8192
Macromolecules 2000, 33, 8192-8199
Composites Prepared by the Anionic Polymerization of Ethyl
2-Cyanoacrylate within Supercritical Carbon Dioxide-Swollen
Poly(tetrafluoroethylene-co-hexafluoropropylene)
Edward Kung, Alan J. Lesser,* and Thomas J. McCarthy*
Polymer Science and Engineering, University of Massachusetts, Amherst, Massachusetts 01003
Received April 20, 2000; Revised Manuscript Received July 28, 2000
ABSTRACT: Supercritical carbon dioxide (SC CO2) was used as an aid in fabricating polymer/polymer
composites. Using a two-stage process, ethyl 2-cyanoacrylate (ECA) monomer was anionically polymerized
within poly(tetrafluoroethylene-co-hexafluoropropylene) substrates. The composite fabrication process
involved first infusing triphenylphosphine (the initiator) into the substrate using SC CO2. In the second
step, monomer was introduced (again using SC CO2) to the substrate. As the monomer absorbed into the
initiator-containing substrate, it polymerized. The composite surfaces were characterized using surfaceselective techniques. The mechanical performance of the composites was determined by measuring the
adhesive fracture toughness of the composites. The locus of failure of fractured interfaces of composites
with epoxy was determined by X-ray photoelectron spectroscopy.
Introduction
Supercritical carbon dioxide (SC CO2) has been used
in the fabrication of polymer-polymer composites. We
have demonstrated the viability of infusing monomers
into a variety of polymer substrates and subsequently
radically polymerizing the monomer within the SC CO2swollen substrates.1,2 Polystyrene/polyethylene composites, in particular, showed very interesting phase morphologies that resulted in enhanced mechanical performance when compared to conventional melt-blended
systems.3 Thus far, our research has focused on radical
synthesis and bulk characterizations. This paper will
discuss research on an anionically polymerized system
and the interface properties of the final composites.
The polymerization of functional monomers in the
surface region of SC CO2-swollen fluoropolymer substrates allows modification of the surface properties of
those substrates, producing composite surfaces. Such a
technique is an alternative to the rather harsh and
hard-to-control techniques usually employed to modify
fluoropolymer surfaces. The introduction of nitrile and
ester groups can be effected by the polymerization of
cyanoacrylate monomers. Polycyanoacrylates are most
commonly synthesized by anionic polymerization, although radical polymerization can also be employed.4,5
The anionic polymerization of cyanoacrylates is an
extremely fast and robust living polymerization. These
traits, which will be discussed below, should allow for
facile synthesis of the target surface composites. In a
CO2 medium, however, an anionic polymerization may
be problematic.
CO2 terminates most anionic polymerizations. CO2 is
susceptible to nucleophilic attack and will react with
anionic initiators or actively propagating carbanions.
For most anionic polymerization systems, the resulting
carboxylate chain end is normally not reactive enough
to continue propagation with monomers or to add to
another CO2 molecule (no homopolymerization of CO2
is known to occur).6 Cyanoacrylate monomers, with
electron-withdrawing nitrile and ester substituents, are
extremely reactive and can be polymerized by very weak
nucleophiles (e.g., amines and phosphines). Anionic
cyanoacrylate polymerizations are also known to be
extremely difficult to terminate. Pepper investigated the
stability of (poly)cyanoacrylate anions by calorimetrically measuring the heat evolved with the successive
addition of aliquots of monomer after the additions of
potential terminating agents to a living reaction mixture.4 It was found that the polymerizations of cyanoacrylates are virtually unaffected by the addition of
oxygen, water, and CO2. Only the addition of a strong
acid (hydrochloric acid) terminated the polymerization.
More recently, Johnston and Pepper studied the
stability of polycyanoacrylate anions spectroscopically.7
The ultraviolet spectrum of a living polycyanoacrylate
anion possesses an absorption centered at ∼250 nm. It
was found that, upon the addition of CO2 to the reaction
mixture, the absorption at 250 nm disappeared nearly
instantaneously. This result suggests that CO2 reacts
with the cyanoacrylate anion to form a different moiety
(presumably a carboxylate anion). Johnston and Pepper
did not attempt to identify the carboxylate anion but
simply stated that the polymer was nearly instantly
terminated by CO2.
