a commonly experienced mal condition. Such failure, in turn, may cause the collapse of the assembly or early malfunction of the actuator or smart device. Of further conventional concern, the need to provide an isolated electrical connection to the wire is often made more complex by the addition of these crimps.
Thus, for these reasons and more, there remains a need in the art for an improved method of joining active material elements, such as a shape memory wire, to structural members that increases structural capacity, reduces the likelihood of premature failure, and enables isolated electrical connection where needed.
The present invention concerns plural embodiments of an assembly (e.g., “link”) for and method of joining an active material element to structural members that addresses the afore-mentioned concerns. The inventive assembly is robust enough to avoid failure, while providing a cost effective and readily implemented solution. In general, the invention utilizes a reinforcing connector attached to the active material element, and various connector/element configurations that cooperatively increase the capacity of the structure.
It is an object of the invention to provide an active assembly, adapted for use in a structure including at least one structural member. In addition to being able to effect a reconfiguration of or biasing force in the structure, the assembly is capable of sustaining a load over a predetermined period not previously sustainable by the prior art.
The assembly generally includes at least one element formed at least in part of an active material operable to change a first condition in response to an activation signal; and at least one reinforcing connector securely fixed to the element. The connector presents an interconnecting portion configured to enable interconnection between the active assembly and said at least one member.
Other aspects and advantages of the present invention, including the employment of at least one shape memory allow wire as the active material element, and connectors comprising ring terminals, metal tubing/shims, and other configurations will be apparent from the following detailed description of the preferred embodiment(s) and the accompanying drawing figures.
A preferred embodiment(s) of the invention is described in detail below with reference to the attached drawing figures, wherein:
a is an elevational view of the structure shown in
a is a perspective view of the assembly shown in
a is a side elevation view of the assembly shown in
a is an elevation view of the assembly shown in
a is a cross-section of the assembly shown in
a is an elevational view of the assembly shown in
The present disclosure concerns a structure 10 comprising at least one structural member 12 and an inventive active material assembly 14 that forms a link or joint in the structure 10. As used herein the term “structure” shall mean an interconnected multi-part embodiment whose function includes generating, transferring or sustaining a load across the link, and shall include active material actuators and smart devices. The inventive assembly 14 is generally configured to increase the structural capacity of the joints cooperatively formed with adjacent members 12, and to that end, includes at least one reinforcing connector 16. The connector 16 is configured to withstand a predetermined load over a period without failure. As such, the connector 16 is formed of material having sufficient tensile strength (e.g., aluminum) to sustain the load.
a, for example, shows a conventional scissor lift structure 10 having a fixed and free end, and comprising a plurality of members 12 pivotably connected at their ends and midpoints. The lift 10 incorporates an active material assembly (e.g., “actuator”) 14 configured to cause the upper end to collapse and descend upon activation. In such structures, it is appreciated that where latching is not provided a tensile load is experienced across the link, even after reconfiguration. An activation signal source 18 is operably coupled to the actuator 14 and configured to selectively (e.g., manually or in response to sensory technology) generate an activation signal. As appreciated by those of ordinary skill in the art, the activation signal may be thermal, magnetic, electrical, chemical, and/or other like activation signal or a combination of activation signals. The source 18 in
More particularly, the source 18 is coupled to an active material element 24 comprising the assembly or actuator 14, and may be directly or indirectly operable. With respect to the later, and as shown in
In response to the activation signal, the active material element 24 changes at least one attribute of the structure 10, and preferably reverts back to the original state of the at least one attribute upon discontinuation of the signal; or, for the classes of active materials that do not automatically revert upon discontinuation of the activation signal, alternative means can be employed to revert the active material to its original state as will be discussed in detail herein.
1. Active Material Description and Function
As used herein the term “active material” shall be afforded its ordinary meaning as understood by those of ordinary skill in the art, and includes any material or composite that exhibits a reversible change in a fundamental (e.g., chemical or intrinsic physical) property, when exposed to an external signal source. Thus, active materials shall include those compositions that can exhibit a change in stiffness properties, shape and/or dimensions in response to the activation signal, which can take the type for different active materials, of electrical, magnetic, thermal and like fields.
Preferred active materials for use with the present invention include but are not limited to the classes of shape memory materials, and combinations thereof. Shape memory materials generally refer to materials or compositions that have the ability to remember their original at least one attribute such as shape, which can subsequently be recalled by applying an external stimulus, as will be discussed in detail herein. As such, deformation from the original shape is a temporary condition. In this manner, shape memory materials can change to the trained shape in response to an activation signal. Exemplary shape memory materials include shape memory alloys (SMA), shape memory polymers (SMP), shape memory ceramics, electroactive polymers (EAP), ferromagnetic SMAs, dielectric elastomers, ionic polymer metal composites (IPMC), piezoelectric polymers, piezoelectric ceramics, various combinations of the foregoing materials, and the like.
