The present disclosure relates generally to porous materials and cellular solids with tailored isotropic and anisotropic 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. Conversely, most materials contract along a particular axis when a tensile load is applied along an axis transverse to the axis of contraction. The material property that characterizes this behavior is known as the Poisson's Ratio, which can be defined as the negative of the ratio of transverse/lateral strain to axial/longitudinal strain under axial loading conditions. The majority of materials are characterized by a positive Poisson's Ratio, which is approximately 0.5 for rubber, approximately 0.3 for aluminum, brass and steel, and approximately 0.2 for glass.
Materials with a negative Poisson's Ratio (NPR), on the other hand, will contract (or expand) in the transverse direction when compressed (or stretched) in the axial direction. Materials that exhibit negative Poisson's Ratio behavior are oftentimes referred to as “auxetic” materials. The results of many investigations suggest that auxetic behavior involves an interplay between the microstructure of the material and its deformation. Examples of this are provided by the discovery that metals with a cubic lattice, natural layered ceramics, ferroelectric polycrystalline ceramics, and zeolites may all exhibit negative Poisson's Ratio behavior. Moreover, several geometries and mechanisms have been proposed to achieve negative values for the Poisson's Ratio, including foams with reentrant structures, hierarchical laminates, polymeric and metallic foams. Negative Poisson's Ratio effects have also been demonstrated at the micrometer scale using complex materials which were fabricated using soft lithography and at the nanoscale with sheet assemblies of carbon nanotubes.
A significant challenge in the fabrication of auxetic materials is that it usually involves embedding structures with intricate geometries within a host matrix. As such, the manufacturing process has been a bottleneck in the practical development towards applications. A structure which forms the basis of many auxetic materials is that of a cellular solid. Research into the deformation of these materials is a relatively mature field with primary emphasis on the role of buckling phenomena, on load carrying capacity, and energy absorption under compressive loading. Very recently, the results of a combined experimental and numerical investigation demonstrated that mechanical instabilities in 2D periodic porous structures can trigger dramatic transformations of the original geometry. Specifically, uniaxial loading of a square array of circular holes in an elastomeric matrix is found to lead to a pattern of alternating mutually orthogonal ellipses while the array is under load. This results from an elastic instability above a critical value of the applied strain. The geometric reorganization observed at the instability is both reversible and repeatable and it occurs over a narrow range of the applied load. Moreover, it has been shown that the pattern transformation leads to unidirectional negative Poisson's Ratio behavior for the 2D structure, i.e., it only occurs under compression.
U.S. Pat. No. 5,233,828 (“828 patent”) shows an example of an engineered void structure—a combustor liner or “heat shield”—utilized in high temperature applications. Combustor liners are typically used in the combustion section of a gas turbine. Combustor liners can also be used in the exhaust section or in other sections or components of the gas turbine, such as the turbine blades. In operation, combustors burn gas at intensely high temperatures, such as around 3,000° F. or higher. To prevent this intense heat from damaging the combustor before it exits to a turbine, the combustor liner is provided in the interior of the combustor to insulate the surrounding engine. To minimize temperature and pressure differentials across a combustor liner, cooling feature have conventionally been provided, such as is shown in the '828 patent, in the form of spaced cooling holes disposed in a continuous pattern. As another example, U.S. Pat. No. 8,066,482 B2 presents an engineered structural member having elliptically-shaped cooling holes to enhance the cooling of a desired region of a gas turbine while reducing stress levels in and around the cooling holes. European Patent No. EP 0971172 A1 likewise shows another example of a perforated liner used in a combustion zone of a gas turbine. None of the above patent documents, however, provide examples disclosed as exhibiting auxetic behavior or being engineered to provide NPR effects.
U.S. Patent Application Pub. No. 2010/0009120 A1 discloses various 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. Said transformation alters the geometric pattern, changing the spacing and the shape of the features within the transformative periodic structure. Upon removal of the critical macroscopic stress or strain, these elastomeric periodic solids recover their original form. By way of comparison, U.S. Patent Application Pub. No. 2011/0059291 A1 discloses structured porous materials, where the porous structure provides a tailored Poisson's ratio behavior. These porous structures consist of a pattern of elliptical or elliptical-like voids in an elastomeric sheet which is tailored, via the mechanics of the deformation of the voids and the mechanics of the deformation of the material, to provide a negative or a zero Poisson's ratio. All of the foregoing patent documents are incorporated herein by reference in their respective entireties and for all purposes.
