Flame Retardant Polymer Compositions
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Abstract:
Flame retardant compositions are disclosed which comprise (a) at least one particulate material which expands on the application of heat and (b) at least one particulate nano-filler, together with at least one polymer and/or at least one curable monomer or oligomer. The compositions may also contain certain silicon-based materials. Flame-retardant compositions comprising polyorganosiloxanes containing one or more functional groups selected from amino, hydroxyl, methacrylic, acrylic and epoxy groups, are also disclosed.
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(19) United States
US 20100056687A1
(12) Patent Application Publication (10) Pub. No.: US 2010/0056687 A1
Diakoumakos et al. (43) Pub. Date: Mar. 4, 2010
(54) FLAME RETARDANT POLYMER (30) Foreign Application Priority Data
COMPOSITIONS
Dec. 20; 2002 (GB) ................................. .. 0229810.7
(75) Inventors: Constantinos D. Diakoumakos; Publication Classification
Trumpington (GB); Dimiter (51) Int CL
Lubomirov Kotzev; Corby (GB) C08K 5/09 (2006.01)
B05D 3/02 (2006.01)
Correspondence Address: C 08K 3/38 (2006.01)
Patent Counsel C08K 3/10 (2006.01)
Huntsman Advanced Materials Americas LLC C 08K 3/16 (2006.01)
Legal Dept., 10003 VVoodloch Forest Drive C03K 3/22 (2006.01)
The Woodlands, TX 77380 (US) C08K 3/34 (2006.01)
(52) U.S. Cl. .................... .. 524/396; 427/385.5; 524/399;
(73) Assignee: Huntsman Advanced Materials
Americas LLC; The Woodlands;
TX (US)
(21) Appl. No.: 12/613,691
(22) Filed: Nov. 6, 2009
Related U.S. Application Data
(63) Continuation of application No. 10/ 539,844; filed on
Jan. 20; 2006; now Pat. No. 7,635,728; filed as appli-
cation No. PCT/GB2003/005503 on Dec. 18; 2003.
524/400; 524/404; 524/405; 524/406; 524/413;
524/431; 524/434; 524/436; 524/437; 524/442;
524/443; 524/445; 524/456; 977/773
(57) ABSTRACT
Flame retardant compositions are disclosed which comprise
(a) at least one particulate material which expands on the
application of heat and (b) at least one particulate nano-filler;
together with at least one polymer and/or at least one curable
monomer or oligomer. The compositions may also contain
certain silicon-based materials. Flarne-retardant composi-
tions comprising polyorganosiloxanes containing one or
more functional groups selected from amino; hydroxyl; meth-
acrylic; acrylic and epoxy groups; are also disclosed.
US 2010/0056687 A1
FLAME RETARDANT POLYMER
COMPOSITIONS
[0001] The present invention relates to flame retardant
polymer compositions and to curable compositions for pre-
paring them.
[0002] In the modern polymer industry, flame-retardants
that are used in polymers are generally based on halogens
(mainly Cl and Br) and organic or inorganic phosphorus
compounds (e.g. ammonium polyphosphate, red phospho-
rus). Classically, intumescent fire retarded materials contain a
char-forming agent which can be a polyol (e.g. pentaerythri-
tol), a catalyst for char formation (usually a phosphoric acid
derivative) and a foaming agent, typically melamine.
Although these reduce hazards during polymer pyrolysis and
combustion by retarding a fire, they nevertheless can generate
large amounts of smoke, and they also present serious eco-
logical threats. There is a need for non-toxic (halogen-, phos-
phorus- and melamine-free), ecologically safe fire retardant
or flame retardant or fire resistant (these terms being synony-
mous for present purposes) compositions characterized by
low flammability and limited smoke levels.
[0003] lntumescent materials have been used as flame
retardants. Expandable graphite has attracted interest over the
last few years for the development of novel chemical intu-
mescent systems. For example U.S. Pat. No. 3,574,644
describes a process for increasing the flame resistance of
flammable materials by the incorporation of expandable
graphite flakes, while U.S. Pat. No. 6,472,070 describes fire-
resistant paints containing amongst other ingredients, an
epoxy resin, a hardener, and expandable graphite.
[0004] Particulate materials known as nanofillers may also
be used in composite materials. For example, Wo 99/09070
describes polymer foams which may contain nanofillers. W0
00/ 66657 describes a polymer composition comprising a
polymer and a nano -clay together with a second polymer, and
GB 2367064 describes a polymer composition containing a
polyolefin together with a nano-clay filler and an additional
filler. WO 99/35186 describes nanocomposites based on a
polymeric matrix and a layered double hydroxide, and pro-
vides information on the preparation of such materials.