The calorimetric data suggest that despite the existence of the terminal carboxylate anions, implied by the
spectroscopic data, cyanoacrylate monomer continues to
polymerize. For this to occur, either the carboxylate
anion decarboxylates and re-forms the cyanoacrylate
anion to continue propagation or the carboxylate anion
adds to new monomer to continue propagation. Acetate
anions are known to initiate polymerization of cyanoacrylates.8 Scheme 1 shows how either of these two
possibilities occur. “I” is a nucleophilic initiator such as
an amine or phosphine. If path B occurs, then ester
moieties will be incorporated into the backbone of the
polymer. This path requires that the kinetics of the
cyanoacrylate anion attack on CO2 are competitive with
normal homopolymerization (which is known to be very
rapid). If the formation of carboxylate anions is competitive, the equilibrium constant (carboxylation-decarboxylation) and the relative rates of paths A and B will
dictate which or if both of the two outcomes occur.
Running an anionic polymerization of a cyanoacrylate
in fluid carbon dioxide should increase the potential for
copolymerization. The increased concentration of CO2
10.1021/ma000695o CCC: $19.00 © 2000 American Chemical Society
Published on Web 10/07/2000
Macromolecules, Vol. 33, No. 22, 2000
Scheme 1
(CO2 now being the solvent) should tend to shift the
equilibrium shown in Scheme 1 toward the carboxylate
anion. Also, increasing the CO2 concentration will
increase the probability of a cyanoacrylate anion finding
a CO2 molecule to attack before it encounters another
cyanoacrylate monomer.
Before we attempted to synthesize polymer composites using cyanoacrylates in SC CO2, we established
what product was formed by the anionic polymerization
of cyanoacrylates in a CO2 medium. We addressed this
issue by examining the polymerization of ethyl 2-cyanoacrylate (ECA) in liquid CO2. Once this issue was
resolved, we synthesized composites of poly(ethyl 2-cyanoacylate) (PECA) and poly(tetrafluoroethylene-cohelfluoropropylene) (FEP) and characterized the surfaces of the composites.
We modified the technique that had been used for the
radical polymerization of styrene within substrates.1-3
Shown in Scheme 2 is the strategy for synthesizing
these composites. First, a polymer substrate is soaked
in a SC solution of CO2 containing a nucleophilic intiator
(pyridine or triphenylphosphine). Then the system is
vented, trapping the initiator within the substrate. The
substrate is then introduced to a SC solution of CO2 and
ECA monomer. As the monomer is absorbed into the
substrate and the initiator begins to desorb from the
substrate, the two reactants meet within the upper
surface regions of the substrate. As the polymerization
proceeds, further outward diffusion of the new polymer
does not occur. The resulting product possesses a
composite surface. Exactly where within the substrate
the secondary polymer forms depends on the relative
diffusion rates of monomer into the substrate and
initiator out of the substrate.
Experimental Section
Materials. Ethyl 2-cyanoacrylate (ECA) was supplied by
Loctite and used without further purification. Poly(tetrafluoroethylene-co-hexafluoropropylene) was supplied by DuPont
(Teflon FEP 1000A) as 10 mil (nominally) thick sheets. The
FEP was cleaned by sonication in HPLC grade tetrahydrofuran
(THF) at 60 °C for 24 h. The two initiators, pyridine (anhydrous, 99.8% pure) and triphenylphosphine (99% pure), were
purchased from Aldrich. The pyridine was distilled under dry
nitrogen from calcium hydride and stored over molecular
sieves. The triphenylphosphine was recrystallized three times
from ethanol and dried under vacuum. THF (anhydrous, 99.9%
pure) that was used for conventional polymerizations was
purchased from Aldrich and distilled as needed under nitrogen
from purple sodium benzophenone dianion. Carbon dioxide
(Coleman grade, 99.99% pure) was purchased from MerriamGraves and further purified through columns of activated
alumina (LaRoche Industries) and a copper catalyst (Engelhard Q-5) to remove water and oxygen, respectively. The CO2
Polymerization of Ethyl 2-Cyanoacrylate 8193
Scheme 2
was compressed using a motorized high-pressure screw pump
(Isco model 100DM).
Conventional ECA Polymerizations in THF. All glassware was base bathed, acid bathed (2.0 M aqueous sulfuric
acid), and then thorough washed with clean water and finally
dried at 120 °C. All reagent handling and reactions were
conducted under a dry nitrogen atmosphere at 23 °C. Using a
plastic syringe, an aliquot of ECA monomer was transferred
to a glass reaction vessel containing THF. In a separate vessel,
an initiator solution of a predetermined concentration of
pyridine in THF was prepared. While the monomer solution
was vigorously stirred, a predetermined amount of pyridine/
THF solution was syringed into the reaction flask. The system
was allowed to react for 1 h. The product was recovered by
precipitation in acidified methanol and subsequent filtration.
