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    IOP PUBLISHING SMART MATERIALS AND STRUCTURES

    Smart Mater. Struct. 17 (2008) 055021 (7pp) doi:10.1088/0964-1726/17/5/055021

    Strain induced anisotropic properties ofshape memory polymer

    Richard Beblo and Lisa Mauck Weiland1

    Department of Mechanical Engineering and Material Science, University of Pittsburgh,

    660 Benedum Hall, Pittsburgh, PA 15261, USA

    E-mail: [email protected] and [email protected]

    Received 17 March 2008, in final form 30 June 2008

    Published 10 September 2008

    Online at stacks.iop.org/SMS/17/055021

    AbstractHeat activated shape memory polymers (SMPs) are increasingly being utilized in ambitious,

    large deformation designs. These designs may display unexpected or even undesirable

    performance if the evolution of the SMPs mechanical properties as a function of deformation is

    neglected. Yet, despite the broadening use of SMPs in complex load bearing structures, there

    has been little research completed to characterize how the material properties change upon

    application of large strain. The following is an experimental investigation into the strain

    induced anisotropic properties of the SMP Veriflex. It is found that under large uniaxial strain

    the SMPs stiffness in the transverse direction can be reduced as much as 86%, while the

    toughness in the axial direction may increase by an order of magnitude in some cases.

    A generalized analysis suggests that this trend should be expected for any SMP.

    1. Introduction

    Since their development in the late 1960s and early 1970s,

    engineered polymers such as shape memory polymers (SMPs)

    have been widely researched for their capability to recover

    from large amounts of strain as well as their ability to switch

    between relatively low and high moduli [13]. Their unique

    characteristics have made them attractive for several design

    concepts which rely on the polymers ability to soften, be

    deformed by relatively low force, and then harden as a

    new shape capable of carrying loads, possibly over several

    cycles. Such characteristics are possible through the use of an

    elastic segment and a transitioning segment. Above the glasstransition temperature Tg, the elastic segment dominates the

    material response, while below Tg, the transitioning segment

    crystallizes, dominating the material response.

    In the biomedical field, SMPs have been proposed

    as stents for the treatment of cardiovascular disease and

    aneurysms [4, 5]. Biodegradable formulations have also

    been developed for use as internal sutures, aiding in

    minimally invasive surgeries [6]. The automotive industry

    is implementing designs using SMPs in active air dams and

    aerodynamic control actuators for improved fuel economy

    and performance [7]. Further, SMPs are being considered

    in the aeronautical and astronautical fields in morphing1 Author to whom any correspondence should be addressed.

    aircraft wing structures as a skin allowing large in-plane

    deformations of the wing. The design goals of the latter

    are to create a class of military aircraft capable of multi-

    mission roles [8, 9]. In efforts to augment such designs, novel

    heating and cooling schemes have been developed, including

    magnetic nanoparticles [10, 11], both reducing the need for

    large and complex heating and cooling systems and improving

    the response time of the polymer.

    Heat activated SMPs are divided into categories based

    on their chemical makeup, the most common of which are

    polystyrene, polyurethane, and epoxy based polymers [12].

    The constitutive response of SMPs is best described by

    considering four discrete temperature regions as illustrated by

    figure 1. In the lowest temperature regime, or the glassy state,

    the small strain approximation is reasonable; hence a constant

    elastic modulus is typically assumed, such as in the generalized

    form of Hookes law,

    i =1

    E

    i

    j + k

    , i j =

    i j

    G, (1)

    where is the strain, E is the Youngs modulus, is the

    stress, is Poissons ratio, G is the shear modulus, is the

    shear stress, is the shear strain, and i , j , and k are any even

    perturbation of an orthonormal basis. In the two transition

    regions, time dependent temperature equations are deriveddescribing the assumed isotropic moduli of the polymer. For

    0964-1726/08/055021+07$30.00 2008 IOP Publishing Ltd Printed in the UK1

    http://dx.doi.org/10.1088/0964-1726/17/5/055021mailto:[email protected]:[email protected]://stacks.iop.org/SMS/17/055021http://stacks.iop.org/SMS/17/055021mailto:[email protected]:[email protected]://dx.doi.org/10.1088/0964-1726/17/5/055021
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    Figure 1. Heat activated shape memory polymer cycle.

