Foams are used in a variety of structural applications for their good compression response and mechanical energy dissipation characteristics while keeping the overall structural weight to a minimum. They are also known for offering good thermal and acoustic insulation. A class of structural foams called syntactic foams is considered for structural applications. These foams can be distinguished from conventional variety by the way they are manufactured. Unlike traditional foams which are produced by gasification of the matrix material, syntactic foams are produced by mechanical blending of hollow polymer, ceramic or metal microballoons (hollow microspheres) in a polymer or metal matrix. Thus porosity is due to the ‘filler’ phase resulting in a closed-cell microstructure. Further distinction of these foams is that porosity in these materials is often microscopic and known to offer many advantages including high surface area to volume ratio as well as macroscopic isotropy. The range of engineering applications of these foams has increased in recent years due to the advancement of materials processing methods that offer choices in microballoon wall-thickness and diameter as well as the materials with which they are made of. Syntactic foams have been extensively used by naval and marine equipment manufacturers for decks and submarines buoys. Syntactic foams are also used in civil and industrial engineering as imitation wood and other building construction materials for their high hear stiffness and specific strength. Due to the high specific energy absorption and impact resistance, syntactic foams have the potential for use as core materials of sandwich structures in lightweight combat vehicles and automobiles. Syntactic foams made of glass and carbon micro-/nano-spheres are used in aerospace structures, missile heads and heat shields for space vehicles. They are also employed in electronics and telecommunications due to superior thermal and dielectric properties as well as shock absorption characteristics.
Continued demand for lighter, stiffer, stronger and tougher structural components requires development of novel materials. Heterogeneous materials with discrete, dispersed and/or embedded phases in a matrix material (fiber reinforced composites, particulate composites, functionally graded materials, syntactic foams, etc.) are found suitable for many structural applications. There are, however, limitations in terms of the degree of concentration of the secondary phase that can be dispersed into the primary phase and the degree of inter connectivity between the phases. Nature overcomes such a limitation by adopting 3-D interpenetrating microstructures as evident in skeletal tissue and botanical systems. This observation has inspired a relatively new category of materials called Interpenetrating Phase Composite/s or IPC (also referred to as co-continuous composites. The IPC are multiphase materials in which the constituent phases are interconnected three-dimensionally and topologically throughout the microstructure (and hence sometimes are referred to as “3-3” composites). That is, both matrix and reinforcement phases/s interpenetrate all over the microstructure in all the three spatial dimensions. Thereby the two constituents in their stand alone state would have an open cell microstructure. Hence, IPC are uniquely different from traditional composites comprising of a matrix with one or more reinforcing filler phases (long fibers, whiskers, particles, microballoons, etc.) where such a complete interpenetration does not occur. Consequently, each phase of an IPC contributes its property to the overall macro scale characteristics synergistically. For example, if one constituent provides strength and toughness, the other might enhance stiffness, thermal stability, acoustic insulation and/or dielectric characteristics. Additionally, it is also possible to tailor residual stresses in the constituents to produce advantageous macro scale response in a metal-ceramic IPC. The tensile residual stresses in the metallic phase and the compressive ones in the ceramic phase delay crack initiation and strengthen the IPC. Based on the occurrence of phase interpenetration of different length scales, interpenetrating phase composites can be classified as molecular, micro or meso varieties. A blend of two or more cross-linked polymers which are interlaced but not covalently bonded to each other and cannot be separated unless chemical bonds are broken is an example of a molecular scale IPC and is called an InterPenetrating Network (IPN).
The present invention is directed to the composition for and methods of processing composite structural foam. In one embodiment, a method of producing a Interpenetrating Phase Composite (IPC) foam is disclosed. In this method, uncured epoxy-based syntactic foam is prepared and infiltrated into an open-cell scaffold. In some embodiments, the uncured epoxy-based syntactic foam contains premixed micron-size hollow glass microballoons. In other embodiments, the scaffold is coated with a silane. The uncured epoxy-based syntactic foam is subsequently cured to produce the Interpenetrating Phase Composite (IPC) foam.