ECA Polymerizations in Carbon Dioxide. All reactions
were carried out in high-pressure stainless steel vessels. All
parts of the vessels were washed in clean acetone, acid bathed
(2.0 M aqueous sulfuric acid), then thoroughly rinsed in clean
water, and finally dried at 120 °C. Two vessels were used per
reaction: a larger reaction vessel (22 mL) and a smaller
initiator vessel (8.5 mL). All reactions were conducted at 23
°C. Using a plastic syringe, an aliquot of ECA monomer was
transferred to the reaction vessel. This vessel was then sealed
and filled with liquid CO2 to a pressure of 102 atm. A
predetermined amount of pyridine was transferred to the
initiator vessel. This vessel was then sealed and filled with
liquid CO2 to 204 atm. The concentrations of the ECA/CO2 and
pyridine/CO2 solutions were determined gravimetrically. The
two vessels were then connected by a 2 in. long stainless steel
nipple. Under vigorous agitation using a vortex mixer, the two
vessels were opened, allowing some of the contents of the
initiator vessel to flow into the reaction vessel as the pressure
difference between the two vessels equilibrated. The two
vessels were then closed and separated. The reaction vessel
was then weighed to determine the mass of pyridine/CO2
solution transferred into the reaction vessel.
Polymer Characterization. 13C NMR spectra were recorded in deuterated acetone using a Bruker DPX 300 spectrometer. All chemical shift values are reported in ppm relative
to tetramethylsilane. IR spectra were obtained from films
solvent-cast on potassium bromide plates using a Bio-Rad FTS
175C spectrometer. The refractive index increment of the
PECA in acetone was measured using a Photal RM-102A
differential refractometer. Molecular weights of the polymers
were measured using gel permeation chromatography (GPC)
through Polymer Laboratories PLgel columns with a Wyatt
Technology DAWN DSP-F light scattering detector. Acetone
was the GPC solvent.
Composite Synthesis. All composite syntheses were carried out in 22 mL high-pressure stainless steel vessels. The
vessels were prepared in the same manner described above.
The composite preparations required two steps, each using two
separate 22 mL vessels. All preparations were conducted at
40 °C.
8194
Kung et al.
In the first step (step I), the first vessel (vessel I) was
charged with a preweighed sample of FEP and an aliquot of
initiatorseither pyridine or triphenylphosphine. This vessel
was then sealed, tared, and filled with SC CO2 at 40 °C to a
pressure of 200 atm. The concentration of the initiator/CO2
solution was determined gravimetrically. Vessel I was then
vigorously agitated on a vortex mixer and allowed to soak at
40 °C for 24 h in a heated water bath. At the end of the intiator
soak period, the vessel was vented and the FEP specimen
removed. The specimen was rinsed throroughly with copious
amounts of clean acetone to remove any adsorbed initiator and
blown dry with nitrogen. To obtain an approximate mass
uptake of the initiator into the FEP, a UV-vis spectrum of
the specimen was obtained using a Perkin-Elmer Lambda 2
spectrometer with a virgin FEP specimen as the reference.
In the second step (step II), the specimen was placed in the
second vessel (vessel II) along with an aliquot of ECA
transferred using a plastic syringe. Vessel II was then sealed,
tared, and filled with SC CO2 at 40 °C to 200 atm. The
concentration of the monomer/CO2 solution was determined
gravimetricallly. Vessel II was then vigorously agitated on a
vortex mixer and allowed to soak at 40 °C for various reaction
times. At the end of the reaction period, the vessel was vented,
and any unreacted monomer leaving the vessel during the
venting was noted. The specimen was removed and placed in
a vial and allowed to sit for 24 h before any analysis was
conducted.
For comparative purposes, pure PECA specimens were
prepared on pieces of clean silicon wafers by a vapor deposition
technique developed by Woods et al.9 The silicon wafers were
dipped in pyridine and blown dry with nitrogen gas. These
substrates were then suspended in a polypropylene container
above a pool of ECA monomer that was heated to 40 °C. Within
a minute, a relatively uniform layer of PECA forms on the
surface of the silicon.
Surface Characterization. Surface compositions of the
composite specimens were investigated using several surface
analytical techniques. Attenuated total reflectance (ATR) IR
spectroscopy was performed using a Bio-Rad FTS 175C
spectrometer and a 45° germanium ATR element. X-ray
photoelectron spectroscopy (XPS) was performed on a PerkinElmer-Physical Electronics 5100 spectrometer using Mg KR
X-rays. All XPS data were collected at takeoff angles of 15°
and 75° (between the specimen surface and the detector).
Advancing and receding contact angles for both water (deionized to 18 MΩ) and hexadecane (Aldrich, 99% pure) were
obtained using a Rame-Hart telescopic goniometer and Gil´
mont syringes.
