The present invention relates to three-dimensional microstructures and methods for forming these microstructures, particularly integral microstructures having components with dimensions less than 1 mm. The three-dimensional microstructures can be formed by applying deformations and/or electroplating to form integral connections.
Rapid growth in the area of microelectromechanical systems (MEMS) has created a demand for three-dimensional micron-scale components. Building microstructures in three dimensions presents significant challenges particularly when applying conventional photolithography techniques involving substrates having inherently planar geometries. Alternatives to photolithography for fabricating three-dimensional (3-D) structures typically include (1) serial patterning, i.e., depositing a series of layers on top of each other; or (2) carving, i.e. removing material from a block-like object in a stepwise manner. Approaches to MEMS fabrication that significantly depart from conventional lithography have been successful in “writing” 3-D structures in metals and polymers in serial fashion. These techniques include: UV stereolithography, laser-assisted chemical-vapor deposition (LCVD), localized electrochemical deposition, and laser micromachining. Although these methods may provide access to 3-D structures, they are often limited in the connectivities and intricacies of the structures that can be generated.
For large structures or macrostructures, well-established techniques exist for shaping metal components, such as casting, rolling, forging, stamping, grinding, milling, and cutting. Nuts and bolts, rivets, glue, and welding join these components. Performing most of these operations on micron-scale components can, however, prove to be difficult or impossible.
Most fabrication techniques used to make components for MEMS are derived from the microelectronics industry. These techniques can be grouped broadly into the categories of silicon micromachining and through-mask plating. Silicon micromachining involves photolithography to define patterns that can be transferred into silicon, and related materials, by standard techniques. 3-D structures can be prepared by these processes only by a layer-by-layer approach. Micromachining, thus, has several disadvantages: 1) it can pattern only a limited number of materials; 2) it can only form low-aspect-ratio planar structures with geometries that are determined by the crystallinity of the material; and 3) it requires facilities that limit accessibility and are not well suited to rapid prototyping. Through mask electroplating or LIGA (Lithographie, Galvanoformung, Abformung), involves lithography to define a mold in photoresist followed by electroplating to deposit metal (usually nickel) in the mold. The use of thick resists (<200 μm) exposed by collimated synchrotron radiation makes high-aspect-ratio structures possible, but variations in the third dimension are still difficult. In one case, 3-D structures have been achieved by use of an elaborate lathe that allows exposure on all sides of a resist-coated fiber. Limited access to synchrotron radiation, however, has resulted in the development of alternative schemes for generating high-aspect ratio molds in photoresist and other materials.
One aspect of the present invention provides a method for making a three-dimensional microstructure comprising, conforming a first microstructure at a predetermined deformable portion.
Another aspect of the present invention provides a method for making a three-dimensional microstructure. The method involves deforming a microstructure at a predetermined deformable portion to provide a deformed portion. The deformed portion is then treated to form a non-deformable portion.
Another aspect of the present invention provides a method for making a three-dimensional microstructure involving providing a microstructure and deforming a portion of the microstructure in a first predetermined orientation to form a deformed portion. A deformed portion is then treated. A deformation is applied to a portion of the microstructure in a second predetermined orientation.
Another aspect of the present invention provides a method for making a microstructure having a chain-link. The method involves providing a first and a second three-dimensional substrate. A pattern is printed on the first and second substrates. The substrate is then supported adjacent the second substrate to provide a combined pattern having at least one feature resembling a link. The method further involves electroplating the supported first and second substrates followed by dissolving the first and second substrates.
Another aspect of the present invention provides a free-standing, integral three-dimensional truss.
Other advantages, novel features, and objects of the invention will become apparent from the following detailed description of the invention when considered in conjunction with the accompanying drawings, which are schematic and which are not intended to be drawn to scale. In the figures, each identical or nearly identical component that is illustrated in various figures is represented by a single numeral. For purposes of clarity, not every component is labeled in every figure, nor is every component of each embodiment of the invention shown where illustration is not necessary to allow those of ordinary skill in the art to understand the invention.