[0005] We have now found that enhanced flame retardancy
in polymer systems can be obtained by using a specific com-
bination of particulate flame retardants. Accordingly, the
invention provides a particulate composition for use as a
flame retardant additive, which comprises (a) at least one
particulate material which expands on the application of heat
and (b) at least one particulate nano-filler.
[0006] The particulate compositions of the present inven-
tion may be used in the manufacture of flame-proof polymers,
and may be composited directly with the polymer, or with one
or more curable monomers, oligomers and/or polymers for
subsequent curing to produce the finished polymer. Accord-
ingly, the invention further provides a composition containing
a particulate composition according to the invention together
with at least one polymer and/ or at least one curable monomer
or oligomer.
[0007] Any desired monomer, oligomer or polymer, or any
mixture thereof, may be present. The fire retardant compo si-
tions are suitable for inclusion in a wide variety of composi-
tions which contain or can be cured to give polymers or
polymer-based materials, for example, polyamides, nylons,
polyesters, epoxy resins, ABS combinations, halogenated
Mar. 4, 2010
polymers such as poly(vinyl chloride) (PVC), polyethylenes,
polypropylenes, polyurethanes, polyacrylates/poly-
methacrylates (home- and copolymers), polystyrenes, poly-
chlopropene, phenolics, silicones, and silicone rubbers and
copolymers and combinations of polymers. Preferably a cur-
able monomer, oligomer or polymer contains one or more
groups selected from epoxy, acrylic, methacrylic, amine,
hydroxyl, carboxyl, anhydride, olefinic, styrene, acetoxy,
methoxy, ester, cyano, amide, imide, lactone, isocyanate or
urethane. The compositions may if appropriate contain a cur-
ing agent. For example, the composition may comprise a
mixture of a polyisocyanate bearing at least two isocyanate
groups with a polyol bearing at least two hydroxyl groups or
with an amine or a carboxylic acid; or a mixture of acrylates
or methacrylates with an appropriate initiator.
[0008] The invention also provides a cured article which
comprises a polymer matrix in association with a flame retar-
dant composition according to the invention.
[0009] The invention also provides a process for the manu-
facture of a cured article, which comprises admixing at least
one particulate material which expands on the application of
heat, at least one particulate nano filler, and at least one
curable monomer, oligomer or polymer, and subsequently
curing the resulting mixture. The three components of the
curable mixture may be mixed together in any desired order,
although preferably the nano-filler is dispersed within the
curable material as a first step. Curing may be carried out by
any appropriate method, for example the application of heat
or light, or the addition of a suitable curing agent, for example
an amine, carboxylic acid, carboxylic acid ar1hydride, or phe-
nol.
[0010] Compositions according to the invention are espe-
cially suitable for use as adhesives, sealants thermal insula-
tors and coatings. Accordingly, the invention further provides
a method of making an adhesive bond, a seal or a coating,
which comprises applying a monomer, oligomer and/or poly-
mer-containing composition according to the invention to a
substrate and if required curing said composition.
[0011] The material comprising component (a) is such that
it expands on the application of heat such as experienced
during a fire. The material should be such that it expands
when exposed to a temperature of above 500° C., preferably
above 300° C., especially above 100° C. Preferably compo-
nent (a) comprises expandable graphite.
[0012] Expandable graphite may be manufactured from
natural crystalline graphite flake. Deposits of crystalline
graphite are numerous and found around the world, usually as
inclusions in metamorphic rock, or in the silts and clays that
result from their erosion. Graphite is recovered from the ore
by crushing and flotation and is usually beneficiated to give
graphite flake that is 90-98% carbon. Crystalline graphite
consists of stacks of parallel planes of carbon atoms. Because
no covalent bonding exists between the layers other mol-
ecules can be inserted between them (intercalation). In one
commercial process for the production of expandable graph-
ite, sulphuric acid is inserted into the graphite after which the
flake is washed and dried. The intercalant is trapped inside the
graphite lattice, so the final product is a dry, pourable, non-
toxic material with minimal acidity (pH~3-4). When the
intercalated graphite is exposed to heat or flame, the inserted
molecules decompose to generate gas. The gas forces apart
the carbon layers and the graphite expands.
[0013] The flakes of expandable graphite are generally
plate-like. For a 50-mesh flake, the typical length and width
US 2010/0056687 A1
are about 0.5 mm, with the largest particles generally being
about 0.9 mm, while the typical thickness is about 0.08 mm.
For a 80-mesh flake, the typical length and width are about 0.4
mm whilst the typical thickness is about 0.07 mm. A wide
variety of expandable graphites of different particle sizes,
acidity, decomposition temperatures, and expansion efli-
ciency, are nowadays commercially available (e.g. GRAF-
GUARD® product series by Graftech). Any of these are
suitable foruse in the present invention. The various grades of
expandable graphite available typically expand when
exposed to temperatures in the range of 160 to 260° C. or
higher.