Mechanical Characterization. The mechanical integrity
of the composites was determined by measuring the fracture
strength in cleavage of adhesive joints between the composites
and metal. The adhesive joints were formed by sandwiching
composite specimens between two metal strips coated with
epoxy to form double-cantilever beam (DCB) specimens. The
epoxy adhesive is a consumer grade epoxy from Devcon (2 Ton
Clear) that was prepared and applied in accordance with the
recommendations of the manufacturer. The metal beams are
stainless steel strips with dimensions 0.307 mm × 12.5 mm
× 70.5 mm; they were cleaned with acetone prior to applying
the epoxy. The DCB specimens were loaded to failure on an
Instron 1123 testing machine fitted with an Instron 2525-807
load cell ((100 N) at a 2 mm/min crosshead speed. From the
load-displacement curves, the critical loads for failure and the
compliances of the specimens were noted.
Results and Discussion
Polymerization in CO2. The polymerizations conducted in liquid CO2 were precipitation polymerizations.
The initial ECA/CO2 solutions, when the systems were
observed in a high-pressure view cell, were clear and
colorless. The view cell was illuminated to allow observations of the transmitted light. As the polymerizations
proceeded, the systems became hazy and changed from
Macromolecules, Vol. 33, No. 22, 2000
Figure 1. 13C NMR spectrum of polymer synthesized in liquid
CO2 showing clean homopolymerization of ethyl 2-cyanoacrylate.
colorless to light yellow and then to dark orange in color.
Gradually, the hazy orange solution became dark and
colorless and filled with large particles that grew in size
until the view cell became completely occluded. The color
developments are most likely due to scattering effects
caused by small polymer particles suspended in the CO2.
The final polymer is a fluffy white product.
Copolymerization? The IR spectrum of ECA monomer was compared to those of the products formed by
polymerizations in THF and CO2. Both products exhibit
the loss of vinyl vibrations at 3128 cm-1 (asymmetric
sp2 CH2 stretching) and 1615 cm-1 (CdC stretching).
The nitrile vibration at 2246 cm-1 (CtN stretching) is
shifted to a slightly higher frequency, and the intensity
is decreased due to the loss of conjugation with the vinyl
moiety. The product synthesized in THF is expected to
be pure homopolymer PECA. By IR, the product formed
in CO2 is indistinguishable from the homopolymer
prepared in THF.
Figure 1 shows the 13C NMR spectrum of the product
that was synthesized in CO2. The spectrum matches the
spectrum for pure PECA found in the literature with
signals at δ 166 (carbonyl carbons), 115 (nitrile carbons),
44 (main chain methylene and quaternary carbons), 64
(side group methylene carbons), and 14 (side group
methyl carbons).10 If CO2 were incorporated into the
main chain of the polymer to any significant extent,
separate signals from main chain carbonyl carbons and
shifted signals from main chain methylene and quaternary carbons would be expected. The shifted signals
would arise from cyanoacrylate monomer units bonded
to electron-withdrawing CO2 monomer units. The extremely strong signals at δ 206 and 30 are due to
deuterated acetone. The spectra of products synthesized
in THF were identical to that shown in Figure 1. The
NMR data concur with the IR results that copolymerization does not occur under the conditions used for
synthesis.
Molecular Weights. GPC with a light scattering
(LS) detector was employed for molecular weight determination. Differential refractometry gave the refractive index increment, dn/dc, for PECA in acetone to be
0.1159 mL/g. Table 1 summarizes the results of the
polymerizationssshowing conditions, molecular weights,
and yields. Regardless of the solvent employed, unlike
truly ideal living anionic polymerizations, the measured
molecular weights are much higher than the theoretical
values determined by the initial monomer-to-initiator
ratio, [M]0/[I]0. Also, the polydispersity ratios, Mw/Mn,
are not nearly as narrow as those found in ideal living
polymerizations. The results of this investigation agree
with the conclusions found by other researchers for
Macromolecules, Vol. 33, No. 22, 2000
Polymerization of Ethyl 2-Cyanoacrylate 8195
Table 1. Results of ECA (M) Polymerizations by Pyridine
(I) in CO2 and THF at 23 °C
10-3Mnb 10-3Mn
yield
sol- 103[I]0
no. vent (mol %) [M]0/[I]0a (theor) (GPC/LS) Mw/Mn (%)
1
2
3
4
5
6
7
CO2
CO2
CO2
CO2
CO2
THF
THF
36.3
26.7
8.3
1.5
1.2
27.4
8.4
28
38
120
656
830
38
121
3.5
4.7
15.1
82.1
103.9
4.7
15.1
670
770
790
1150
3490
1780
1880
2.0
1.5
1.4
1.7
1.3
1.2
1.6
91.4
85.5
89.8
86.7
80.0
82.8
81.4
a Initial monomer concentration is the same for all reactions,
[M]0 ) 1.0 mol %. b Mn(theor) assumes complete initiation, i.e., )
([M]0/[I]0)(monomer MW).