    instance, from conservation of energy theory, the internal

    energy can be expressed as [13]

    u

    t =

    mnD

    mn +r

    q

    m,m, (2)

    which can then be related to the Youngs modulus, where

    is the density, u is the internal energy, t is time, D is a

    deformation rate tensor, r represents internal heat generation

    per unit mass, q represents the heat flux across the boundary,

    and m and n are indicial indices. The first term on the right-

    hand side of the equation is referred to as the stress power, and

    it accounts for the mechanical work done to the polymer. In the

    highest operating temperature regime, or the elastic region, the

    material response is viscoelastic, for which there are several

    accepted models including Maxwells model,

    Totalt

    = Dt

    + St

    = + 1

    Eddt

    , (3)

    where is the viscosity, and the subscripts D and S

    indicate damper and spring related quantities, respectively.

    Moreover, several mathematical models of varying complexity

    and accuracy have been proposed. There are two basic

    methodologies utilized in the development of constitutive

    models describing SMPs. The first employs the use of

    piecewise functions, breaking up the response of the polymer

    into the four distinct regimes illustrated by figure 1 and

    outlined in equations (1)(3). Such methods have been used

    by Barot et al, and have proven accurate under most loading

    conditions with the exception of being ill-suited to modelplastic strain below Tg [14]. Bhattacharyya et al have also

    proposed a model paralleling this methodology [15]. The

    second approach used to model SMPs makes assumptions such

    as the polymer being isotropic under all conditions in order to

    derive a single constitutive equation, for example the model

    proposed by Tobushi et al [16]:

    =

    E+ m

    y

    k

    m1

    k+

    + 1

    b

    c 1

    n

    s

    + , T (4)where the dot denotes a time derivative, m, b, and kare material

    parameters, the subscripts y and c represent yield and creeplimits respectively, s denotes unrecoverable quantities, T is

    temperature, and , and are the viscosity, retardation time,

    and the coefficient of thermal expansion respectively. Strictly

    speaking, the assumption of isotropy is not true; however,

    the resulting single thermoviscoplastic constitutive equation

    is useful for many applications where 3D modeling is not

    required. Such models as those developed by Tobushi et al

    [15, 16] are useful for unidirectional loading environments andmultiple-cycle modeling. Diani et al have also proposed a

    single equation constitutive model capable of 3D predictions;

    however, the model assumes the polymer to be isotropic below

    Tg and that all strain is elastic, and is thus incapable of

    modeling plastic deformation in the glassy state [17]. Other

    models proposing single equation constitutive relations include

    those by Liu et al [18] and Lin et al [19].

    Extensive experimental studies have also been performed

    characterizing the thermomechanical properties of SMPs,

    including changes in stiffness with respect to temperature and

    strain recovery capabilities [2022]. Gall et al have reported

    the storage and release of internal stress through a typical

    shape memory cycle of a composite of epoxy based SMP and

    dispersed SiC particles [23]. An SMPs ability to recover from

    nearly any amount of applied strain has been quantified as well

    as its creep characteristics under continuous loading [24, 25].

    Tobushi et al have conducted experiments indicating that

    the shape recovery characteristics of a polyurethane SMP

    foam are time and temperature dependent [25]. Yang et al,

    studying an ether based polyurethane SMP, have reported the

    effect of prolonged moisture exposure on the glass transition

    temperature [26, 27]. Applications and material characteristics

    of thin film SMP have also been reported [28, 29]. Poilane

    et al, for example, have confirmed macroscale test results of

    thin films of SMP using nanoindentation, bulge, and membranepoint deflection test techniques [28], while Tobushi et al

    have proposed using such thin film SMPs as passive choke

    devices for engines and customizable utensils for disabled

    patients [29].

