Shape memory is the ability of a material to remember its original shape after mechanical deformation. As illustrated in example
These properties of shape memory materials have applications in aerospace technologies, automotive technologies, electronics, entertainment, and any other applications where repeatable shape changing is a desired feature. For example, in satellites, shape memory materials may be used to inflate a relatively large antenna in space that is stored in a relatively small protected compartment in the satellite during launch and orbiting of the satellite, with repeatable and dependable deployment.
In shape memory applications, shape memory material should be heated in an effective and efficient manner. As illustrated in example
Accordingly, damaged electrodes 4 and 5 illustrated in example
Embodiments relate to an apparatus (e.g. a shape memory device) that includes a nano-particle layer, a linking agent layer, and a shape memory layer. An electrode for heating shape memory material during shape transitions of the shape memory layer may include the nano-particle layer and the linking agent layer. The nano-particle layer may include conductive nano-size particles (e.g. gold clusters having a diameter less than 1000 nanometers or less than 50 nanometers). The electrode may be substantially resilient to deformation of the shape memory material due to individual bonding of individual particles of the nano-particle layer to the shape memory layer and/or the linking agent layer.
In embodiments, since the conductive material of an electrode is nano-size conductive particles (e.g. nano-size gold clusters) that are independently bonded to the deformable shape memory layer (and/or linking agent layer), the electrode will not substantially deteriorate due to strain of the shape memory layer. In other words, the conductive particles (e.g. nano-size gold clusters) of the nano-particle layer may strain with the shape memory layer. In embodiments, although the conductive nano-particles may be electrically coupled to each other (i.e. electrical current can flow between the conductive particles), they are not structurally bonded to each, but rather the conductive nano-particles are bonded to the shape memory layer (and/or linking agent layer). Since the conductive nano-particles are not bonding to each other, when the nano-particle layer is strained with the shape memory layer, the conductive nano-particles remain structurally stable, thus substantially avoiding crack or delamination or other structural deterioration.
In many applications (e.g. satellite technologies), embodiments will result in dependable shape memory materials. For example, in satellites, shape memory materials may be used to inflate a relatively large antenna in space that is stored in a relatively small protected compartment in the satellite during launch and orbiting of the satellite, with repeatable and dependable deployment that are not compromised by deteriorating electrodes.
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First nano-particle material layer 14 includes nanoparticles 22. In embodiments, nano-particles 22 may be conductive nano-particles (e.g. nano-size gold clusters). Nano-particles 22 may be individually bonded to first linking agent material layer 16. Bonding of nano-particles 22 to first linking agent material layer 16 may be either electrostatic bonding and/or covalent bonding. Nano-particles 22 may not be substantially bonded to each other. Accordingly, as first linking agent material layer 16 expands or contracts, the bond between the nano-particles 22 and first linking agent material layer 16 is not significantly compromised.
As illustrated in example
Although nano-particles 22 in first nano-particle material layer 14 are not bonded to each other, nano-particles 22 may be arranged close enough to each other, such that they may be electrically coupled to each other. In other words, in embodiments, electrical current may flow between adjacent nano-particles 22 in first nano-particle material layer 14. In fact, in embodiments, the rate of electrical conduction (i.e. electrical resistance) in first nano-particle material layer 14 (e.g. including gold nano-clusters) may be comparable and/or exceed that of solid gold (due to lattice inefficiencies in solid gold). Although straining or stretching of first linking material layer 16 may reduce the resistance of first nano-particle material layer 14 (due to an increase in distance between neighboring nano-particles 22), first nano-particle material layer 14 may remain conductive even when stressed or strained.
Second linking agent material layer 12 may also be bonded to first nano-particle material layer 14, with the same or similar bonding mechanism as the bonding between first nano-particle material layer 14 and first linking agent material layer 16, in accordance with embodiments. In embodiments, first linking agent material layer 16 and second linking agent material layer 12 may include the same material and/or configuration. In embodiments, first linking agent material layer 16 and second linking agent material layer 12 may include different materials and/or configurations.
Second nano-particle material layer 10 may be bonded to second linking agent material layer 12 with the same or similar bonding mechanism as the bonding between first nano-particle material layer 14 and first linking agent layer 16. Additional linking agent material layer(s) and/or nano-particle material layer(s) may be formed over second nano-particle material layer 10, in accordance with embodiments. In embodiments, first nano-particle material layer 14 and second nano-particle material layer 10 may include the same material (i.e. nano-particles 20 and nano-particles 22 may be the same type of nano-particles) and/or configuration. In embodiments, first nano-particle material layer 14 and second nano-particle material layer 10 may include different materials (i.e. nano-particles 20 and nano-particles 22 may be different types of nano-particles) and/or configurations.