a-1c show a patterned 2-D microstructure having deformable portions that can be folded into to form a tetrahedron, including a photocopy of a photomicrograph of the tetrahedron (1c);
a-2e show a scheme for patterning a 2-D microstructure via microcontact printing;
a-3e show a scheme for patterning a 2-D microstructure via photolithography;
a-5g shows the use of two deformable portions to control the degree of bend of a cylindrical mesh, including a photocopy of a photomicrograph of the 3-D microstructure;
a-6e shows the formation of a 3-D microstructure by applying axial stress and simultaneously deforming a plurality of deformable portions, including a photocopy of a photomicrograph of the 3-D microstructure;
a-7g shows the formation of a 3-D microstructure having a chain link via two supporting substrates, including a photocopy of a photomicrograph of the 3-D microstructure;
a-8e shows the formation of a 3-D microstructure having a trefoil know via two supporting substrates, including a photocopy of a photomicrograph of the 3-D microstructure;
a-9c shows the formation of a 3-D truss having micron-scale thicknesses;
The present invention is directed to the preparation of 3-dimensional (3-D) microstructures through a variety of techniques such as soft lithography and microelectroplating. The 3-D microstructures can have very small components, i.e. in the micron-scale, while possessing stability and durability. These microstructures can be achieved without the need for tedious processes such as numerous layering steps or carving material from a solid object. Such 3-D microstructures have uses in MEMS where high-aspect ratio structures having intricate features are required. Examples of these microstructures include trusses and other open framework structures comprising slender, lightweight components which are capable of supporting objects many times its weight.
One aspect of the present invention provides a method for making a 3-dimensional microstructure. “Microstructures” as used herein, refers to a structure having at least one component with a dimension of less than about 1 mm, preferably less than about 500 μm, preferably less than about 100 μm, more preferably less than about 50 μm and even more preferably less than about 25 μm. A “component” refers to any discrete portion of the structure. For example, a ladder would have a number of components which include each rung and the two rods supporting each rung. The component can be planar, non-planar or curved. A dimension of the component can refer to at least any one of a height, width, length or diameter.
In one embodiment, a microstructure has at least about 50% of its components with at least one dimension of less than about 1 mm (i.e. microcomponents), preferably at least about 66% of its components with at least one dimension of less than about 1 mm, more preferably at least 75% of its components with at least one dimension of less than about 1 mm, more preferably at least about 90% of its components with at least one dimension of less than about 1 mm, even more preferably at least about 95% of its components with at least one dimension of less than about 1 mm, and even more preferably still at least about 99% of its components with a dimension of less than about 1 mm. In other embodiments, any of the recited percentages of components have a dimension less than any of the previously recited dimensions.
“3-dimensional microstructure” or “3-D microstructure” as used herein refers to a non-planar microstructure. A planar, or “2-D microstructure”, as used herein, refers to a structure having a substantially planar orientation with a height no more than {fraction (1/10)} of the smaller of its width or length, preferably no more than {fraction (1/25)} and more preferably no more than {fraction (1/50)}. In one embodiment, a 3-D microstructure refers to a structure having 3 dimensions in which the smallest dimension is at least {fraction (1/20)} the larger of the other two dimensions.
In one embodiment, the method for making the 3-dimensional structure comprises providing a first microstructure and deforming that microstructure at a predetermined deformable portion. The first microstructure can be a 3-D microstructure. In one embodiment, the first microstructure is a two-dimensional (2-D) microstructure which can be deformed to make the 3-D microstructure. The 2-D microstructure can be formed by conventional lithography techniques.
“Deforming” refers to controlled manipulation of at least one portion of the first microstructure, preferably a predetermined deformable portion, to achieve a predetermined orientation. Examples of deforming include bending, unbending, folding, unfolding, twisting, untwisting or the like. Deforming does not include accidental deformations, which can result in an almost infinite number of orientations.
Typically, the “deformable portion” is structurally or mechanically weaker than surrounding portions and therefore will yield to force by bending, twisting. In one embodiment, the deformable portion has dimensions that are smaller than adjacent non-deformable portions. For example, an article can have a non-deformable portion that tapers to a relatively thin dimension. Applying a force to the deformable portion will result in a high likelihood of deformation at the area of the thin dimension while maintaining the original structure and orientation of the non-deformable portion. In one embodiment, the deformable portion has a smallest dimension which is less than about 50% that of adjacent, non-deformable portions. In other embodiments, the deformable portion has a smallest dimension which is less than about 40%, 30%, 20%, 10% and even as low as 5% the smallest dimension of adjacent nondeformable portions. Generally, the deformable portions comprise a malleable material such as a ductile metal that can be bent or folded easily. Deformable portions can also be created by providing a discontinuous pattern, i.e. a dotted line comprising segments of material alternating with segments of empty space. Alternatively, the deformable portion can be created by providing it with more degrees of freedom of movement than adjacent non-deformable portions. For example, a non-deformable portion can be structurally limited to a certain configuration or point in space with respect to the structure, whereas the deformable portion can be manipulated about with relative ease.
“Predetermined” refers to the capability to achieve a desired orientation. In one embodiment, the deformable portion allows deformation to a predetermined angle. In another embodiment, the deformable portion allows deformation at a predetermined direction. In another embodiment, the deformation can occur at both a predetermined direction and a predetermined angle.