    While each of the above models and experimental studies

    is well suited for its intended purpose, none appropriately

    addresses the anisotropies that occur at high strains in

    SMPs. Moreover, the anisotropies that arise in polymers

    in general when subjected to large strain have been well

    documented. For instance, refer to the classic works of

    Treloar et al [30] and Flory et al [31] involving rubber

    elasticity. More recent experimental studies continue tosupport this expectation. For instance, Arruda et al [32] have

    conducted experiments similar to those presented below on

    polycarbonate and polymethylmethacrylate specimens. Strain

    induced orientated crystallization has also been studied and

    modeled, and has been found to cause similar anisotropies in

    polyethylene terephthalate (PET) by Rao et al [33]. Below

    Tg, strain hardening in polycarbonate has been observed by

    Govaert et al, revealing a sinusoidal-like relationship between

    the yield stress and the angle between the investigated direction

    and the direction of alignment [34]. HAPEX, a substitute

    for bone having an isotropic tensile strength of 18 MPa,

    after being oriented through an extrusion process, has been

    found to become anisotropic, with tensile strengths of 80 and9 MPa in the direction of and perpendicular to the direction

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    of extrusion, respectively, by Bonner et al [35]. Experiments

    proving strain induced alignment of microdomain structures

    in polystyrene-block-polybutadiene-block-polystyrene (SBS)

    triblock copolymers have been conducted with the use of x-

    ray scattering techniques and transmission electron microscopy

    by Aida et al [36]. While the phenomenon of polymer chain

    alignment due to strain and its effect on mechanical propertieshas been well researched, differences between polymer

    systems substantiate the need for the direct experimental

    investigation of this effect in shape memory polymers. At

    least as significant is the need to ensure that end users of

    SMPs become alert to this generalized phenomenon, as this

    discussion is relatively absent from current SMP literature.

    The following work is an experimental investigation

    into the effect large strains have on the styrene based SMP

    Veriflex (a product of Cornerstone Research Group, LLC)

    above and below the glass transition temperature Tg. The

    experiments outlined in this work explicitly aim to quantify

    these anisotropies to aid in the design of structures requiring

    both morphing capabilities and multi-directional loading.

    Following the experimental results, a generalized modeling

    construct for anticipating the observed anisotropies is offered

    to further reinforce the expectation that similar anisotropies

    should be expected to evolve in other SMP (or any polymer)

    formulations.

    2. Experimental procedures

    Veriflex is a cross-linked thermoset copolymer manufactured

    in two parts: a resin and a hardener. Once mixed, the polymer

    can be cast into any shape as well as machined after curing.

    The manufacturer reports a glass transition temperature Tg of62 C.

    2.1. Sample preparation

    The resin and hardener are mixed per the manufacturers

    specifications. A medium vacuum, approximately 27 Hg, ispulled on the sample until there are no remaining air bubbles

    from mixing, while avoiding excess vacuum as this will remove

    styrene from the mixture. The uncured polymer is then poured

    into a steel mold conforming to the ASTM D638-03 type IV

    specimen standard. The mold, treated with a manufacturer

    supplied mold release, is then placed in a laboratory ovenat 75 C for 39 14

    h. The extended 314

    h as compared to

    the manufacturers specifications compensates for the thermal

    capacity of the mold.

    In the creation of the samples for characterizing axial

    response, the resulting 25 mm thick molded polymer is cut into

    4 mm thick specimens for the standard isotropic tensile tests.

    Each specimen is sanded with 200 then 600 grit sandpaper to

    remove all tool marks and ensure a flaw free test sample.

    In the creation of samples that are preconditioned with

    axial strain, the 25 mm thick molded polymer is heated well

    above Tg to 80C, strained, and cooled to below Tg prior

    to slicing. Each specimen is then sliced and sanded per the

    method above. Some of these samples are tested in thiscondition to characterize any changes in axial response as a

    result of preconditioning; the remainder are further conditioned

    for transverse characterization.

    Samples for characterizing transverse response are sliced

    from the preconditioned dog-bones such that only the

    traditional gage length remains. This results in rectangular

    specimens, as opposed to the preferred dog-bone style;

    however, use of a video extensometer to monitor deformationonly in the central portion of the sample minimizes the edge-

    effect error associated with this sample type.