Aspects of the present disclosure are directed towards auxetic structures with repeating patterns of elongated apertures (also referred to herein as “voids” or “slots”) that are engineered to provide a desired negative Poisson's Ratio (NPR) behavior and improved cooling performance. Unlike prior art NPR void shapes that extend through the plane of the structure material, traversing the thickness of the material in a direction normal to the material's plane, NPR voids disclosed herein traverse the thickness of the material at an angle that is oblique to the materials' plane. These angled void configurations enhance the cooling performance of the structure while retaining a low porosity and providing a desired NPR behavior. Other aspects of the present disclosure are directed to multi-functional NPR structures with angled air passages in the hot section of a gas turbine. Additional aspects are directed towards gas turbine combustors that are made with walls from a material with engineered angled void features that provide particular thermal, damping and/or acoustic functionalities. Such functionalities include, for example, acoustic attenuation (or noise damping), stress reduction (or load damping), and thermal cooling (or heat damping).
According to aspects of the present disclosure, auxetic structures with angled NPR slots are disclosed. In an example, an auxetic structure includes an elastically rigid body, such as a metallic sheet or other sufficiently elastic solid material, with opposing top and bottom surfaces. First and second pluralities of elongated apertures extend through the elastically rigid body from the top surface to the bottom surface. The first plurality of elongated apertures extends transversely (e.g., orthogonally) with respect to the second plurality of elongated apertures. The first and/or second pluralities of elongated apertures are obliquely angled with the top and/or bottom surfaces of the elastically rigid body. In an example, each slot traverses the thickness of a sheet material at an angle that is oblique (e.g., approximately 40-70 degrees) to the material's plane. The elongated apertures are cooperatively configured to provide a desired or minimum cooling performance while exhibiting stress reduction through negative Poisson's Ratio (NPR) behavior under macroscopic planar loading conditions. By way of example, the elongated apertures are engineered with a predefined porosity, a predetermined pattern, and/or a predetermined aspect ratio to achieve the desired NPR behavior. The auxetic structure may exhibit an effusion cooling effectiveness of approximately 30-50%, a porosity of about 0.3 to about 9%, and a Poisson's Ratio of approximately −0.2 to −0.9%. Cooling effectiveness (Eta) can be defined as the difference of the hot gas temperature to the wall temperature in the presence of a cooling device divided by the difference of the hot gas temperature to the temperature of the supplied cooling gas: Eta=(T_hotgas−T_wall)/(T_hotgas−T_coolant).
In accordance with other aspects of this disclosure, effusion-cooling auxetic sheet structures are featured. In an example, an effusion-cooling auxetic sheet structure is presented which includes a metallic sheet with opposing top and bottom surfaces. First and second pluralities of elongated apertures extend through the metallic sheet from the top surface to the bottom surface. The first plurality of elongated apertures has a first set of geometric characteristics and is arranged in a first pattern. Likewise, the second plurality of elongated apertures has a second set of geometric characteristics and is arranged in a second pattern. The elongated apertures of the first plurality are orthogonally oriented with respect to the elongated apertures of the second plurality. Each of the elongated apertures is obliquely angled with respect to the top surface of the elastically rigid body. The geometric characteristics and pattern of the first plurality of elongated apertures are cooperatively configured with the geometric characteristics and pattern of the second plurality of elongated apertures to provide a desired or minimum cooling performance while exhibiting negative Poisson's Ratio (NPR) behavior under macroscopic planar loading conditions.
Other aspects of the present disclosure are directed to methods of manufacturing and methods of using auxetic structures. In an example, a method is presented for manufacturing an auxetic structure. Said method includes: providing an elastically rigid body with opposing top and bottom surfaces; adding to the elastically rigid body a first plurality of apertures extending through the elastically rigid body from the top surface to the bottom surface, the first plurality of apertures being arranged in rows and columns; and, adding to the elastically rigid body a second plurality of apertures extending through the elastically rigid body from the top surface to the bottom surface, the second plurality of apertures being arranged in rows and columns. Each aperture of the first and/or second pluralities of elongated apertures is obliquely angled with the top surface of the elastically rigid body. The first and second pluralities of apertures are cooperatively configured to provide a desired or minimum cooling performance while exhibiting a negative Poisson's Ratio (NPR) behavior under macroscopic planar loading conditions. By way of example, the elongated apertures are engineered with a predefined porosity, a predetermined pattern, and/or a predetermined aspect ratio to achieve the desired NPR behavior. The auxetic structure may exhibit an effusion cooling effectiveness of approximately 30-50% and a Poisson's Ratio of approximately −0.2 to −0.9%. The elastically rigid body may take on various forms, such as a metallic sheet or other sufficiently elastic solid material.