Shape memory alloys (SMA's) generally refer to a group of metallic materials that demonstrate the ability to return to some previously defined shape or size when subjected to an appropriate thermal stimulus. Shape memory alloys are capable of undergoing phase transitions in which their yield strength, stiffness, dimension and/or shape are altered as a function of temperature. The term “yield strength” refers to the stress at which a material exhibits a specified deviation from proportionality of stress and strain. Generally, in the low temperature, or martensite phase, shape memory alloys can be plastically deformed and upon exposure to some higher temperature will transform to an austenite phase, or parent phase, returning to their shape prior to the deformation. Materials that exhibit this shape memory effect only upon heating are referred to as having one-way shape memory. Those materials that also exhibit shape memory upon re-cooling are referred to as having two-way shape memory behavior.
Shape memory alloys exist in several different temperature-dependent phases. The most commonly utilized of these phases are the so-called martensite and austenite phases discussed above. In the following discussion, the martensite phase generally refers to the more deformable, lower temperature phase whereas the austenite phase generally refers to the more rigid, higher temperature phase. When the shape memory alloy is in the martensite phase and is heated, it begins to change into the austenite phase. The temperature at which this phenomenon starts is often referred to as austenite start temperature (As). The temperature at which this phenomenon is complete is called the austenite finish temperature (Af). When the shape memory alloy is in the austenite phase and is cooled, it begins to change into the martensite phase, and the temperature at which this phenomenon starts is referred to as the martensite start temperature (Ms). The temperature at which austenite finishes transforming to martensite is called the martensite finish temperature (Mf). Generally, the shape memory alloys are softer and more easily deformable in their martensitic phase and are harder, stiffer, and/or more rigid in the austenitic phase. In view of the foregoing, a suitable activation signal for use with shape memory alloys is a thermal activation signal having a magnitude to cause transformations between the martensite and austenite phases.
Shape memory alloys can exhibit a one-way shape memory effect, an intrinsic two-way effect, or an extrinsic two-way shape memory effect depending on the alloy composition and processing history. Annealed shape memory alloys typically only exhibit the one-way shape memory effect. Sufficient heating subsequent to low-temperature deformation of the shape memory material will induce the martensite to austenite type transition, and the material will recover the original, annealed shape. Hence, one-way shape memory effects are only observed upon heating. Active materials comprising shape memory alloy compositions that exhibit one-way memory effects do not automatically reform, and will likely require an external mechanical force to reform the shape that was previously suitable for airflow control.
Intrinsic and extrinsic two-way shape memory materials are characterized by a shape transition both upon heating from the martensite phase to the austenite phase, as well as an additional shape transition upon cooling from the austenite phase back to the martensite phase. Active materials that exhibit an intrinsic shape memory effect are fabricated from a shape memory alloy composition that will cause the active materials to automatically reform themselves as a result of the above noted phase transformations. Intrinsic two-way shape memory behavior must be induced in the shape memory material through processing. Such procedures include extreme deformation of the material while in the martensite phase, heating-cooling under constraint or load, or surface modification such as laser annealing, polishing, or shot-peening. Once the material has been trained to exhibit the two-way shape memory effect, the shape change between the low and high temperature states is generally reversible and persists through a high number of thermal cycles. In contrast, active materials that exhibit the extrinsic two-way shape memory effects are composite or multi-component materials that combine a shape memory alloy composition that exhibits a one-way effect with another element that provides a restoring force to reform the original shape.
The temperature at which the shape memory alloy remembers its high temperature form when heated can be adjusted by slight changes in the composition of the alloy and through heat treatment. In nickel-titanium shape memory alloys, for instance, it can be changed from above about 100° C. to below about −100° C. The shape recovery process occurs over a range of just a few degrees and the start or finish of the transformation can be controlled to within a degree or two depending on the desired application and alloy composition. The mechanical properties of the shape memory alloy vary greatly over the temperature range spanning their transformation, typically providing the airflow control devices with shape memory effects, superelastic effects, and high damping capacity.
Suitable shape memory alloy materials include, without limitation, nickel-titanium based alloys, indium-titanium based alloys, nickel-aluminum based alloys, nickel-gallium based alloys, copper based alloys (e.g., copper-zinc alloys, copper-aluminum alloys, copper-gold, and copper-tin alloys), gold-cadmium based alloys, silver-cadmium based alloys, indium-cadmium based alloys, manganese-copper based alloys, iron-platinum based alloys, iron-platinum based alloys, iron-palladium based alloys, and the like. The alloys can be binary, ternary, or any higher order so long as the alloy composition exhibits a shape memory effect, e.g., change in shape orientation, damping capacity, and the like. For example, a nickel-titanium based alloy is commercially available under the trademark NITINOL from Shape Memory Applications, Inc.