    2.2. Experimental setup

    All tests are conducted with a screw driven MTI universal

    load frame under displacement control. Characterization of

    axial response is performed at a strain rate of 2 mm per

    minute to avoid viscous effects, resulting in a maximum

    starting strain rate of 4.5% per minute for unconditioned

    samples. Characterization of transverse response is performed

    at a rate of 0.25 mm per minute, resulting in a maximum

    starting strain rate of 3.5% per minute for conditioned samples.Ambient tests are conducted at room temperature, 23 C, usinga 2 kN Transducer Techniques load cell. Tests above Tg(reported to be 62 C) are conducted at 80 C using a 1 kNTransducer Techniques load cell. A Bemco FTU3.0-100x600

    UTM temperature/humidity chamber is used for environmental

    control. A Messphysik ME46-450 video extensometer is used

    to monitor axial and transverse deformation, with contrast

    lines drawn directly on the samples. Specimen dimensions

    are recorded with digital calipers, accurate to 0.01 mm.

    Experimental results are reported as true stress/strain values.

    3. Experimental results

    Tables 13 and figure 2 summarize the experimental results

    and include statistical errors as calculated using Students

    t-distribution; per ASTM D638-03, at least five tests are

    performed per reported measurement. Figure 2 is presented

    using representative true strain values measured from the

    original isotropic state before testing or any preconditioned

    strain is applied. This method results in the curves for the 40%

    and 70% preconditioned cases being offset (figure 2). This

    reporting strategy allows a direct comparison of the total strain

    applied to the sample beginning from the isotropic state. For

    the characterization of transverse response in preconditionedsamples, this strategy results in an initial offset to a negative

    strain due to the Poisson effect.

    While offsetting for preconditioning in the figures enables

    a convenient visual of the total linear deformation away from

    the isotropic state, this strategy may obscure the meaning

    of in-service performance. All tabulated results correspond

    with zeroed initial conditions for all tested samples. Table 1

    provides a summary of the measured material properties as

    functions of preconditioning, temperature, and direction. Here,

    the Youngs modulus of the specimens tested below Tg is

    defined as the slope of the linear portion of the stress/strain

    curve as seen in the top left and top right graphs in figure 2;

    the slope is measured between the strains of 0.25% and 1.0%.The Youngs modulus above Tg is reported as the initial slope

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    Figure 2. Representative stressstrain curves with offsets to illustrate preconditioning: axial testing below Tg (top left); transverse testingbelow Tg (top right); axial testing above Tg (bottom left); transverse testing above Tg (bottom right).

    Table 1. Experimentally determined Youngs modulus, yield stress, and Poissons ratio.

    Youngs modulus (MPa) Yield (MPa)Below Tg (23

    C) Below Tg (23 C) Poisson ratioPreconditioned

    strain (%) Axial Transverse Axial Transverse Axial

    0 1140 71 13.0 1.2 0.4840 1300 50 190 15 15.6 1.1 11.3 2.0 0.4770 1270 120 160 51 14.6 1.2 9.5 0.4 0.38

    Above Tg (80C) Above Tg (80 C)

    Preconditionedstrain (%) Axial Transverse Axial Transverse Transverse

    0 0.44 0.046 NA 0.4840 0.96 0.08 0.51 0.04 NA NA 0.4770 1.56 0.03 0.10 0.01 NA NA 0.38

    of the stress/strain graph at the beginning of the test, as seen in

    the bottom left and bottom right graphs in figure 2; the slope

    is measured between the strains of 0% and 25%. Poissons

    ratio is defined as the ratio of transverse strain to axial strain

    in the same stress/strain region as that used to calculate the

    Youngs modulus, where the video extensometer employed

    tracks the response in both directions throughout any given test.

    There is only modest variation in the Youngs modulus in the

    axial direction, with all experimentally determined values in

    the range of the manufacturers reported value of 1241 MPa.

    Similarly the yield stress, taken as the onset of the non-linear

    response, is relatively insensitive to preconditioning in the

    axial direction.

    However, the Youngs modulus in the transverse directionis seen to decrease by as much as 86%, falling from 1140 MPa

    initially to 160 MPa with 70% strain preconditioning. The

    yield stress is also observed to fall off by 30% in this case.

    No yield stresses are reported above Tg because, although the

    response is not linear to failure, there is no onset of plastic

    deformation; this is consistent with the polymers rubber-like

    behavior in the soft state and its ability to recover from nearly

    any applied strain up to failure.

