The present disclosure relates generally to porous structures with tailored Poisson's ratios. More particularly, aspects of this disclosure relate to auxetic structures with engineered patterns that exhibit negative Poisson's Ratio (NPR) behavior, as well as systems, methods and devices using such structures.
When materials are compressed along a particular axis, they are most commonly observed to expand in directions transverse to the applied axial load. The material property that characterizes this behavior is known as the Poisson's Ratio, which is defined as the negative of the ratio of transverse/lateral strain to axial/longitudinal strain under uni-axial loading conditions. The majority of materials are characterized by a positive Poisson's Ratio (e.g., about 0.3 for aluminum, brass and steel) and will expand in the transverse direction when compressed in the axial direction and will contract in the transverse direction when stretched in the axial direction. However, materials with a negative Poisson's Ratio (NPR), also known as “auxetic” materials, will contract in the transverse direction when compressed in the axial direction and expand in the transverse direction when stretched in the axial direction.
U.S. Pat. No. 5,233,828 (“'828 Patent”), to Phillip D. Napoli, shows an example of an engineered structural member—a combustor liner—utilized in high temperature applications. Combustor liners are generally used in the combustion section of a gas turbine, but can also be used in the exhaust section or in other sections of or components of the gas turbine, such as the turbine blades. In operation, the combustors burn gas at intensely high temperatures, such as 3,000° F. or higher. To prevent this intense heat from damaging the combustor before it exits to a turbine, the combustor liner is inserted in the combustor to insulate the surrounding engine. To minimize temperature and pressure differentials across the combustor liners, cooling slots have conventionally been provided, as shown in '828 Patent. The '828 Patent shows a portion of an annular combustor liner having spaced cooling holes disposed in a continuous pattern, angled through the wall of the liner. U.S. Pat. No. 8,066,482 B2, to James Page Strohl et al., shows another example of an engineered structural member having cooling holes shaped to enhance the cooling of a desired region of a gas turbine and to reduce stress levels in and around the cooling holes. European Patent No. EP 0971172 A1, to Dr. Jakob Keller, likewise shows another example of a perforated liner used in a combustion zone of a gas turbine.
In yet another example, U.S. Patent Application Pub. No. 2010/0009120 A1, to Mary C. Boyce et al., discloses a number of transformative periodic structures which include elastomeric or elasto-plastic periodic solids that experience transformation in the structural configuration upon application of a critical macroscopic stress or strain. PCT patent application PCT/US2014/025324, to the President and Fellows of Harvard College, discloses, inter alia, void structures with repeating elongated-aperture patterns providing Negative Poisson's Ratio behavior. PCT patent application PCT/US2014/024830, to the President and Fellows of Harvard College, discloses, inter alia, a solid having an engineered void structure that causes the solid (having a positive Poisson ratio) to exhibit pseudo-auxetic (NPR) behavior upon application of stress to the solid. The engineered void structure provides a porosity amenable to, for example, applications involving gas turbine combustors. All of the foregoing patent documents are incorporated herein by reference in their respective entireties for all purposes.
Aspects of the present disclosure are directed toward multi-layer negative Poisson's Ratio (NPR) structures and particularly auxetic structures for industrial applications where thermo-mechanical expansion and porosity are important design considerations.
In some aspects of the present concepts, an auxetic structure includes a first sheet and a second sheet, the first sheet defining therein a plurality of first openings in a first pattern, the plurality of first openings providing a first porosity and the second sheet defining therein a plurality of second openings in a second pattern to provide a second porosity. The second sheet is overlaid on the first sheet so that the plurality of second openings at least partially occlude the plurality of first openings to define a plurality of third openings in a third pattern, the plurality of third openings defining a third porosity less than that of the first porosity or the second porosity. The second sheet is connected to the first sheet by a plurality of distinct connection elements. In some aspects, the first sheet and the second sheet have the same porosity and the same type of voids, with the only difference between them being their relative orientations and/or their scale factor.
According to some aspects of the present concepts, an auxetic structure comprises a first auxetic sheet defining therein a plurality of first openings in a first pattern, the plurality of first openings defining a first porosity, a second auxetic sheet defining therein a plurality of second openings in a second pattern, the plurality of second openings defining a second porosity and a third auxetic sheet defining therein a plurality of third openings in a third pattern, the plurality of third openings defining a third porosity. The third auxetic sheet overlays the second auxetic sheet so that the plurality of third openings at least partially occlude the plurality of second openings and the second auxetic sheet overlays the first auxetic sheet so that the plurality of second openings at least partially occlude the plurality of first openings. The third auxetic sheet is connected to the second auxetic sheet by a plurality of connection elements likewise the second auxetic sheet is connected to the first auxetic sheet by a plurality of connection elements. Only the mid-points of the cells are connected to each other since the mid-points have the same deformation pattern when an external load is applied.