As illustrated in example
In embodiments, a shape memory material layer and linking agent material layer(s) may have the same, similar, and/or compatible elastic properties. In other words, when shape memory material layer is deformed through stress or straining, the elasticity of linking agent material layer(s) may not prevent a shape memory material layer from deforming. Since nano-particle material layer(s) include individual nano-particles that are independently bonding to an adjacent shape memory material layer(s) and/or linking agent material layer(s), nano-particle material layer(s) may not prevent a shape memory material from deforming, in accordance with embodiments. Further, during deformation of a shape memory material layer, nano-particle material layers may not be subjected to significant mechanical strain, since there is substantially no bonding between adjacent nano-particles in the nano-particle material layer(s), in accordance with embodiments.
Nano-particles (e.g. nano-particles 20, nano-particles 22, and/or nano-particles 24) may be formed through a self-assembly, in accordance with embodiments. U.S. patent application Ser. No. 10/774,683 (filed Feb. 10, 2004 and titled “RAPIDLY SELF-ASSEMBLED THIN FILMS AND FUNCTIONAL DECALS”) is hereby incorporated by reference in its entirety. U.S. patent application Ser. No. 10/774,683 discloses self-assembly of nano-particles, in accordance with embodiments. In embodiments, the size (i.e. diameter or substantial diameter) of the nano-particles may be less than approximately 1000 nanometer. In embodiments, the size of the nano-particles may be less than approximately 50 nanometers. In embodiments, nano-particles may be gold and/or gold clusters. However, in other embodiments, nano-particles may be other metals (e.g. silver, palladium, copper, or other similar metal) and/or metal clusters. In embodiments, nano-particles may include metals, metal oxides, inorganic materials, organic materials, and/or mixtures of different types of materials. In embodiments, nano-particles may be semiconductor materials.
Through self assembly, nano-particles may be substantially uniformally and/or spatially dispersed during deposition to form a self assembled film, in accordance with embodiments. The self assembly of nano-particles may utilize electrostatic and/or covalent bonding of the individual nano-particles to a host layer (e.g. a linking agent material layer and/or a shape memory material layer). A host layer may be polarized in order to allow for the nano-particles to bond to the host layer, in accordance with embodiments. Since the deposition of the nano-particles may be dependent on individual bonding of the nano-particles to the host layer, a nano-particle material layer may have a thickness that is approximately the diameter of the individual nano-particles. Through a self-assembly deposition method, nano-particles that do not bond to a host layer may be removed, so that a nano-particles material layer is formed that is relatively uniform in thickness and material distribution.
Linking agent material layer(s) (e.g. first linking agent material layer 16 and/or second linking agent material layer 12) may be a material that is capable of covalently and/or electrostaticly bonding to nano-particles, in accordance with embodiments. U.S. patent application Ser. No. 10/774,683 (which is incorporated by reference above) discloses examples of materials which may be included in linking agent material layer(s). Linking agent material layer(s) may include polymer material. In embodiments, the polymer material may include poly(urethane), poly(etherurethane), poly(esterurethane), poly(urethane)-co-(siloxane), poly(dimethyl-co-methylhydrido-co-3-cyanopropyl, methyl)siloxane, and/or other similar materials. Linking agent material layer(s) may include materials that are polarized, in order for bonding with nano-particles, in accordance with embodiments.
In embodiments, linking agent material layer(s) may include a flexible material, an elastic material, and/or an elastomeric polymer. Accordingly, when nano-particles are bonded to sites of material in a linking agent material layer, then the nano-particle material layer may assume the same elastic, flexible, and/or elastomeric attributes of the host linking agent material layer, in accordance with embodiments. This physical attribute may be attributed by the individual bonding of substantially each nano-particle (of a nano-particle material layer) to a site of the linking agent material layer through either covalent and/or electrostatic bonding. Accordingly, when a linking agent material layer is stretched, strained, and/or deformed, bonded nano-particles will move with sites of the linking agent material layer to which they are bonded, thus avoiding any disassociation of the nano-particles from their host during deformation.