Shape memory polymers (SMP's) are known in the art and generally refer to a group of polymeric materials that demonstrate the ability to return to some previously defined shape when subjected to an appropriate thermal stimulus. Shape memory polymers are capable of undergoing phase transitions in which their shape is altered as a function of temperature. Generally, SMP's have two main segments, a hard segment and a soft segment. The previously defined or permanent shape can be set by melting or processing the polymer at a temperature higher than the highest thermal transition followed by cooling below that thermal transition temperature. The highest thermal transition is usually the glass transition temperature (Tg) or melting point of the hard segment. A temporary shape can be set by heating the material to a temperature higher than the Tg or the transition temperature of the soft segment, but lower than the Tg or melting point of the hard segment. The temporary shape is set while processing the material at the transition temperature of the soft segment followed by cooling to fix the shape. The material can be reverted back to the permanent shape by heating the material above the transition temperature of the soft segment.
The temperature needed for permanent shape recovery can be set at any temperature between about −63° C. and about 120° C. or above. Engineering the composition and structure of the polymer itself can allow for the choice of a particular temperature for a desired application. A preferred temperature for shape recovery is greater than or equal to about −30° C., more preferably greater than or equal to about 0° C., and most preferably a temperature greater than or equal to about 50° C. Also, a preferred temperature for shape recovery is less than or equal to about 120° C., and most preferably less than or equal to about 120° C. and greater than or equal to about 80° C.
Suitable shape memory polymers include thermoplastics, thermosets, interpenetrating networks, semi-interpenetrating networks, or mixed networks. The polymers can be a single polymer or a blend of polymers. The polymers can be linear or branched thermoplastic elastomers with side chains or dendritic structural elements. Suitable polymer components to form a shape memory polymer include, but are not limited to, polyphosphazenes, poly(vinyl alcohols), polyamides, polyester amides, poly(amino acid)s, polyanhydrides, polycarbonates, polyacrylates, polyalkylenes, polyacrylamides, polyalkylene glycols, polyalkylene oxides, polyalkylene terephthalates, polyortho esters, polyvinyl ethers, polyvinyl esters, polyvinyl halides, polyesters, polylactides, polyglycolides, polysiloxanes, polyurethanes, polyethers, polyether amides, polyether esters, and copolymers thereof. Examples of suitable polyacrylates include poly(methyl methacrylate), poly(ethyl methacrylate), ply(butyl methacrylate), poly(isobutyl methacrylate), poly(hexyl methacrylate), poly(isodecyl methacrylate), poly(lauryl methacrylate), poly(phenyl methacrylate), poly(methyl acrylate), poly(isopropyl acrylate), poly(isobutyl acrylate) and poly(octadecyl acrylate). Examples of other suitable polymers include polystyrene, polypropylene, polyvinyl phenol, polyvinylpyrrolidone, chlorinated polybutylene, poly(octadecyl vinyl ether) ethylene vinyl acetate, polyethylene, poly(ethylene oxide)-poly(ethylene terephthalate), polyethylene/nylon (graft copolymer), polycaprolactones-polyamide (block copolymer), poly(caprolactone) dimethacrylate-n-butyl acrylate, poly(norbornyl-polyhedral oligomeric silsequioxane), polyvinylchloride, urethane/butadiene copolymers, polyurethane block copolymers, styrene-butadiene-styrene block copolymers, and the like.
H. Exemplary Systems and Methods
Referring now to
In
The crimp 26 includes a fastening section 28 configured to facilitate removable interconnection (i.e., facile or manual connection and disconnection) between the active material assembly 14 and adjacent structural members 12. More particularly, in this configuration, a flat “O”-shaped section 28 is provided and configured to receive a fastener (not shown), as is known in the art. Opposite the fastening section 28, the crimp 26 presents an engaging section 30, which consists essentially of two wings 32 that are folded over when “crimped,” so as to define an interior connector space 34 and compress a distal section of the wire 24 extending within the space 34. As is known in the art, the crimp 26 adds mechanical strength and stress relief to the active material wire 24. It can also be made of insulative materials, so as to provide electrical isolation from nearby metal surfaces. As shown in the plural illustrations, the crimps 26 may interconnect one or more wires, as desired.