In one embodiment, the 3-D microstructure is free-standing, i.e., it can exist in its 3-D configuration without support by a substrate or other supporting structure. The free-standing microstructure can be initially constructed on a supporting substrate but is capable of being released from the substrate. In another embodiment, the free-standing 3-D microstructure can be formed from without the need of a supporting substrate.
In one embodiment, the present invention features a 3-D microstructure having at least one microcomponent (having the micro-dimensions listed previously) integral with at least two other microcomponents in which the three components encompass three dimensions. “Integral” refers to any connection in which one component is welded, soldered, or otherwise permanently connected to the other such that disconnection of the two require fracture, i.e., not simply clipped, screwed, or attached by any other non-permanent process. Preferably, the integral connection is such that a point of attachment is not detectable either visibly or by any light microscopy technique. Thus, in this embodiment, an integral device incorporating an attachable microcomponent, such as a computer having a silicon chip.
In one embodiment, the 3-D microstructure can be maintained (i.e. held in place) by any non-permanent attachment, such as gluing, clipping, taping or the like. Referring back to
Metals that are easily patterned via soft lithography and then deformed may not provide sufficient structural integrity for all applications. For example, when a ductile metal such as silver or gold is folded, bent or otherwise deformed, the resulting structure may have cracks, small tears, or stress-thinned regions resulting around the area of deformation. Thus, in one embodiment, the method further comprises reinforcing the microstructure at least in the regions encompassing the deformed portions. Reinforcing allows these defects to be either covered or filled, and thus the mechanical integrity of the structure is retained and even enhanced. In alternative embodiment, the entire microstructure can be reinforced.
In one embodiment, the step of reinforcing comprises increasing the thickness of the structure by at least about 10%, more preferably by at least about 25%, more preferably by at least about 50% and even more preferably by at least about 100%. Of course, one of ordinary skill in the art can determine an appropriate thickness of coating such that the thickness can be increased by as much as 500%, 1000% or more. In one embodiment, the step of reinforcing involves coating at least the deformed regions with a material capable of conferring greater stability or rigidity to the 3-D microstructure. The reinforcing material can be the same or a different material from the initially deformed microstructure.
In one embodiment, the 3-D microstructure is reinforced by plating with a metal. Examples of metal plating processes include electroless plating and electroplating. “Electroplating” refers to a process involving exposing at least a portion of an article to a solution containing metal ions and subjecting the portion of the article and solution to electrochemical conditions. In one embodiment, at least a portion of the article is immersed in the solution, and preferably at least the deformed portion is immersed. Electrochemical conditions involve the application of an electrical current resulting in a transformation (e.g. reduction) of metal ions to metal atoms. The resulting metal atoms can be deposited onto the article as a metal coating formed around the immersed article portion.
When electroplating, a thickness of the metal coating can be manipulated by certain factors such as concentration of the metal ions in solution, electroplating time and/or current density. The electroplated metal can be selected from any metal capable of being electroplated, i.e. the metal can exist as a stable solution of metal ions and subjected to electrochemical conditions to form the neutrally charged metal. Examples of such metals include nickel, silver, etc. Electroplating can be considered a method of “electrochemical welding” to provide a final product having high structural integrity.
Prior to the step of reinforcing, the structure can be fastened, attached or held in place in a non-permanent manner, as described previously. Non-permanent attachments allow the structure to maintain its form for the duration of the reinforcing step. Where the reinforcing comprises electroplating, the non-permanent attachment is capable of withstanding solution and/or electrochemical conditions.
Electroplating can be considered as a method of “electrochemical welding.” An advantageous feature of the method of electrochemical welding lies in the capability to make integral connections between several points at the same time. Thus, one embodiment of the present invention involves a method for simultaneously making a plurality of at least two integral connections to form a 3-dimensional microstructure. An additional advantageous feature involves the added benefit of also simultaneously coating other portions of the structure not involved in the formation of integral connections, such that a microstructure having thicker dimensions is readily obtained to confer structural stability to the microstrcuture.
From
In one embodiment, the present invention provides a method for making a 3-D microstructure comprising connecting a first microstructure to a second microstructure. In this aspect is the resulting 3-D microstructure involves the first microstructure being integral with the second microstructure. An advantageous feature is that the resulting integral connection confers rigidity and structural integrity to the 3-D microstructure. The first microstructure is preferably not supported by a substrate whereas the second microstructure can either be supported by a substrate or can also be free-standing.
In one embodiment, connecting the two microstructures to form an integral connection is accomplished by reinforcing technique such as coating. In one embodiment, the coating step involves electroplating.