The advantages of the invention will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the aspects described below. The advantages described below will be realized and attained by means of the elements and combinations particularly pointed out in the appended claims. It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive.
a is a cross-section of a lightweight IPC foam cylinder according to an example embodiment of the present invention having an open-cell aluminum preform infiltrated with epoxy based syntactic foam.
b is a micrograph of the IPC foam of
a is a chart showing the stress-strain curves of example syntactic foam having a volume fraction of 20% of microballoons for multiple aspect ratios.
b is a chart showing the stress-strain curves of example syntactic foam having a volume fraction of 20% of microballoons and having a length to diameter ratio of 0.74.
a is a SEM image of an example deformed syntactic foam sample with 30% volume fraction of microballoons at a strain of about 10%.
b is a SEM image of an example deformed syntactic foam sample with 30% volume fraction of microballoons at a strain of about 60%.
c is a SEM image of the highlighted portion of
a is a chart demonstrating the compression response of example uncoated IPC foams with varying microballoon volume fractions and example unfilled aluminum preforms.
b is a chart demonstrating the compression response of example silane coated IPC foams with varying microballoon volume fractions.
a is a SEM image of an example silane coated IPC foam at a strain of 10%.
b is a SEM image of an example silane coated IPC foam at a strain of 58%.
c is a SEM image of an example uncoated IPC foam at a strain of 14%.
a is a chart demonstrating the comparison of stress-strain response of syntactic foam examples, IPC foam examples with uncoated preform, and IPC foam examples with silane coated preform for 20% volume fraction of microballoons.
b is a chart demonstrating the comparison of stress-strain response of syntactic foam examples, IPC foam examples with uncoated preform, and IPC foam examples with silane coated preform for 30% volume fraction of microballoons.
c is a chart demonstrating the comparison of stress-strain response of syntactic foam examples, IPC foam examples with uncoated preform, and IPC foam examples with silane coated preform for 40% volume fraction of microballoons.
a is a chart showing the comparison of energy absorption (up to 50% strain) for syntactic foams and IPC foam samples per unit volume.
b is a chart showing the comparison of energy absorption (up to 50% strain) for syntactic foams and IPC foam samples per unit mass.
The present invention may be understood more readily by reference to the following detailed description of the invention taken in connection with the accompanying drawing figures, which form a part of this disclosure. It is to be understood that this invention is not limited to the specific devices, methods, conditions or parameters described and/or shown herein, and that the terminology used herein is for the purpose of describing particular embodiments by way of example only and is not intended to be limiting of the claimed invention. Any and all patents and other publications identified in this specification are incorporated by reference as though fully set forth herein.
Also, as used in the specification including the appended claims, the singular forms “a,” “an,” and “the” include the plural, and reference to a particular numerical value includes at least that particular value, unless the context clearly dictates otherwise. Ranges may be expressed herein as from “about” or “approximately” one particular value and/or to “about” or “approximately” another particular value. When such a range is expressed, another embodiment includes from the one particular value and/or to the other particular value. Similarly, when values are expressed as approximations, by use of the antecedent “about,” it will be understood that the particular value forms another embodiment.
Described herein are Interpenetrating Phase Composite (IPC) foams and methods for making and using the same. As described above, the Interpenetrating Phase Composite (IPC) foams described herein (also called co-continuous composites) are multiphase materials in which the constituent phases are interconnected three-dimensionally and topologically throughout the microstructure (and hence sometimes are referred to as “3-3” composites). That is, both matrix and reinforcement phase/s interpenetrate all over the microstructure in all the three spatial dimensions. In one embodiment, the IPCs are meso-/micro-scale IPCs.
In one embodiment, the Interpenetrating Phase Composite (IPC) is produced by the method comprising:
a. providing an uncured epoxy-based syntactic foam;
b. infiltrating the uncured epoxy-based syntactic foam into an open-cell scaffold; and
c. curing the uncured epoxy-based syntactic foam to produce the Interpenetrating Phase Composite.
In another embodiment, the Interpenetrating Phase Composite comprises:
a. a scaffold; and
b. a cured epoxy-based syntactic foam in contact with the scaffold.