In embodiments, shape memory material layer(s) (e.g. shape memory material layer 18) may be a material that has the ability to be deformed from its original shape, hold a new deformed shape for a predetermined period of time, and then return to its original shape again. Examples of shape memory materials are shape memory polymers and shape memory metal alloy, both which may be implemented in shape memory material layer 18, in accordance with embodiments. Shape memory polymer may be deformed from an original shape upon application of heat of the glass transition temperature (Tg). When heat above the glass transition temperature is applied, a shape memory polymer may be deformed into a new shape. If a shape memory polymer is cooled below the glass transition temperature while being deformed in the new shape, then the shape memory polymer will remain in the new shape.
For example, a shape memory polymer material may have an original shape (e.g. the shape of shape memory material layer 18 in example
Accordingly, applications of shape memory materials may extend to applications in aerospace technologies, automotive technologies, electronics, entertainment, and any other application where repeatable shape changing is a desired feature. As an example, in aerospace satellite applications, shape memory materials may be applied in deployable structures (e.g. a deployable antenna). For example, a deployable antenna formed of a flexible material may be compactly stored in a secure compartment during launching and orbiting of a satellite. Once in orbit, the antenna with shape memory materials may be deployed by application of heat (through electrodes). The shape memory material may be specifically tailored to have a glass transition temperature for specific applications. For example, in some satellite applications, the glass transition temperature may be tailored between approximately −127° C. and approximately 3° C., in accordance with embodiments. In embodiments, the glass transition temperature may be tailored to be above approximately 3° C. In embodiments, the glass transition temperature may be tailored to be below approximately −127° C. However, shape memory material may be tailored for virtually any glass transition temperature based on the application, in accordance with embodiments.
In embodiments, shape memory material may include at least one of a polysiloxane material, a polyurethane, and/or a siloxane-urethane copolymer. However, one of ordinary skill in the art would appreciate other similar materials that may be used, depending on the application, in accordance with embodiments. In embodiment, shape memory material may include at least one of fluorine, amine, thiol, phosphine, nitrile, phthalonitrile, hydroxyl, and/or a metal complexing moiety material. For example, at least one of polysiloxane, polyurethane, and or a siloxane-urethane copolymer may be fluorinated with fluorine to tailor the glass transition temperature. For example, a siloxane polymer may have a glass transition temperature of approximately −127° C. without fluorination, approximately −98° C. with a 50% mole percentage of fluorine, and −80° C. with a 100% mole percentage of fluorine, in accordance with embodiments. For example, a urethane polymer may have a glass transition temperature of approximately −75° C. without fluorination, approximately −28° C. with a 50% mole percentage of fluorine, and 3° C. with a 100% mole percentage of fluorine, in accordance with embodiments.
A glass transition temperature may be tailored by implementation of the Fox equation with the integration of two different shape memory materials. In the Fox equation,
the glass transition temperature (Tg) of a shape memory material may be calculated and/or estimated by the relationship of the mole ratio (W1) of a first shape memory material, the glass transition temperature of the first material (Tg1), the mole ratio (W2) of a second shape memory material, the glass transition temperature of the second material (Tg2).
In embodiments, shape memory material (e.g. shape memory material layer 18) may be covalently and/or electrostatically bonded to a linking agent material layer (e.g. first linking agent material layer 16 illustrated in example
Example
In embodiments, linking agent material layers (i.e. first linking agent material layer 32 and second linking agent material layer 36) may be of a flexible material (e.g. an elastomeric polymer). Accordingly, conductive fiber 30 may be formed that has relatively highly conductive attributes and substantially maintain the physical flexibility and robustness of the host fiber, in accordance with embodiments.
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Mesh 52 of fibers may have many different applications, in accordance with embodiments. Example
Although embodiments have been described herein, it should be understood that numerous other modifications and embodiments can be devised by those skilled in the art that will fall within the spirit and scope of the principles of this disclosure. More particularly, various variations and modifications are possible in the component parts and/or arrangements of the subject combination arrangement within the scope of the disclosure, the drawings and the appended claims. In addition to variations and modifications in the component parts and/or arrangements, alternative uses will also be apparent to those skilled in the art.
The present application claims priority to U.S. Provisional Patent Application No. 60/866,375 (filed Nov. 17, 2006), U.S. Provisional Patent Application No. 60/866,359 (filed Nov. 17, 2006), and U.S. Provisional Patent Application No. 60/884,529 (filed Jan. 11, 2007), which are all hereby incorporated by reference in their entireties.
Number | Date | Country | |
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60866375 | Nov 2006 | US | |
60866359 | Nov 2006 | US | |
60884529 | Jan 2007 | US |