Another aspect of the present invention provides a method for making a 3-D microstructure involving deforming a microstructure at a predetermined deformable portion to provide a deformed portion. This deformed portion is then treated to form a non-deformable portion. In one embodiment, the treating involves electroplating the deformed portion. In this manner, the once deformable portion, can be rendered sufficiently non-deformable.
Thus, reinforcing (e.g. electroplating) the folded structure thus can serve three functions: (1) providing thicker metal features where desired; (2) providing an integral connection; (3) covering any cracks or defects resulting from the deformation; and (4) rendering deformable portions non-deformable.
By bending portion 92 out of the plane in a direction indicated by arrow 94, a 3-dimensional microstructure 97 can be achieved. Although it may be possible to bend deformable portion 92 in several directions other than arrow 94, the most stable orientation is achieved when portion 92 is bent in the direction of arrow 94 to the extent that all zig-zag lines 96 are straightened equivalently. Thus, deformable portion 92 is intended to be deformed in a predetermined direction. Should it be desired that deformable portion 92 be directed towards another direction, the dimensions of zig-zag lines 96 can be altered, such as by changing the length of each straight-line portion of zig-zag line 96 or the points of intersection of two zig-zag lines 96, to achieve the most stable configuration in the other direction. It is understood that portion 92 can be deformed in the direction of arrow 94 to a variety of heights. For example, a small deformation of portion 92 will result in a smaller height than a larger deformation. The extent of deformation can also be predetermined by varying the dimensions of zig-zag lines 96 (i.e., changing the length of straight line portions of the zig-zag line 96).
Use of deformable portions allow the remaining portions to retain their structural integrity. For example, it is known that bending a rigid mesh cylinder typically results in collapse of the open mesh framework, at least in the regions in the vicinity of the bend.
To achieve further structural stability, protruding points of diamond 102 can be bent in the direction of arrows 106a and 106b, to result in the structure shown in
The cylindrical structures of
Thus, the methods of the present invention can be used to prepare 3-D structures which cannot be achieved by conventional two-dimensional lithography techniques. However, the initial microstructures can be provided by various patterning methods.
In one embodiment, a concerted deforming mechanism involving a plurality of deformable portions can provide 3-D microstructures having resulting rigid deformed portions, without the need for further reinforcement. For example,
FIGS. 6(c) and 6(e) show copies of photomicrographs of structure 110 before and after deformation, respectively. The cylinder can include alternating sections of deformable portions and cylindrical mesh units throughout the length of the structure 110. The deformable portion does not necessarily need to result in a cuboid structure, as many other geometries that provide rigid structures can be envisioned.
In the structures of
Another aspect of the present invention provides a method for making a microstructure having a link. A link can be constructed by providing a hollow portion and a component penetrating the hollow portion. In one embodiment, the hollow portion is contained within an outline of a closed shape. The closed shape can be a regular shape such as a triangle, a circle, an oval, a rectangle, an octagon. Alternatively, the closed shape can be irregular.
The component penetrating the hollow portion links the outline of the closed shape. The link can be detachable e.g. a rod penetrating a hoop is linked to the hoop but can be withdrawn from the hoop to break the link. The component penetrating the hollow portion can be straight, curved, planar, three-dimensional, or the like, so long as it is of a sufficient dimension to fully penetrate the hollow portion. The component penetrating the hollow portion can be non-detachable, e.g. a chain link. A chain link comprises two components fastened two each other, yet each are freely movable. Thus, the component penetrating the hollow portion can also comprise an outline of a closed shape having any of the features described previously.
In this aspect, the method involves patterning a link by providing first and second 3-D substrates, each substrate having a pattern printed thereon. The pattern on each substrate is designed such that upon supporting the first substrate adjacent the second substrate, the combined pattern has at least one feature resembling a link. In one embodiment, the first and second substrates are non-planar, e.g. curved or contain a fold.
The supported first and second substrates can be electroplated, and upon dissolving the first and second substrates, the chain-link results.
A chain link is designed by patterning semicircles 134a and 134b on faces 133a and 133b of respective substrates 130a and 130b where a portion of semicircles 134a and 134b penetrate the whole circle (hollow portion) of complementary semicircles 132a and 132b. Thus, a whole circle formed by matched semicircles 134a and 134b function as the component that penetrates the hollow portion formed by whole circle 132a and 132b. The component does not necessarily need to be a whole circle to penetrate a hollow portion and can be any closed geometrical shape, an open circle having a small gap, a straight line portion etc.
It has been discovered that alignment is achieved easily by using non-planar substrates such as cylindrical substrates in place of block-like substrates 130a and 130b. In
From these basic principles for preparing chain-link structures, more intricate intertwined structures can be achieved by appropriate design of the photomask for each substrate.