    Also evident from figure 2, and summarized in table 2,

    is the sometimes substantial increase in failure strain upon

    application of strain preconditioning. Below Tg there is a

    significant increase in the failure strain in the axial direction. In

    fact, with preconditioning, the SMP is capable of withstanding

    nearly as much strain below Tg as it is above Tg. Accounting

    for the preconditioned strain, the maximum strains at failurein the axial direction below Tg for the 40% and 70%

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    Table 2. Failure strain as a function of preconditioned strain (zero offset).

    Axial TransversePreconditionedstrain (%) Minimum (%) Maximum (%) Minimum (%) Maximum (%)

    0 5.2 31.2 5.2 31.2Below Tg (23

    C) 40 67.7 82.3 36.6 47.6

    70 11.4 61.2 23.5 32.30 110.9 119.1 110.9 119.1

    Above Tg (80C) 40 58.3 138.4 78.0 85.8

    70 29.1 40.2 168.1 176.4

    Table 3. Modulus of toughness as a function of preconditioned strain.

    Axial (MJ m3) Transverse (MJ m3)Preconditionedstrain (%) Minimum Maximum Minimum Maximum

    0 0.9 4.6 0.9 4.6Below Tg (23

    C) 40 15.1 20.0 2.7 5.070 1.8 13.9 1.0 2.0

    Above Tg (80C) 0 0.47 0.57 0.47 0.57

    40 0.18 1.27 0.20 0.2870 0.04 0.15 0.08 0.12

    preconditioned cases become 123% and 130%, respectively,

    which is comparable to the isotropic above Tg case having a

    maximum failure strain of 120%.

    Directly related to the amount of strain the polymer

    is capable of withstanding before failure is the modulus of

    toughness, presented in table 3. As is evident, below Tg the

    modulus of toughness in the axial direction is increased by

    more than an order of magnitude with strain preconditioning.

    4. Discussion

    An SMP is frequently employed for its ability to sustain large

    strain. More specifically, an SMP is often considered desirable

    for design because it may be warmed, subjected to substantial

    deformation with low forces, and then locked into the new,

    load carrying configuration at a lower temperature. This shape

    may be expected to support complex loads. The foregoing

    experimental procedure employs strain preconditioning as a

    means to explore the load carrying capability of the newly

    locked-in shape.

    Based on the experimental results of the previous section,for simple uniaxial design strategies it is appropriate to treat

    the Youngs modulus as a constant below Tg. Further, while

    the stiffness above Tg increases by a factor of three over the

    range of preconditioning considered, as compared to the cold

    state stiffness it may be appropriate to also treat this value of

    Youngs modulus as a constant for uniaxial loading. However,

    in SMP based designs carrying complex loads, the foregoing

    clearly illustrates that assuming constant, isotropic stiffness

    values above and below Tg would be ill-advised. Similarly, any

    design that relies on SMP toughness may display unexpected

    performance; in fact, in the case of toughness the material may

    be under-utilized.

    The following explanation is offered for the observedanisotropic response. It is proposed that during the

    preconditioning above Tg the energy required for shear

    between two adjacent polymer chains is greatly reduced,

    allowing them to slide relative to one another and partially

    align. This proposition is consistent with the partial polymer

    chain alignment reported for other polymer systems at large

    strains [20]. Once cooled, the response of the polymer in the

    axial (aligned) direction will be dominated by the deformation

    of the polymer chain covalent bonds. This is expected to

    correspond with an increase in stiffness, but more importantly,the amount of energy required to break these aligned covalent

    bonds will become significant.

    Consider next the response in the transverse direction. It

    can be argued intuitively that, if partial alignment results in

    a stronger material in the aligned direction, then the cross-

    links that enabled this alignment are necessarily less able to

    support load. However, this intuitive argument alone fails to

    adequately address the substantial degradation in transverse

    stiffness. In addition, however, this point may also be argued

    from Boltzmann statistical thermodynamics first principles.

    If it is assumed that rotation about a given polymeric bond

    is unrestricted, then the Helmholtz free energy is strictly a

    function of the entropy, where the entropy is given as

    S(r) = c + kln P(r), (5)

    where c is a constant of integration, k is Boltzmanns constant,

    and P(r) is the probability density function defining the

    distance between polymer chain cross-links. One relatively

    simple way to explore this is via the three-chain rule, which

    essentially assumes that in the virgin state the polymer chains

    will tend to align with each of the Cartesian axes [30],

    S= 3

    S(ro) + 2S(ro1/2) 3S(ro)

    , (6)

    where S is the change in entropy associated with an applieddistortion, is the number density of network chains, r0 is the

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    root mean square of the distance between cross-links and =L/L i is the relative length of the sample upon deformation.