Each component and step listed above is described in detail below. The syntactic foams useful herein are produced from uncured epoxy-based resins. The epoxy resin can vary and includes conventional, commercially available epoxy resins. Two or more epoxy resins may be employed in combination. In one embodiment, the epoxy resins can be glycidated resins, cycloaliphatic resins, epoxidized oils, and so forth. In one aspect, the glycidated resins are the reaction product of a glycidyl ether, such as epichlorohydrin, and a bisphenol compound such as bisphenol A. C4-C28 alkyl glycidyl ethers; C2-C28 alkyl- and alkenyl-glycidyl esters; C1-C28 alkyl-, mono- and poly-phenol glycidyl ethers; polyglycidyl ethers of pyrocatechol, resorcinol, hydroquinone, 4,4′-dihydroxydiphenyl methane (or bisphenol F), 4,4′-dihydroxy-3,3′-dimethyldiphenyl methane, 4,4′-dihydroxydiphenyl dimethyl methane (or bisphenol A), 4,4′-dihydroxydiphenyl methyl methane, 4,4′-dihydroxydiphenyl cyclohexane, 4,4′-dihydroxy-3,3′-dimethyldiphenyl propane, 4,4′-dihydroxydiphenyl sulfone, and tris (4-hydroxyphynyl)methane; polyglycidyl ethers of the chlorination and bromination products of the above-mentioned diphenols; polyglycidyl ethers of novolacs; polyglycidyl ethers of diphenols obtained by esterifying ethers of diphenols obtained by esterifying salts of an aromatic hydrocarboxylic acid with a dihaloalkane or dihalogen dialkyl ether; polyglycidyl ethers of polyphenols obtained by condensing phenols and long-chain halogen paraffins containing at least two halogen atoms; N,N′-diglycidyl-aniline; N,N′-dimethyl-N,N′-diglycidyl-4,4′-diaminodiphenyl methane; N,N,N′,N′-tetraglycidyl-4,4′-diaminodiphenyl methane; N,N′-diglycidyl-4-aminophenyl glycidyl ether; N,N,N′,N′-tetraglycidyl-1,3-propylene bis-4-aminobenzoate; phenol novolac epoxy resin; cresol novolac epoxy resin; and combinations thereof. In one aspect, the epoxy resin is Epo-Thin manufactured by Buehler, Ltd., which is a bisphenol-A-(epichlorhydrin) epoxy resin.
In certain embodiments, a curing agent can be used to produce the syntactic foam. The selection of a given curing agent is dependent on the size of the syntactic foam batch to be cured and the reactivity of a given curing agent. In one aspect, an amine curing agent can be employed. Various polyamines can be used for this purpose, including aliphatic and aromatic amines, cycloaliphatic amines, a Lewis base or a Mannich base. For example, the aliphatic amine and cycloaliphatic amines may be alkylene diamines such as ethylene diamine, propylene diamine, 1,4-diaminobutane, 1,3-diaminopentane, 1,6-diaminohexane, 2,5-diamino-2,5-dimethylhexane, 2,2,4-trimethyl-1,6-diaminohexane, 1,11-diaminoundecane, 1,12-diaminododecane, 1,3- or 1,4-cyclohexane diamine, 1-amino-3,3,5-trimethyl-5-aminomethyl-cyclohexane, 2,4- or 2,6-hexahydrotolvylene diamine 2,4′- or 4,4′-diaminodicyclohexyl methane, 3,3′-dialkyl-4,4′-diamino-dicyclohexyl methane isophoronediamine, trimethylhexamethylene diamine, triethylene diamine, piperazine-n-ethylamine, polyoxyalkylene diamines made from propylene oxide and/or ethylene oxide. Examples of aromatic polyamines include 2,4- or 2,6-diaminotoluene and 2,4′- or 4,4′-diaminodiphenyl methane. Mixtures of amine curing agents can also be used herein.
In certain embodiments, the uncured epoxy-based syntactic foam comprises premixed micron-size hollow microballoons (also referred to as microbubbles or microspheres). The microballoons can be made of a variety of materials including, but not limited to, glass and ceramics. In other aspects, the microballoons are polymeric microspheres. For example, the microsphere can be Expancel manufactured by AkzoNobel. In another aspect, the microballoon is a sodium-lime-borosilicate glass sold under the tradename K-1 by 3M Corp. Other examples of commercially available glass microballoons useful herein include S15/300, B38, C15, K20, VS 5500, A16, H2O and the like, which are available from 3 M. In one embodiment, the microballoons have a mean diameter of about 50-70 micrometers and wall thickness of about 0.5-0.7 micrometers. In another embodiment, the volume fraction of microballoons in the syntactic foam is from 10%-50% while keeping the volume fraction of the metallic scaffold the same in order to produce different IPC foam varieties.