[0014] The proportion of component (a), especially
expandable graphite, used in a monomer, oligomer and/or
polymer-containing composition of the invention preferably
ranges between 0.1 and 95% w/w, preferably between 1 and
40% w/w.
[0015] Nano-fillers are particles of a sub-micron size. Typi-
cal nano-fillers may comprise silica, barium sulphate or, espe-
cially, clays. A nano-clay is an ionic phyllosilicate; it may be
any hydrophilic or organophilic layer silicate obtainable from
a natural or synthetic layer silicate. Such materials have a
sheet-type or platey multiscale structure. At the Angstrom
scale is the platelet, which is 0.7-1 nm thick and several
hundred nanometers long and wide (ca. 100-1000 nm). As a
result individual sheets have aspect ratios (Length/Thickness,
L/T) varying from 200-1000 or even higher, with a majority
of platelets in the 200-400 range after purification. In other
words, these sheets usually measure approximately 200>20 6.0 7.0 5.0 4.0 20.0 6.0 9.0 10.0
Dripping 0 0 0 0 0 0 0 0 0
extinction time
(sec)
Afterglow (sec) 0 0 0 0 0 0 0 0 0
Smoke level 5 2 2 2 4 2 2 4 3
*indicates a comparative example
[0104] Upon comparing compositions C3 and Cl (compari-
son), C2 (comparison) and C4, the synergy of expandable
graphite with the nano-clay is seen not only as regards
enhanced flame retardancy but also and most importantly the
smoke suppression effect. When no expandable graphite is
present (comparison composition C6), the inorganic addi-
tives alone are not able to achieve the same flame resistance.
The flammability test data of the compositions C5 (compari-
son) and C10 provide strong evidence of effective smoke
Resin or dispersion
Silicone fluid 65000
D4608
D5006
MY—05 10
Silicone Wacker CLM
42205
D3710
Tolylene diisocyanate
DBTDL
Ammonium Octamolybdate
C11 C12 C13 C14 C15
5 7 4 6 0
10.0 11.0 10.0 7.0 7.0
0 0 0 0 0
length, no dripping, no afterglow and limited smoke) was far
better than any of the epoxy-based comparison compositions.
Examples 28-49
Preparation of Novel Flame Retardant Compositions
Based on Silicon Polymeric Platforms
[0107] The following formulations were prepared accord-
ing to the procedure described below
TABLE 6
Compositions
s2 s3 s4 s5 S6 s7 S8 s9 S10 s11
Wt-(g)
15.00 15.00 15.00 15.00 15.00 15.00
14.76 14.76 14.76 14.76 14.76
1.85 1.85 1.85 1.85 1.85 1.85 1.65 1.65 1.65 1.65 1.65
US 2010/0056687 A1
9
TABLE 6-continued
Expandablegraphite 0.18 0.90 1.86 2.97 4.23 0.15 0.87 1.83
220-80B
Zincborate
Aluminum trihydroxide
Compositions
S12 S13 S14 S15 S16 S17 S18 S19
Resin or dispersion Wt. (g)
Silicone fluid 65000 14.40
D4608 15.84 15.84 15.84 15.84
D5006 15.84 15.84 15.84
MY-0510 1.76 1.76 1.76 1.76 1.76 1.76 1.76 1.76
Silicone Wacker CLM
42205
D3710
Tolylene diisocyanate
DBTDL
AmmoniumOctamolybdate 0.68 0.68 0.68 0.68 0.76 0.72 0.72
Expandablegraphite 1.60 1.72 1.56 1.56 1.76 0.72 0.24
220-80B
Zincborate 2.28 2.32 2.44 2.24 2.52 2.4 2.32
Aluminumtrihydroxide 2.28 2.32 2.44 2.24 2.52 2.4 2.32
[0108] Procedure: [0113]
[0109] The ingredients of the formulations S1-S19 were
added and mixed as follows:
[0110] 1” addition: All the components but the epoxy resin
MY-0510 or the D4608 or the D5006 (where applicable).
Thorough mixing.
[0111] 2"d addition: The epoxy resin MY-0510 or the
D4608 or the D5006 (where applicable), was added to the
previously prepared mixtures.
[0112] Subsequently, they were mixed thoroughly and then
coated on aluminium strips (for flammability testing) accord-
ing to the procedure described above.
[0117]
Mar. 4, 2010
2.89 4.11
S20 S21
20.00
22.00
1.34 1.34
0.10 0.12
1.00
2.34
3.34
3.34
The ingredients of the formulations S20-S21 were
added and mixed as follows:
[0114] 15’ addition: All the components except the tolylene
diisocyanate. Thorough mixing.