Another aspect of the invention provides a free-standing 3-dimensional truss. “Truss” refers to a structure having an open framework capable of supporting an object at least 2, 3, 5 or even 10 or more times its weight. In one embodiment, the truss comprises an open framework and has at least one dimension less than about 1 mm. Open framework structures have advantageous properties of rigidity and stability while using a minimal amount of material. Trusses can be either two-dimensional or three-dimensional. Macroscopic trusses are found in many building components. 2-D trusses are often used as roof supports whereas 3-D trusses can be found in the ceiling of a gymnasium, cylindrical vaults and hemispherical domes. A 2-D truss takes advantage of the inherent stability of triangles where angles of a triangle cannot changed without changing the lengths of its sides. Because a truss is based on triangular shapes, elements of a truss are relatively slender and widely spaced, allowing trusses to retain a high strength-to-weight ratio. 3-D trusses utilize either a tetrahedron as the basis of the open framework where a tetrahedron comprises four triangles, or a square pyramid comprising four triangles arising from a square base.
In one embodiment, the 3-D truss comprises at least two tetrahedra placed side-by-side. “Side-by-side” can involve aligning two edges of the tetrahedra together or aligning two faces of the tetrahedra together. In another embodiment, the 3-D truss comprises at least two square pyramids placed side-by-side.
The techniques to build macroscopic trusses are not applicable at the micron scale. Macroscopic trusses utilize a large number of individually machine components, such as nuts, bolts and welding. Trusses are often made of steel components, and the process to produce steel components, such as rolling, casting and forging are not feasible at scales of less than 1 mm.
This aspect of the present invention to prepare trusses can be accomplished by using several techniques described previously.
The function and advantage of these and other embodiments of the present invention will be more fully understood from the examples below. The following examples are intended to illustrate the benefits of the present invention, but do not exemplify the full scope of the invention.
Referring to
Described in this Example is a transformation of a planar structure into a 3-D microstructure of
Described in this Example is a deformation of free-standing cylindrical microstructure 101 of
Described in this Example is a schematic illustration of the fabrication of 3-D microstructure of
Described in this Example is a scheme for fabricating a chain-link using a flexible photomask and electrochemical welding, as shown in
Described in this Example is a scheme for the formation of a trefoil knot of
The preparation of a 3-D truss is described in this Example. A design for truss patterns is generated using a suitable computer aided drawing (CAD) software application (Macromedia Freehand 7.0) printed onto a transparency using a commercial laser-assisted image-setting system (Hercules PRO, 3387 dpi, Linotype-Hell Company, Hauppauge, N.Y.). This transparency is used as a photomask to generate a relief pattern in a layer of photoresist. Microcontact printing is performed as described in
After electrically contacting the silver pattern, the glass substrate is immersed in a Ag electroplating bath (Techni-Silver E2, Technic Inc., Providence, R.I.) at room temperature and electrodeposited Ag at a current density of ˜20 mA/cm2 for 15 min. At this point, the adhesion between the electroplated Ag layer and the initial vapor-deposited Ag layer was sufficiently poor to make possible manual separation of the Ag grid structure from the substrate using tweezers.
As described previously, the 3-D truss can be thought of as an array of tetrahedra or as an array of square-based pyramids. The truss can also be assembled from its component set of grids, two of which are planar (grids 155 and 156 of
The three grids are aligned manually as shown in
The open framework of
Those skilled in the art would readily appreciate that all parameters listed herein are meant to be examples and that actual parameters will depend upon the specific application for which the methods and apparatus of the present invention are used. It is, therefore, to be understood that the foregoing embodiments are presented by way of example only and that, within the scope of the appended claims and equivalents thereto, the invention may be practiced otherwise than as specifically described.
This application is a continuation of U.S. application Ser. No. 09/593,716, filed Jun. 14, 2000, which claims the benefit under Title 35, U.S.C. § 119(e) of U.S. provisional application Ser. No. 60/140,177, filed Jun. 18, 1999, entitled “Three-Dimensional Microstructures,” by Rebecca J. Jackman et al., incorporated herein by reference, and of U.S. provisional application Ser. No. 60/141,184, filed Jun. 25, 1999, entitled “Three-Dimensional Microstructures,” by Rebecca J. Jackman et al., incorporated herein by reference.
Number | Date | Country | |
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60140177 | Jun 1999 | US | |
60141184 | Jun 1999 | US |
Number | Date | Country | |
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Parent | 09593716 | Jun 2000 | US |
Child | 10924759 | Aug 2004 | US |