The open-cell scaffold can be composed of a variety of different metals. In one embodiment, the scaffold is composed of a metal or metal oxide. For example, the scaffold is composed of aluminum, copper, nickel. In one embodiment, metallic scaffolds sold by ERG Aerospace, Inc. can be used herein. In other embodiments, the scaffolds are made of one or more polymeric materials. For example, the scaffold is composed of a tough polymeric material such as a urethane. In one embodiment, the scaffold has 30-50 pores per inch and about 8-10% relative density.
In certain embodiments, the scaffold can be coated with a silane in order to enhance adhesion of the uncured epoxy-based syntactic foam to the scaffold. In one embodiment, the silane comprises a straight or branched-chain aminosilane, aminoalkoxysilane, aminoalkylsilane, aminoarylsilane, an aminoaryloxysilane, or any combination thereof. In another embodiment, the silane comprises gamma-aminopropyl trimethoxysilane, N-(beta-aminoethyl)-3-aminopropyl trimethoxysilane, N-(beta-aminoethyl)-3-aminopropyl triethoxysilane, N′-(beta-aminoethyl)-3-aminopropyl methoxysilane, or aminopropylsilsesquixoane.
After applying the uncured epoxy-based syntactic foam to the scaffold, the uncured epoxy-based syntactic foam is cured to produce the Interpenetrating Phase Composite foam. In one embodiment, the foam is cured at room temperature and atmospheric temperature. By varying the temperature, it is possible to cure the uncured epoxy-based syntactic foam at an increased rate.
In certain embodiment, molds can be used to produce the Interpenetrating Phase Composite in a variety of different shapes and sizes. In one embodiment, the method involves:
a. pouring the uncured the epoxy-based syntactic foam into a mold;
b. inserting the open-cell scaffold into the mold containing the uncured epoxy-based syntactic foam; and
c. curing the uncured epoxy-based syntactic foam to produce the Interpenetrating Phase Composite.
Exemplary procedures for making the Interpenetrating Phase Composites described herein using molds are provided in the Examples.
With reference now to the drawing figures, wherein like reference numbers represent corresponding parts throughout the several views, specific embodiments of the invention are described below.
In particular, example embodiments of IPC foam according to the present invention (such at the IPC foam depicted in
The metallic preforms can be utilized “as-is” from commercial suppliers or can be degreased with laboratory grade alcohol before being inserted into the liquid syntactic foam. Optionally, a degreased metallic preform can be coated with amino silane, γ-aminopropyltrimethoxysilane (H2C2H4NHC3H6Si(OCH3)3) to enhance adhesion between syntactic foam/epoxy and the metallic ligaments of the scaffolding/network/preforms. The adhesion between the metallic preform and syntactic foam is substantially stronger when the preform is pre-coated with amino silane (or other adhesion enhancers as desired by a user) than when the preform is used “as-is” or is merely degreased prior to be introduced to the liquid syntactic foam.
While numerous types of syntactic foams can be incorporated into IPC foams according to the present invention, epoxy-based syntactic foams containing different volume fractions of hollow soda-lime glass microballoons are typically utilized as shown in
SEM images showing polished surfaces of example embodiments of syntactic foam and IPC foam with 30% volume fraction of microballoons are seen in
The Interpenetrating Phase Composites described herein can be used in a number of different applications. In one embodiment, the composites can be in any article where it is desirable to absorb energy. In certain embodiments, the composites can be used as lightweight energy absorbing structural materials or core materials in sandwich structures used in aircraft structures, high-speed trains, automobiles as well as marine structures and submersibles.