In accordance with other aspects of the present concepts, a computer-implemented method of manufacturing a multi-sheet auxetic structure comprises the act of receiving, via one or more input devices operatively associated with a computer, design requirements of the multi-sheet structure, the received design requirements comprising at least one of a required porosity, a required Negative Poisson's Ratio (NPR) value, and a required stiffness. The method also includes the act of using the computer to construct a model for a plurality of sheets, each of the sheets defining a unit cell arrangement and opening parameters and to construct a model of a multi-sheet structure utilizing the plurality of sheets, each of the plurality of sheets being connected at center points of unit cells at least to adjoining ones of the plurality of sheets. The method also includes the act of using the computer to conduct a modeling of the multi-sheet structure under simulated loading and to determine if the multi-sheet structure satisfies the design requirements. If not, the computer is configured to execute instruction sets causing the computer to iteratively perform the acts of (i) modifying at least one aspect of the model for at least one of the plurality of sheets, the model of the multi-sheet structure, or both the model for at least one of the plurality of sheets and the model of the multi-sheet structure and (ii) modeling of the multi-sheet structure under the simulated loading until the model of the multi-sheet structure is determined to satisfy the design requirements. The method also includes the act of causing the computer to save the model of the multi-sheet structure in a non-transient physical computer-readable storage medium.
The above summary is not intended to represent every embodiment or every aspect of the present disclosure. Rather, the foregoing summary merely provides an exemplification of some of the novel aspects and features set forth herein. The above features and advantages, and other features and advantages of the present disclosure, will be readily apparent from the following detailed description of representative embodiments and modes for carrying out the present invention when taken in connection with the accompanying drawings and the appended claims.
The present disclosure is susceptible to various modifications and alternative forms, and some representative embodiments have been shown by way of example in the drawings and will be described in detail herein. It should be understood, however, that the inventive aspects are not limited to the particular forms illustrated in the drawings. Rather, the disclosure is to cover all modifications, equivalents, combinations, and alternatives falling within the spirit and scope of the invention as defined by the appended claims.
This disclosure is susceptible of embodiment in many different forms. There are shown in the drawings, and will herein be described in detail, representative embodiments with the understanding that the present disclosure is to be considered as an exemplification of the principles of the present disclosure and is not intended to limit the broad aspects of the disclosure to the embodiments illustrated. To that extent, elements and limitations that are disclosed, for example, in the Abstract, Summary, and Detailed Description sections, but not explicitly set forth in the claims, should not be incorporated into the claims, singly or collectively, by implication, inference or otherwise. For purposes of the present detailed description, unless specifically disclaimed or logically prohibited: the singular includes the plural and vice versa; and the words “including” or “comprising” or “having” means “including without limitation.” Moreover, words of approximation, such as “about,” “almost,” “substantially,” “approximately,” and the like, can be used herein in the sense of “at, near, or nearly at,” or “within 3-5% of,” or “within acceptable manufacturing tolerances,” or any logical combination thereof, for example.
Aspects of the present disclosure are directed towards hybrid dimple-and-void auxetic structures which include repeating aperture and protrusion patterns that provide negative Poisson's Ratio (NPR) behavior when macroscopically loaded. Poisson's Ratio (or “Poisson coefficient”) can be generally typified as the ratio of transverse contraction strain to longitudinal extension strain in a stretched object. Poisson's Ratio is typically positive for most materials, including many alloys, polymers, polymer foams and cellular solids, which become thinner in cross section when stretched. The auxetic structures disclosed herein exhibit a negative Poisson's Ratio behavior.
According to aspects of the disclosed concepts, when the auxetic structure is compressed along one axis (e.g., in the Y direction), coaxial strain results in a moment around the center of each cell because of the way the adjacent apertures are arranged. This, in turn, causes the cells to rotate. Each cell rotates in a direction opposite to that of its immediate neighbors. This rotation results in a reduction in the transverse axis (X-direction) distance between horizontally adjacent cells. In other words, compressing the structure in the Y direction causes it to contract in the X direction. Conversely, tension in the Y direction results in expansion in the X direction. At the scale of the entire structure, this mimics the behavior of an auxetic material. But many of the structures disclosed herein are composed of conventional materials. Thus, the unadulterated material itself may have a positive Poisson's Ratio, but by modifying the structure with the introduction of the aperture patterns and combinations disclosed herein, the structure behaves, locally and/or globally, as having a negative Poisson's Ratio.