pyridine-initiated polymerizations of cyanoacrylates and
indicate slow and incomplete initiator utilization.11-14
Composite Components. The virgin FEP specimens
used in this study are translucent in appearance/and
possess a density of 2.14 g/mL. XPS analysisof the FEP
showed that the starting material is clean and consists
of approximately 33% carbon and 66% fluorine (F/C )
2) as expected; a spectrum of FEP is displayed in Figure
2. The titanium signal may be from some additive(s) in
the polymer. Water contact angles for FEP are θA/θR )
121°/99°; hexadecane contact angles for FEP are θA/θR
) 55°/36°.
From XPS analysis, PECA consists of 69% carbon,
20% oxygen, and 11% nitrogen (O/N = 2); a spectrum
is displayed in Figure 3. Water contact angles for PECA
are θA/θR ) 78°/55°; hexadecane contact angles for
PECA are θA/θR ) 3°/0°. For both water and hexadecane,
the contact angles are reasonable for a substrate that
contains polar nitrile and ester moieties.
Composites Using Pyridine as Initiator. Pyridine
was used as one of the initiators and was infused into
the FEP substrates during step I of the fabrication
technique. The UV spectra for FEP specimens soaked
in 2.6 wt % and 0.5 wt % solutions of pyridine in CO2
are shown in Figure 4. Using a literature value for the
extinction coefficient of pyridine (1995 L mol-1 cm-1 at
250 nm),15 the concentration, c, of pyridine loaded into
the FEP specimens can be estimated using the BeerLambert-Bouguet law. The specimens were 0.0232 cm
in thickness. The specimen soaked in the 2.6 wt %
solution of pyridine/CO2 had a concentration of ap-
proximately 0.022 M (or approximately 0.081 wt %), and
the specimen soaked in the 0.5 wt % solution had a
concentration of approximately 0.0068 M (or approximately 0.014 wt %).
The specimens soaked in either 2.6 wt % or 0.5 wt %
pyridine/CO2 solutions did not produce composites during step II of the fabrication technique. In both cases,
the reaction time was 24 h, and after the reaction period,
the specimens were found to be encased in a thick layer
of foamed PECA. The PECA foam could be peeled off
the FEP substrates, and the underlying substrates did
not exhibit any change in mass (i.e., no mass uptake of
PECA into the FEP). It was concluded that the diffusion
of pyridine out of the substrate is much faster than the
diffusion of ECA monomer into the substrate and that
polymerization occurred completely outside the substrate. All of the monomer was consumed in the
“external” polymerization.
Composites Using Triphenylphosphine as Initiator. Triphenylphosphine was also used as an initiator and, like pyridine, was infused into the FEP substrates during step I of the fabrication technique. The
UV spectrum for a FEP specimen soaked in a 0.9 wt %
solution of triphenylphosphine in CO2 is shown in
Figure 5. Using the same method as in the pyridine
system, the concentration of triphenylphosphine in FEP
after step I was estimated. A literature value for the
extinction coefficient of triphenylphosphine is 11 000 L
mol-1 cm-1 at 261 nm.16 The concentration of triphenylphosphine in FEP was appoximately 0.00061 M
or approximately 0.0075 wt %.
Unlike the pyridine system, the triphenylphosphine
system produced composites in step II. Composites were
synthesized using three reaction times: 6, 24, and 49
h. In all cases, the composite specimens were not
encased in PECA. The specimens remained translucent
although slightly more turbid than virgin FEP. Also,
the specimens gained mass and grew in dimension, both
due to the uptake of PECA. The incorporation of PECA
in FEP increased with increasing reaction time, as is
shown in Table 2. Polymerization of monomer in the
fluid phase (outside the substrate) did not occur. Polymerization took place only within the FEP substrates.
Figure 2. XPS spectrum of FEP obtained at a 15° takeoff angle between the specimen and the detector.
8196
Kung et al.
Macromolecules, Vol. 33, No. 22, 2000
Figure 3. XPS spectrum of PECA obatined at a 15° takeoff angle between the specimen and the detector.
Figure 4. UV spectra of FEP specimens soaked in supercritical solutions of pyridine/CO2 at 40 °C and 200 atm for 24 h:
(a) soaked in 2.6 wt % pyridine/CO2; (b) soaked in 0.5 wt %
pyridine/CO2. Specimens were 0.0232 cm thick.
Chemical characterization of the surface of the specimens showed that the materials are composites. Comparisons can be made between pure FEP, pure PECA,
and the composites. In all subsequent references, the
composites are designated PECA/FEP-X, where X is the
reaction time used in step II of the fabrication technique.