The following examples are put forth so as to provide those of ordinary skill in the art with a complete disclosure and description of how the compounds, compositions, and methods described and claimed herein are made and evaluated, and are intended to be purely exemplary and are not intended to limit the scope of what the inventors regard as their invention. Efforts have been made to ensure accuracy with respect to numbers (e.g., amounts, temperature, etc.) but some errors and deviations should be accounted for. Unless indicated otherwise, parts are parts by weight, temperature is in ° C. or is at ambient temperature, and pressure is at or near atmospheric. There are numerous variations and combinations of reaction conditions, e.g., component concentrations, desired solvents, solvent mixtures, temperatures, pressures and other reaction ranges and conditions that can be used to optimize the product purity and yield obtained from the described process. Only reasonable and routine experimentation will be required to optimize such process conditions.
Epoxy-based syntactic foams containing different volume fractions (20%, 30% and 40%) of hollow soda-lime glass microballoons were processed. The method involved heating epoxy resin to 50° C. for approximately 45 min. Predetermined amount of microballoons (spherical hollow balloons of mean diameter approximately 60 μm and wall-thickness approximately 600 nm) were added into epoxy resin and the mixture was carefully stirred ensuring uniform distribution of the filler. Subsequently, an amine based curing agent was introduced and stirring was continued. The mixture was then placed in a vacuum chamber and evacuated down to −75 kPa (gage) pressure. Once this pressure was reached the vacuum was released and the chamber was returned to atmospheric condition. This process was repeated (about 8-10 times) until no air bubbles were observed in the mixture. (This method of cyclic vacuuming of the mixture was found to be more effective when compared to holding the vacuum continuously for a set period of time.) When the mixture showed a tendency to gel, it was transferred into a silicone rubber mold with a blind cylindrical cavity. The increased viscosity of the mixture prevented segregation of microballoons due to buoyancy forces. The mixture was then cured at room temperature for a period of 48 h and rested for over a week to obtain a macroscopically homogeneous and isotropic solid. The cylindrical sample was then machined to the required dimensions. Unless specified otherwise, in this work, the sample length and diameter were 20 mm and 26.7 mm, respectively.
The pressureless infiltration technique was used to produce the IPC foam. Commercially available open-cell aluminum foam (made of A16101-T6; pore density=40 ppi, relative density=9%, manufactured by ERG Inc., USA) was used as the scaffold for the IPC foam. The preform has a uniform cell size distribution resulting in an isotropic mechanical response at macro scales. The manufacturing of the IPC foam consisted of the following steps. A silicone rubber mold was first prepared with a blind cylindrical well of dimensions nearly close to the final sample dimensions. The syntactic foam (prepared as previously described) was then poured into the rubber mold just before the mixture started to gel. Subsequently a cylindrical aluminum preform of the required dimensions was slowly lowered into the cavity previously filled with uncured syntactic foam. This ensured good percolation of the uncured syntactic foam mixture into all the cells of the preform. The resulting IPC foam was then cured at room temperature for 48 hours before removing from the mold for machining. The cylindrical sample was subsequently machined to a length of 20 mm and diameter 26.7 mm.
Two different types of cylindrical IPC foam specimens were prepared. In the first type, the aluminum preform was used in ‘as-is’ state after degreasing it with laboratory grade alcohol. In the second type, the surface of the degreased aluminum preform was coated with amino silane, γ-aminopropyltrimethoxysilane (H2C2H4NHC3H6Si(OCH3)3). This coating was to enhance adhesion between syntactic foam/epoxy and the aluminum ligaments whereas the former produced a weaker adhesion between polymer and metal phases of the IPC foam. Some of the relevant properties of different phases of the IPC foam are listed in Table 1.
1supplied by Buehler, Inc., under the trade name ‘Epo-Thin’
2supplied by 3M Corp., under the trade name K-1 microballoons
A series of compression tests were carried out by the Applicants on syntactic and IPC foam specimens at room temperature using a MTS universal testing machine fitted with a 100 kN load cell. The tests were performed according to ASTM standard D-695 for plastics. A cross-head speed of 1.25 mm/min was used during the tests done in displacement control mode. Dry graphite powder was used as a lubricant between the platens and the specimen surfaces to minimize friction.
First, uniaxial compression tests were performed on syntactic foam samples of two different specimen length (L) to diameter (D) ratios—0.74 and 0.85. (The aspect ratio was altered by changing the length of the specimen while keeping the specimen diameter same.) The measured engineering stress-strain responses for syntactic foam specimens with 20% microballoon volume fraction and two aspect ratios are shown in
Next, the repeatability of compressive stress-strain responses of syntactic foam samples was studied.