In
In operation, when the outer wall 38 of the crimp 26 is compressed, they engage the individual tubes 42, which are caused to also flatten and compress the wires 24. Increased frictional hold strength results between the tubes 42 and the connector 16 due to the greater surface area of engagement and a higher static friction provided in part by the individual tube material in comparison to the wire 24. It is appreciated that a small degree of metallurgical bonding also results from compressing the outer and individual tube materials together. As shown in
In
In another embodiment shown in
In
Other variants can be derived from this general concept as well. For example, it is appreciated that a single wire 24 looping through a pair of metal tubes 56. The wires 24 can be joined at the bent point or other locations using a conventional method of joining, such as welding. Alternatively, it is appreciated that the external ring terminal crimp 26 may be omitted, where an interior tube is flattened and bent; for example, at least one wire 24 may be received by opposite tubes 56 (
The interior metal tubes 56 and/or crimp 26 may be formed of insulative materials so that the wires 24 are electrically isolated from the crimp 26. The lead wires 22 connecting to electrodes can also be crimped together with the wires 24 within the flattened metal tube 56 or inserted into the crimp 26 and flattened. The wires 24 may run continuously or discontinuously.
It is also within the ambit of the present invention to increase friction by introducing longitudinal waves in the wire 24. For example,
In a preferred embodiment, the connector 16 is configured to provide self-locking capabilities, wherein increased tensile load within the wire 24 results in a greater hold force being applied.
In
It is appreciated that a variation in the coefficient of friction (e.g., due to exposure to oil, water, etc.) and finite flexibility of the housing 66 may lead to loosening of the grip especially when the wire 24 is repeatedly cycled, so as to lead to repeated variations in the wire tension. The finite stiffness of the housing 66 implies that the clamping stress on the wires 24 varies along the engaging surface defined by the wire 24 and wedge 68; it is highest at the base of housing 66, where housing 66 is the stiffest, and lowest near the top of housing 66, where the stiffness of housing 66 is least. This leads to a stress concentration at the base of housing 66. Finally, it is noted that the non-positive locking provided by the wedge 68, may cause non-repeatability in the end positions of the wire 24 as it is cycled. These concerns are addressed in the slotted wedge-action grip shown in
The slots allow the wedge 68 to flex as it is driven downward. The width, length and spacing of the slots can be selected to ensure generally uniform clamping pressure on the wire 24 at the engagement surface for the anticipatory pressure distribution obtained on the wedge surface when the wedge 68 is pushed into housing 66. One or more slots 72 corresponding to different wire diameters or limit loads in an application may be provided at the top and base of housing 66 to provide a positive restraint against overload on the wire 24 and to ensure repeatability of the wire end-position when used in conjunction with locking rings (not shown). Finally, it is appreciated through-out the embodiments that all exterior corners/edges are preferably rounded or otherwise relieved.
In another embodiment, a pair of off-centered identical gears (or cams) 74 provides a self-locking mechanism (
It is appreciated that the more force applied to the wire 24, the greater the normal pressure applied by the teeth against the wire 24, and that the pressure, teeth design and roughness of the wire 24 cooperatively determine the holding strength of the gears 74. It is also appreciated that the gears 74 must be driven over center in order to maintain the lock after a tensile load is ceased; else the wire 24 will be released when the force is released. Finally, the gears 74 may be the primary mechanism or can also serve as a backup grip.
Yet another embodiment is illustrated in
In operation, feeding the wire 24 top-down into the crimp 26 causes it to engage the shoe 80. As the wire 24 is pulled through, the oppositely engaging shoes 80 grab the wire 24 and the arms 78 are caused to deflect by the force on the shoes 80, which ensures a generally uniform stress distribution. The geometry of arms 78 and the shape of shoes 80 are selected to minimize stress concentration in the clamped wire 24.
Once the wire 24 has been grasped with the desired force, dimples 82 are embossed in the crimp 26 such that they protrude into the frame 76 area and provide positive constraint that holds the arms 78 in the final position. Depending on the desired limiting force in the application and/or the wire diameter the location of dimples 82 relative to frame 76 may be varied. This provides a one-way restraint against joint loosening. Thus, if the wire 24 experiences higher forces, the clamping force will also increase. Alternatively, other geometry may be presented by the arms 78 that causes the clamping force to be reduced or even saturate towards a limiting value that prevents damaging the wire in the joint, if the force in the wire increases beyond a set limit.
Other methods of reinforcing structural capacity of active material assemblies 14 include wrapping bare shape memory wires 24 or shape memory wires 24 in thin metal tubes together using a hose fastener, or through mechanical bending, and using shrink fitting and variable crimping strength along the length of the wire 24. With respect to shrink fitting, for example,
In some cases it can be advantageous for the tightness of the crimp 26 to vary over its length (
Another selectively advantageous approach is to have the end attachment fixed to the structure 10. In this case, however, any misalignment of the attachment with respect to the orientation of the wire/direction of the actuation force will lead to a kinking of/stress concentration in the wire 24 as it exits from the connector 16. Here, it is appreciated that providing a compliant element 86 (
As shown in
Lastly,
This invention has been described with reference to exemplary embodiments; it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to a particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.