As seen in
The NPR structures disclosed herein may be utilized, for example, in a gas turbine combustor wall, which requires a certain “porosity” (i.e., openings for cooling air flow), defined generally as the surface area of the apertures, AA, divided by the surface area of the structure, AS, or Porosity=AA/AS. By way of example, a porosity of 40-50% may be required for a particular component. In various aspects of the present concepts, the porosity of the disclosed NPR structure can be tailored to provide any desired porosity between, for example, 0-50% (e.g., between 0.3-9%, between 1-4%, approximately 2%, etc.) by selective combination of two or more layers of structures (e.g., structures 100, 200 in
In some embodiments, the material of one or more of the layers 100, 200 comprises a superalloy, such as a nickel-based superalloy, including but not limited to Inconel (e.g. IN100, IN600, IN713), Waspaloy, Rene alloys (e.g. Rene 41, Rene 80, Rene 95, Rene N5), Haynes alloys, Incoloy, MP98T, TMS alloys or CMSX (e.g. CMSX-4) single crystal alloys. The present concepts are not material-limited, may comprise other materials (e.g., stainless steel, titanium, etc.) suitable for utilization in a particular application utilizing a non-zero porosity structure. By way of example, the NPR structure 500 may comprise a first layer 100 of a first material composition, a second layer 200 of a second material composition, a third layer of a third material composition, etcetera. Alternatively, each of the layers forming the NPR structure 500 may comprise the same material.
Each layer 100, 200, as well as the NPR structure 500, each present a preselected aspect ratio for the elongated openings 105, 205, 505. As used herein, the “aspect ratio” of the openings is defined to mean the length of the opening divided by the width of the opening, or the length of the major axis divided by the length of the minor axis of the opening. It may be desirable, in some embodiments, that the aspect ratio of the openings be approximately 5-40 or, in some embodiments, approximately 20-30. Dimensionally, the disclosed concepts and structures are presented utilizing patterns having a millimeter lengthscale; however, the concepts are not limited to any particular lengthscale and the concepts are equally applicable to structures possessing the same patterns and structures at smaller or larger lengthscales.
Again, in the example of
As to the attachment of one layer (e.g., layer 100) to another layer (e.g., layer 200), the layers can be attached to one another in a number of conventional ways, a few illustrative examples of which follow.
In a first example, as shown in
In a second example, shown in
In a third example of an NPR structure 500, shown in
In the NPR structure 500 shown
In the above-noted examples, the relation between and connections between two layers of auxetic sheets 100, 200 was discussed; however, it is to be emphasized that the present concept expressly contemplate the use of any number of layered sheets, and particularly layered auxetic sheets, to provide control over the resulting porosity of the NPR structure 500.
Further, although the concepts of a multi-layer auxetic structure and methods for forming a multi-layer auxetic structure are disclosed in relation to layers or sheets with elliptical openings 105, 205, auxetic layers or sheets with all manners of openings (e.g., stop-holes, double-T voids, S-slots, etc.) can also be attached together via connection elements (e.g., rivets, welds, etc.) to yield a multi-layer auxetic or NPR structure in accord with the present concepts. By way of illustration,
The multi-layer structure in accord with aspects of the present concepts not only achieves auxetic behavior, but also enables a tailored reduction in porosity. By way of example, the aforementioned techniques may be used to provide an NPR structure having a porosity of 1.6% by combining a first layer having a 5% porosity pattern comprising elliptical voids (see, e.g.,
Although the particular application of auxetic structures in gas turbine components is emphasized, the concept can be applied to other industrial components where transverse thermo-mechanical expansion and/or fatigue failure should be considered in the components' design.
In accord with at least some aspects of the present concepts, a design of an NPR structure 300 is informed by a known final porosity value that is to be achieved, as well as a required negative Poisson's ratio and maximum allowable stress of the structure. Within this design envelope, the permissible geometry of the openings (e.g., pattern, shape (e.g., elliptical, S-shaped, etc.), aspect ratio, etc.) are determined for the application. It may be determined that the design envelope permits utilization of a single-layer NPR structure having a suitable porosity value and such a single layer NPR structure may be utilized in accord with conventional techniques. However, if the porosity of this single-layer NPR structure is higher than the porosity required for the application, a plurality of layers or sheets (e.g., 100, 200, etc.) can be advantageously designed and constructed to provide a tuned, multi-layer NPR structure having the desired porosity. In general, there is no preference over the different configurations, respectively shown in
For example, for a plurality of sheets of fixed porosity patterned with elliptical voids, the porosity reduction obtained by layered combinations of two (or more) auxetic sheets is inversely related to the ellipses' aspect ratio such that sheets with higher aspect ratio ellipses provide greater reductions in porosity than sheets with lower aspect ratio ellipses. A degree of porosity reduction is also related to the number of sheets used, with greater numbers of sheets used in combination leading to correspondingly greater reductions in porosity.