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, which are considered to be inventive singly or in any combination, 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 of this disclosure are not limited to the particular forms illustrated in the drawings. Rather, the disclosure is to cover all modifications, equivalents, combinations and subcombinations, 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 auxetic structures which include repeating patterns of angled slots 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 an 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 angled-slot patterns disclosed herein, the structure behaves as having a negative Poisson's Ratio.
As seen in
Also disclosed are gas turbine combustors that are made with one or more walls from a material with any of the specific auxetic structure configurations disclosed herein. In some embodiments, the angled slots are generated in a metal body directly in a stress-free state such that the apertures are equivalent in shape to collapsed void shapes found in rubber under external load in order to get NPR behavior in the metal body without collapsing the metallic structure in manufacturing. Various manufacturing routes can be used to replicate the void patterns in the metallic component. The manufacturing does not necessarily contain buckling as one of the process steps. The auxetic structures disclosed herein are not limited to the combustor wall; rather, these features can be incorporated into other sections of a turbine (e.g., a blade, a vane, etc.).
In a conventional combustor wall, holes used for cooling air flow and damping also act as stress risers. In some of the disclosed embodiments, as the wall material at a hot spot presses against its surrounding material, e.g., in a vertical direction, the negative Poisson's Ratio will make the wall material contract in the horizontal direction, and vice versa. This behavior will reduce the stresses at the hotspot significantly. This effect is stronger than just the impact of the reduced stiffness. Stress at hot spot gets reduced, for example, by 50% which, in turn, leads to an increase in stress fatigue life by several orders of magnitude. The stress reduction by the NPR behavior does not increase the air consumption of the combustor wall. The longer life could be used as such or the wall material could be replaced by a cheaper one in order to reduce raw material costs.
It has also been demonstrated that the replacement of circular combustor cooling holes with a fraction of elongated and angled air passages of 2-3% reduces thermo-mechanical stress by a factor of at least five, while maintaining the cooling and damping performance. For example, elliptical cooling holes in the combustor have been predicted to result in a five-fold decrease in the worst principal stress. Inducing NPR behavior, thus, adds further functionality to the cooling holes of the combustor in that the NPR behavior generates a five-fold reduction in worst principal stress as compared to traditional cooling holes. In stress fatigue of a combustor-specific superalloy, halving the component stress increases the fatigue life by more than an order of magnitude. In some embodiments, the superalloy may be a nickel-based superalloy, such as 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, and CMSX (e.g. CMSX-4) single crystal alloys.
It has been shown that optimized porosity offers increased cooling function. As used herein, “porosity” can be defined to mean the surface area of the apertures, AA, divided by the surface area of the structure, AS, or Porosity=AA/AS. It may be desirable, in some embodiments, that the porosity of a given void structure be approximately 0.3-9.0% or, in some embodiments, approximately 1-4% or, in some embodiments, approximately 2%. By comparison, many prior art arrangements require a porosity of 40-50%.
There may be a predetermined optimal aspect ratio for the elongated apertures to provide a desired NPR behavior. As used herein, “aspect ratio” of the apertures can be defined to mean the length divided by the width of the apertures, or the length of the major axis divided by the length of the minor axis of the apertures. It may be desirable, in some embodiments, that the aspect ratio of the apertures be approximately 5-40 or, in some embodiments, approximately 20-30. An optimal NPR may comprise, for example, a PR of about −0.2 to about −0.9 or, for some embodiments, about −0.5. Aspects of the disclosed concepts can be demonstrated on structural patterns created with a pattern lengthscale at the millimeter, and are equally applicable to structures possessing the same periodic patterns at a smaller lengthscale (e.g., micrometer, submicrometer, and nanometer lengthscales) or larger lengthscales so far as the unit cells fit in the structure.