    The first parenthetical term of equation (6) corresponds with

    the axial response; the second parenthetical term corresponds

    with the transverse response; the final parenthetical term

    corresponds with the virgin state. The nominal stress f and

    corresponding modulus [ f] of the system are then expressedas [37]

    f = T

    S

    T

    f= f

    2 , (7)

    where T is the temperature. For the general case presented

    here, a normal distribution function, such as equation (8), is

    utilized for P(r), the chain length probability density function.

    P (r) = 1

    2exp

    (x )

    2

    22

    , (8)

    where is the standard deviation, is the expected value,

    and x becomes r0 in the axial direction and r01/2in the transverse direction, as indicated in equation (6).

    Substituting equation (8) into equation (5) and subsequently

    into equation (6) yields

    Saxial

    = kr0

    2(r0 ) (9)

    Stransverse

    = kr0

    22

    r0

    1/2

    , 3/2 (10)

    where the entropic response with respect to distortion is

    considered for the respective axial and transverse directions. In

    this form, it is relatively easy to envision that the magnitude of

    the axial term will increase with increasing axial deformation as all other terms in the expression are positive constants.

    Further manipulation of equations (9) and (10) via equation (6)

    only serves to multiply the expressions by terms that will

    cancel in the resulting ratio of interest,

    faxial =

    2

    r03 2

    r0 1/2

    ftransverse . (11)

    Because r0 and are necessarily positive and is greater

    than 1 for our tensile preconditioning, the numerator will

    be larger than the denominator, yielding a coefficient greater

    than 1. This supports the experimental observation that themodulus in the transverse direction is smaller than in the axial

    direction with increasing strain. Further, because the terms in

    the numerator are of higher order than the denominator, the

    transverse properties decrease relative to the axial properties at

    a correspondingly increased rate.

    The details of the above discussion may be easily

    manipulated. For instance, considerable detail could

    be introduced to accommodate the multiphased nature of

    Veriflex in comparison to the rubber elasticity basis of this

    development; the Johnson family of distributions might have

    been employed [38]; or more formally developed orthotropic

    constitutive equations may have been offered [39]. In

    addition, it should be noted that the above theory is knownto have increasingly significant errors above extension ratios

    between 2 and 2.5, depending upon the polymer system [30].

    However, despite the simplistic application of statistical

    thermodynamics, the characteristic qualities of the analysis are

    fixed. Thus first principles support the observed, substantial

    degradation in transverse stiffness with the introduction of

    preconditioning. The significance of choosing this highly

    generalized construct is that it may be reasonably argued thatthe experimentally observed anisotropic trends in Veriflex

    should be expected in any SMP, and for that matter, any

    polymer employed in large strain applications.

    5. Conclusions

    With shape memory polymers being aggressively considered

    for high strain applications, it is becoming increasingly

    important that their three-dimensional characteristics be

    quantified. When first partially aligning the polymer chains

    with strain preconditioning above Tg, such as is likely tooccur in high strain applications, substantial variations in the

    fundamental material properties are observed. These include

    substantially decreased transverse stiffness and substantially

    increased axial toughness (in some cases an order ofmagnitude). While the above results may necessitate the

    use of somewhat more complex material models during the

    material design process, the ability to manipulate directional

    material stiffness and toughness could also become a powerful

    design tool in itself. The foregoing offers insight into how the

    property variation will manifest itself. Moreover, because the

    physical mechanisms proposed for the observed response are

    argued from principles applicable to any polymer material, theexperimental trends presented in this report are not expected to

    be limited to the specific case of Veriflex.

    Acknowledgments

    The authors would like to acknowledge Dr Clark, for

    his assistance and expertise; HRL Laboratories, LLC, for

    their knowledge of shape memory polystyrenes and aid in

    sample preparation techniques, and CRG Industries, LLC, for

    supplying Veriflex and counsel.

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