The ATR IR spectra of virgin FEP, PECA/FEP-24, and
PECA/FEP-49 are compared in Figure 6. The XPS
spectra for PECA/FEP-24 and PECA/FEP-49 are provided in Figures 7 and 8. The elemental compositions,
as determined by XPS, are tabulated in Table 3. The
nitrogen, oxygen, and carbon contents increase and the
fluorine content decreases with increasing reaction time.
The XPS results, however, show a lower content of
PECA in the upper 10-50 Å of the specimens compared
with the gravimetrically determined compositions shown
in Table 2. The hexafluoropropylene comonomer content
in FEP is generally 10-12 wt %.17 Assuming that the
FEP material is made up of 12 wt % hexafluoropropylene, then the chemical formula for an average FEP
repeat unit is C2.075F4.150 with a (repeat unit) molar mass
of 103.77 g/mol. The chemical formula for a PECA
repeat unit is C6H7NO2 with a molar mass of 125.13
Figure 5. UV spectra of a FEP specimen soaked in a
supercritical solution of 0.9 wt % triphenylphosphine/CO2 at
40 °C and 200 atm for 24 h. Specimens were 0.0232 cm thick.
Table 2. Mass Uptake and Composition of PECA into
FEP as a Function of Reaction Time for the
Triphenylphosphine System
reaction time (h)
mass uptake (%)
composition (wt %)
6
24
49
19.4
31.2
69.9
16.3
23.8
41.1
g/mol. Using the nitrogen and fluorine concentrations
determined by XPS and the chemical formulas of the
repeat units of the component polymers, the mass
compositions of the specimens within the sampling
depth of the XPS experiments can be calculated. These
surface mass compositions are tabulated in Table 4.
Contact angle data are tabulated in Table 5. As might
be expected, PECA-24 is more like FEP than PECA/
FEP-49. The advancing water contact angle is higher
for the composite specimens than pure FEP. This
indicates a mixed hydrophobic (FEP) and hydrophilic
(PECA) surface. As the water droplet is advanced over
hydrophilic domains, the contact line pins causing the
contact angle to increase above the pure hydrophobic
(FEP) value. The receding water angle also shows
pinning and is lower than the pure FEP value, indicat-
Macromolecules, Vol. 33, No. 22, 2000
Polymerization of Ethyl 2-Cyanoacrylate 8197
Mechanical Performance. The fracture strength in
cleavage of the DCB specimens can be described by the
opening mode fracture toughness, Gq. This is a measure
of the energy to propagate a crack (create new crack
surface area) assuming linear elasticity and is calculated by
Gq )
Figure 6. ATR IR spectra comparing a composite synthesized
for 49 h (top), a composite synthesized for 24 h (middle), and
virgin FEP (bottom). A 45° germanium crystal was used as
the ATR element.
ing that the composites possess a slightly more hydrophilic surface. The hexadecane results concur with the
water results.
PECA/FEP-24 specimens were both rinsed briefly in
acetone and subjected to an extensive extraction in THF.
The extraction involved sonicating a specimen in THF
at 60 °C for several days. The specimens were then
analyzed gravimetrically and with XPS. By XPS, the
surfaces of the specimens showed a significant loss of
PECA (Table 6). However, gravimetrically, the specimens lost only a few fractions of a percent in weight.
The PECA is washed from the surface of the specimens,
but the solvent resistance of FEP prevents the extraction of PECA from within the bulk of the specimens.
Certainly, a great deal of the PECA is located below the
surface of the specimens. To what depth the PECA is
incorporated and how it is distributed are not known.
(
)
Pq2 dC(a)
2B da
(1)
where B is the beam thickness (0.307 mm), Pq is the
critical load at failure, and C(a) is the specimen compliance as a function of a, the crack length.18 The use of
metal beams in the DCB geometry allows the compliance of the test specimens to be dominated by the
compliance of the metal beams. A schematic of the test
specimen is shown in Figure 9.
The metal beams must be calibrated to obtain their
compliance as a function of crack length. DCB test
specimens can be simulated by clamping the metal
beams together and measuring their compliance at
various clamped distances from the loaded ends (thus
simulating different crack lengths). From this curve, the
compliance as a function of crack length and the
derivitave of the compliance with respect to crack length
can be determined. This curve can be used to backcalculate the starting crack length of the test specimens
once the compliance of the test specimen is measured,
because the compliance of the metal beams dominates
the compliance of the test specimen. This back calculation requires the use of an iterative numerical method,
but that is a trivial problem for modern computers.