With reference to the flow chart of
As a starting point, the method requires an input of relevant design requirements for a structure, such as but not limited to external load requirements, thermal damping requirements, Poisson's ratio (if specified), porosity, stiffness, etcetera. From these design requirements, it is then determined whether the design requirements for the structure would potentially benefit from utilization of an auxetic (NPR) structure. For example, a structure can be anticipated to benefit from an NPR structure if the intended application for the structure is thermal-stress dominated or operates under displacement-controlled loading conditions. If it is determined that the auxetic structure application is not beneficial, then a conventional design for the structure is utilized.
However, if the structure may advantageously comprise an NPR structure, a Negative Poisson's Ratio (NPR) value or anticipated acceptable range of values for the structure is determined, at least in part, from the remainder of the received design values. Responsive to the dominant design variables (e.g., stiffness, porosity, etc.), an initial design for a multi-layer structure in accord with the present concepts (e.g., the techniques presented in each of
Once the general bounds of the structure's design are established, additional details are selected for each layer of the multi-layer structure to establish a starting point for further computer modeling including, but not limited to, selection of (for each layer) slot/opening (e.g., openings 105, 205 in
Once a suitable design has been determined, it is saved on a non-transient physical computer-readable medium for later (or substantially concurrent) transmission to a remote computer or CNC (computer numerical control) system via a suitable conventional wireless or hard-wired communication device. The design process generally disclosed is advantageously computer-implemented using a computer-executable set(s) of instructions borne by a non-transient physical computer-readable medium such as a hard disk, magnetic tape, magnetic drive, CD-ROM, DVD, RAM, PROM, EPROM, FLASH-EPROM, or semiconductor memory device (memory chip, flash drive, etc.). These set(s) of instructions are executed by one or more processors operatively associated with a computer (e.g., a desktop computer, laptop computer, tablet computer, handheld device, etc.) to design a multi-layer NPR structure subject to a predetermined design envelope (e.g., maximum stress, minimum predetermined lifespan, etc.) and to save and/or transmit such design to an external computer or system. By way of example, the external computer or system comprises a CNC machine (e.g., laser cutter) used to form individual layers of the multi-layer NPR structure to cause the CNC machine to create one or more layers of the multi-layer structure.
In accord with the present concepts, a uniform or “universal” single-layer structure (a single sheet material having openings of a specified porosity and opening geometry) can be used to fabricate a plurality of different NPR structures having a plurality of different porosities. These NPR structures provide lower stresses and longer fatigue lives than conventional structures and can be further tuned to have higher stiffness and better load-bearing capacities.
This invention can be used in a wide range of industrial components where thermo-mechanical expansion and porosity (or absence of porosity) are important including, but not limited to, turbine components, heat exchangers, piping, supports, fuselages, automotive or vehicular components, or any other structure or component subjected to mechanical and/or thermal loading. By way of example, it is noted that if the same type of sheets (e.g., elliptical openings with aspect ratio equal to 30) are attached using the technique shown in
The sheets, such as sheet steel or Inconel, can be made individually using CNC laser cutting or other conventional forming process (e.g., punching, straight or curved slitting, perforating, sawing, flame cutting, water jet machining, etc.), and can then be welded or riveted to each other to make the necessary connections.
The present invention is not limited to the precise construction and compositions disclosed herein. Rather, any and all modifications, changes, and variations apparent from the foregoing descriptions are within the scope and spirit of the invention as defined in the appended claims. Moreover, the present concepts expressly include any and all combinations and sub-combinations of the preceding elements and aspects.
This application claims the right of priority to U.S. Provisional Patent Application No. 62/118,821, filed on Feb. 20, 2015, and U.S. Provisional Patent Application No. 62/101,827, filed on Jan. 9, 2015, both of which are incorporated herein by reference in their respective entireties.
Filing Document | Filing Date | Country | Kind |
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PCT/US16/12766 | 1/9/2016 | WO | 00 |
Number | Date | Country | |
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62118821 | Feb 2015 | US | |
62101827 | Jan 2015 | US |