The influence of volume fraction (Vf) of microballoons on stress-strain response of syntactic foam was also studied. A few representative stress-strain responses for three volume fractions (20%, 30% and 40%) are shown in
The elastic modulus and compressive strength decreased from 1595 MPa and 55.7 MPa, respectively for 20% volume fraction case to 1260 MPa and 36.7 MPa for 40% volume fraction case. The example foam samples SF-20 (Vf=20%), SF-30 (Vf=30%) and SF-40 (Vf=40%) show a linear elastic response up to strains of approximately 0.028, 0.031, 0.039, respectively. The plateau stress values in the three cases are 42 MPa, 33 MPa and 27 MPa for SF-20, SF-30 and SF-40, respectively. That is, the plateau stress decreases with increasing volume fraction of microballons. The onset of densification for the three cases is in the strain range of 0.3-0.5 with the lower value corresponding to the lower volume fraction of microballoons. Beyond this strain, stress increases with increasing strain. All specimens showed formation of inclined cracks at advanced stages of loading suggesting shear localization. This is consistent with previously known properties for syntactic foams.
In order to explain the failure behavior of syntactic foams, deformed specimens were sectioned and microscopically examined at a few select strain levels.
a & 8b show typical stress-strain curves for different IPC foam samples. These plots correspond to samples made of aluminum preform infiltrated with syntactic foam containing 20%, 30% and 40% volume fractions of microballoons.
For comparison, the compression response of an unfilled aluminum preform is shown as an inset in
Another comparison between the responses of IPC foam with silane coated and uncoated aluminum ligaments can be made from
The elastic modulus of the composite was determined using the initial linear portion of the measured stress-strain curves. The elastic modulus and the upper yield stress for IPC foam made from uncoated and coated aluminum preforms are quantified in Table 3 and are found to monotonically decrease with increasing volume fraction of microballons in the syntactic foam:
This behavior is consistent with the corresponding values of pure syntactic foam (see Table 2). From Table 3 it can also be noted that the elastic modulus and yield stress of IPC foam with silane coating is higher when compared with the corresponding uncoated preform for all volume fractions of microballoons in syntactic foam. As noted earlier, the increase in elastic modulus and compressive strength of silane coated preform can be attributed to improved wettability, which in turn enhances adhesion between the metal and polymer phases. The IPC foam is also found to have improved mechanical properties when compared with those for the respective syntactic foams.
In
Conventional cellular materials have found application in automotive and packaging industries due to their excellent energy dissipation characteristics. The cellular structure of these materials enables them to undergo large deformations in compression, enabling them to absorb considerable amounts of energy. Thus, improvements in energy absorption achieved by IPC foam samples when compared to the corresponding syntactic foam counterparts need to be highlighted. The energy absorbed per unit volume (U) can be found by evaluating the area under the stress-strain curve
where σ(∈) denotes uniaxial stress as a function of strain. The energy absorbed up to 50% strain are plotted as histograms in
Specifically, 48%, 53% and 49% increase in the absorbed energy per unit volume for IPC-S20, IPC-S30 and IPC-S40 relative to the conventional syntactic foam samples SF-20, SF-30 and SF-40, respectively, is indicative of the potential of IPC foams for energy dissipation applications. On the other hand, when IPC foam samples had an uncoated preform, the absorbed energy was modestly lower and was found to be 31%, 37%, 40% for IPC-20, IPC-30 and IPC-40 relative to SF-20, SF-30, and SF-40, respectively. Introduction of aluminum preform increases the overall weight of the composite and hence specific energy absorption (energy absorbed per unit mass) was also calculated. From
While the invention has been described with reference to preferred and example embodiments, it will be understood by those skilled in the art that a variety of modifications, additions and deletions are within the scope of the invention, as defined by the following claims.
This application claims priority to U.S. Provisional Patent Application Ser. No. 61/217,548, filed Jun. 1, 2009, which is hereby incorporated herein by reference for all purposes.
The research leading to this invention was funded in part by the U.S. Army Research Office, Grant No. W911 NF-08-1-0285. The U.S. Government has certain rights in this invention.
Number | Date | Country | |
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61217548 | Jun 2009 | US |