The specimens behave linear elastically until a critical
load is achieved, after which the specimen fails by
cleavage between one of the metal beams and the
specimen. From the slope of the specimen’s loaddisplacement curve, the compliance of the specimen can
be determined, which in turn provides the crack length
and the derivative of compliance with respect to crack
length. This and the measured critical load allow the
calculation of fracture toughness. The locus of failure
was determined to differentiate whether cleavage occurs
within the specimen, at the specimen-epoxy interface,
Figure 7. XPS spectrum of a PECA/FEP composite specimen synthesized for 24 h (PECA/FEP-24) obtained at a 15° takeoff
angle between the specimen and the detector.
8198
Kung et al.
Macromolecules, Vol. 33, No. 22, 2000
Figure 8. XPS spectrum of a PECA/FEP composite specimen synthesized for 49 h (PECA/FEP-49) obtained at a 15° takeoff
angle between the specimen and the detector.
Table 3. XPS Atomic Composition Data for FEP/PECA
Composite Surfaces
sample
atomic concentration
takeoff
angle (deg) C (%) F (%) O (%) N (%) Ti (%)
FEP
PECA
PECA/FEP-24
PECA/FEP-49
15
75
15
75
15
75
15
75
33.5
33.0
69.2
68.8
42.1
37.0
45.2
43.2
65.2
65.7
47.5
56.9
41.6
46.4
1.3
1.3
20.7
20.2
6.7
3.7
9.0
6.7
10.1
11.0
3.3
1.8
4.2
3.7
0.4
0.5
Table 4. Mass Composition of the Surface of PECA/FEP
Composites As Determined from XPS Data
sample
PECA/FEP-24
PECA/FEP-49
takeoff
angle (deg)
composition as determined from
N and F data (wt % PECA)
15
75
25
75
25.8
13.7
33.6
28.5
FEP
PECA
PECA/FEP-24
PECA/FEP-49
probe
fluid
water
hexadecane
water
hexadecane
water
hexadecane
water
hexadecane
treatment
rinsed in acetone
contact angles
θR (deg)
θA (deg)
121
55
78
3
122
52
133
46
Table 6. XPS Atomic Composition Data for PECA/FEP-24
Specimens That Were Rinsed in Acetone or Extracted in
Tetrahydrofuran
none
Table 5. Dynamic Contact Angle Data for FEP/PECA
Composite Surfaces
sample
Figure 9. Schematic representation of a double-cantilever
beam adhesive test specimen.
99
36
55
0
86
18
83
15
within the epoxy or at the epoxy-metal interface. XPS
was employed when the locus of failure was not visually
obvious. If failure appeared to occur at the specimenepoxy interface, then both sides of the interface were
examined using XPS. The chemical composition of the
cleaved surfaces gives an indication of where the failure
actually occurred.
Table 7 lists the adhesive fracture toughness of
various specimens tested, and Table 8 lists the XPS data
used for the failure locus determinations. FEP, as is
expected, forms a very weak bond with epoxy. XPS
reveals that failure occurs cohesively within the FEP
extracted in THF
atomic concntration
takeoff
angle (deg) C (%) F (%) O (%) N (%) Ti (%)
15
75
15
75
15
75
42.1
37.0
39.4
37.4
40.9
37.0
47.5
56.9
58.0
61.1
57.2
61.5
6.7
3.7
2.0
0.8
1.2
0.8
3.3
1.8
0.4
0.5
0.7
0.8
0.7
0.8
Table 7. Adhesive Fracture Toughness Data
sample
adhesive fracture toughness, Gq (kJ/m2)
FEP
PECA/FEP-24
PECA/FEP-49
0.00051 ( 0.00012
0.00051 ( 0.00011
0.00452 ( 0.00078a
a Mixed failure between specimen-epoxy and metal-epoxy
interfaces.