Turning next to
S-shaped through slots 312, 318 are arranged in an array or matrix of rows and columns, with the first plurality of elongated apertures 312 extending transversely with respect to the second plurality of elongated apertures 318. Note that hidden lines indicating the internal structural configuration of slots 318 have been omitted from
The illustrated pattern of elongated, angled slots provides a specific porosity (e.g., a porosity of about 0.3 to about 9.0%) and a desired cooling performance (e.g., an effusion cooling effectiveness of approximately 30-50%) while exhibiting a desired negative Poisson's Ratio behavior (e.g., a PR of about −0.2 to about −0.9) under macroscopic planar loading conditions (e.g., when tension or compression is applied in the plane of the sheet). When the auxetic structure 300 is stretched, for example via tensile force FT along a vertical axis Y, axial strain in the vertical direction results in a moment around the center of each cell, which causes the cells to rotate. A cell may consist of two laterally adjacent vertical slots aligned with two vertically adjacent horizontal slots to form a square-shaped unit. Each cell rotates in a direction opposite to that of its immediate neighboring cells. This rotation increases the X-direction distance between horizontally adjacent cells such that stretching the structure in the Y-direction causes it to stretch in the X-direction. The first plurality of S-shaped through slots 312 have (first) engineered geometric characteristics, including a predefined geometry and a predefined aspect ratio, while the second plurality of S-shaped through slots 318 have (second) engineered geometric characteristics, including a predefined geometry and a predefined aspect ratio, that are cooperatively configured with (third) engineered geometric characteristics of the aperture pattern, including NPR-slot density and cell arrangement, to achieve a desired NPR behavior under macroscopic loading conditions.
Each slot of the first and/or second pluralities of elongated S-shaped through slots 312, 318 can be obliquely angled with respect to the top surface 314 or bottom surface 316, or both, of the auxetic structure's 300 elastically rigid body 310. In an example, slot 312 is shown in
Patterned angled NPR-slot features, such as those disclosed in
It has been determined that having inclined cooling slots help to provide better film cooling effectiveness coverage in comparison to normal cooling holes with internal walls that are perpendicular to cooling flow. In addition, early investigation demonstrates that coolant ejection from an angled NPR slot is more efficient than ejection from normal cooling holes because the mixing process is less intensive for the closed film ejected from the slot. While the high thermal stresses encountered on gas turbine blades and vanes typically do not allow for the use of highly elongated slots, angled NPR slots help to reduce or otherwise eliminate high thermal stresses on turbine blades/vanes while enhancing film cooling performance. For at least some embodiments, it is generally desirable to minimize surface porosity and the amount of coolant used in a turbine engine; normal NPR slots can be replaced with a smaller number of angled NPR slots to minimize porosity. In this case, cooling flow consumption will be reduced while the film cooling performance of the effusion slots is maintained.
As an exemplary implementation of the disclosed features, one can consider a combustor liner with sheet metal walls in which conventional round effusion holes or normal effusion slots are replaced with a pattern of angled S-shaped NPR slots forming an auxetic structure. Cooling air fed through these angled S-shaped slots removes heat from the structure and produces an even distribution of cooling air over the surface. These angled slots, which have an increased internal surface area, enhance film cooling performance and improve mechanical response. Moreover, angled NPR slots are capable of sustaining higher flame temperatures, and help impart to the sheet a much longer life compared to conventional sheet metal walls with normal effusion holes.
Shown in
With continuing reference to
A new NPR slot shape, for instance, Z-shaped slots 512A (
Aspects of this disclosure are also directed to methods of manufacturing and methods of using auxetic structures. By way of example, a method is presented for manufacturing an auxetic structure, such as the auxetic structures described above with respect to
In some embodiments, the method includes at least those steps enumerated above and illustrated in the drawings. It is also within the scope and spirit of the present invention to omit steps, include additional steps, and/or modify the order presented above. It should be further noted that the foregoing method can be representative of a single sequence for designing and fabricating an auxetic structure. However, it is expected that the method will be practiced in a systematic and repetitive manner.
The present invention is not limited to the precise construction and compositions disclosed herein. Rather, any and all modifications, changes, combinations, permutations 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 subcombinations of the preceding elements and aspects.
This application claims the right of priority to U.S. Provisional Patent Application No. 62/118,826, filed on Feb. 20, 2015, and U.S. Provisional Patent Application No. 62/101,840, 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/US16/12769 | 1/9/2016 | WO | 00 |
Number | Date | Country | |
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62118826 | Feb 2015 | US | |
62101840 | Jan 2015 | US |