specimen, as is evidenced by the fluorine content at the
surface of the epoxy side. Unfortunately, the PECA/
FEP-24 composites also form very weak bonds to the
epoxy. The toughness values for FEP and PECA/FEP24 are identical. The failure locus XPS data show that,
like FEP, the PECA/FEP-24 composites also fail cohesively within the specimen. The failure locus data
provides a hypothesis for the poor bonding behavior of
both samples. It is not the lack of adhesion between FEP
and epoxy that causes the poor performance, rather it
is FEP’s cohesive weakness that cause easy failure in
adhesion tests. The PECA/FEP-24 composite is predominantly FEP in composition and also fails as though
Macromolecules, Vol. 33, No. 22, 2000
Polymerization of Ethyl 2-Cyanoacrylate 8199
Table 8. XPS Atomic Composition Data of the Two Sides
of Cleaved DCB Test Specimens Where Failure Occurred
at the Specimen-Epoxy Interface
sample
and side
virgin
cured epoxy
FEP
specimen side
FEP
epoxy side
PECA/FEP-24
specimen side
PECA/FEP-24
epoxy side
atomic concentration
takeoff
angle (deg) C (%) F (%) O (%) N (%) Ti (%)
15
75
15
75
15
75
15
75
15
75
80.0
77.7
35.4
37.7
67.8
71.1
42.6
36.4
70.1
71.4
11.0
12.3
64.4
62.1
18.3
9.1
53.1
61.6
13.9
9.8
9.0
10.0
0.2
11.3
16.2
3.5
1.1
12.5
13.7
2.7
3.6
0.2
0.8
0.9
3.5
5.1
it was pure FEP. Note (Table 8) that no nitrogen is
observed in the XPS spectrum of the FEP side of the
interface after failure. This indicates failure at FEPrich regions of the composite. This weak cohesive
performance of FEP may be a bulk property or evidence
of a “weak boundary layer”.
In contrast to PECA/FEP-24, PECA/FEP-49 shows an
order of magnitude improvement in the adhesion tests.
The failure locus was determined by eye. Visually, one
could see patches of the specimen where epoxy remained
bonded and other areas where the specimen was visible.
The PECA/FEP-24 results suggest that adding polar
groups to the FEP surface is not necessary to improve
adhesive performance. What is needed, is a method of
strengthening the cohesive performance. The higher
incorporation of PECA in the PECA/FEP-49 specimens
may have provided that strengthening.
Conclusions
The anionic polymerization of ECA in a CO2 medium
was attempted and determined to be viable: the anionic
polymerization of ECA proceeds effectively to completion
in liquid CO2. Although CO2 is susceptible to nucleophilic attack, CO2 is not incorporated into the final
polymer product to any measurable extent under the
conditions used in this study. Reducing the temperature
of the system and diluting the ECA monomer concentration may yield copolymer; however, neither of these
experiments were attempted in this work. Generally,
the polymerization results in CO2 compare quite well
to polymerizations found in the literature with amine
initiators in conventional solvents. The high reactivity
of cyanoacrylate monomers toward anionic polymerization is derived from the two electron-withdrawing
substituents; other monomers with two electron-withdrawing substiuents may anionically polymerize in CO2
as well.
Using the composite synthesis method described in
Scheme 2, it is possible to produce composites of PECA
and FEP. The goal of producing a composite at the
surface of the FEP substrate was only partially achieved
when triphenylphosphine was used as the initiator. The
amount of PECA incorporated into the substrate could
easily be varied by controlling the time that the initiator-containing substrate was allowed to soak in the
ECA/CO2 solution. With longer soak times, more monomer was absorbed into the substrate and incorporated
with the existing living PECA. Surface analysis showed
that the surface of the substrate was indeed a mixture
of PECA and FEP. However, gravimetric analysis and
extraction experiments showed that the majority of the
PECA was located below the surface. The ECA monomer
diffuses into the substrate faster than triphenylphosphine can diffuse out. The location of the polymerization
is thus below the surface.
The surface composite fabrication technique investigated here was not optimized. Pyridine diffuses out of
the substrate much faster that triphenylphosphine. The
experiments with pyridine showed that, with the faster
diffusing initiator, the polymerization location was
entirely outside the substrate. By selecting an appropriate anionic initiator, one with an appropriate diffusivity
under the chosen reaction conditions, the location of the
polymerization should be controllable. An initiator that
diffuses out of the substrate faster than triphenylphosphine but slower than pyridine should produce a more
surface-stratified composite. An investigation of different intiators and different monomers (e.g., butyl 2-cyanoacrylate) would be a logical next step to this research.
Still, with enough PECA incorporation, the composites showed an improvement in DCB cleavage tests.
DCB cleavage tests are designed to test the integrity of
substrate/adhesive joints. The reason for the improved
performance of the composites was not due to increased
adhesion between the substrate and the test adhesive
(epoxy). Adding functional groups to the surface did not
improve the performance of the composites. Mechanical
integrity in the DCB tests was improved by enhancing
of the cohesive strength of the substrate surface. Joints
of pure FEP and epoxy are poor, not because of poor
adhesion between the two materials: rather, the joints
fail within the FEP either due to poor bulk cohesiveness
or the existence of a weak surface later. The incorporation of PECA into FEP at high enough concentrations
seems to enhance the cohesive strength of the material.
Acknowledgment. We thank the Office of Naval
Research and the Green Polymer Chemistry Cluster of
the Center for UMass-Industry Research on Polymers
for financial support. We also thank the NSF-funded
UMass Materials Research Science and Engineering
Center for use of the central facilities.
References and Notes
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