[01 15] 2”’ addition: Tolylene diisocyanate was added to the
previously prepared mixtures.
[01 1 6] Subsequently, they were mixed thoroughly and then
coated on aluminium strips (for flammability testing) accord-
ing to the procedure described above.
The following Table summarizes the BSS7230
flammability test results for the reference compositions.
TABLE 7
Compositions
BSS7230 Test S1 S2 S3 S4 S5 S6 S7 S8 S9 S10 S11 S12
Extinction time 0 0 0 0 0 0 42 8 0 0 0 0
(sec)
Burn length (cm) 6.00 4.00 3.00 3.00 3.00 2.00 20.00 8.00 4.00 4.00 1.00 2.00
Dripping 0 0 0 0 0 0 0 0 0 0 0 0
extinction time
(sec)
Afterglow (sec) 0 0 0 0 0 0 0 0 0 0 0 0
Smoke level 2 4 4 4 4 4 3 3 1 1 0 0
Compositions
BSS7230 Test S13 S14 S15 S16 S17 S18 S19 S20 S21
Extinction time 10 0 0 0 0 0 0 15 0
(sec)
Burn length (cm) 7.00 2.00 2.50 2.00 1.00 3.00 4.00 13.00 3.00
Dripping 0 0 0 0 0 0 0 0 0
extinction time
(sec)
Afterglow (sec) 0 0 0 0 0 0 0 0 0
Smoke level 5 0 1 0 0 2 3 2 1
US 2010/0056687 A1
[0118] An additive-free composition (S1) presented a very
good flame proofness that was further enhanced by the intro-
duction of expandable graphite (loads>5% w/w) and nano-
clay. Compositions, S1 -511 illustrate the effect of varying
amounts of expandable graphite. Flammability test data of the
S1 composition compared to those of the S2-S6 compositions
shows a synergy between silicon and expandable graphite.
[0119] The effect of nano-clay in a silicon-based composi-
tion is further enhanced when it is combined with other inor-
ganic additives for loads of expandable graphite higher than
3% w/w (compositions S12 and S17). The effect of including
expandable graphite in silicon-based compositions is illus-
trated by comparing the flarmnability test data of the compo-
sitions S13 and S17. The role of ammonium octamolybdate in
silicon-based compositions seems to be rather positive for
decreased flammability (S14 and S17) rather than acting as a
smoke suppressant. Aluminium trihydroxide (S16) appears to
behave like ammonium octamolybdate in silicon-based poly-
meric platforms.
[0120] The flammability test data of the S17-S19 compo-
sitions confirm the synergy between silicon and expandable
graphite. The improvement of the fire resistance of a much
softer material, a silicon-based polyurethane, is illustrated by
compositions S20 and S21. Composition S17 presented the
best flame retardancy performance achieved.
Examples 50-65
Preparation of Novel Flame Retardant Compositions
Based on Silicon and Carbon Polymeric Blends
[0121] The following formulations were prepared accord-
ing to the procedure described below
TABLE 9
CS1 CS2 CS3 CS4 CS5 CS6
Resin or dispersion
Silicone fluid 65000
D3508
MY—05 10
Tetraethylpentamine
Silicone Wacker CLM 42205
Voranol EP1900
D3710
D371 1
Tolylene diisocyanate
DBTDL
D3 61 1
D3 81 1
Poly(urethane-
methacrylate)
Dimthelyl p-toluidine
Benzoyl peroxide
Ammonium Octamolybdate
Expandable grpahite 220-
80B
Zinc borate
13.34 13.34
6.12
8.98 8.98
9.80
8.92
1.04 2.10
4.44 4.44
13.02
5.58
1.04
11.84
2.10 3.16 3.16
0.88
2.06
0.90
2.08
0.88
2.06
2.94
2.94
2.98
2.98
2.94
Aluminum trihydroxide 2.94
CS7
2.14
14.16
3.70
Mar. 4, 2010
10
[0122] Procedure:
[0123] The ingredients of the formulations CS1-CS13 were
added and mixed as follows:
[0124] 15’ addition: All the components except the epoxy
resin MY-0510 or the D3508 (where applicable). Thorough
mixing.
[0125] 2”’ addition: The epoxy resin MY-0510 or the
D3508 (where applicable), was added to the previously pre-
pared mixture.
[0126] Subsequently, they were mixed thoroughly and then
coated on aluminium strips (for flammability testing) accord-
ing to the procedure described above.
[0127] The ingredients of the formulations CS 1 4-C14 were
added and mixed as follows:
[0128]
diisocyanate and the benzoyl peroxide, respectively. Thor-
ough mixing.
[0129]
oxide were added to their corresponding previously prepared
1” addition: All the components except the tolylene
2”’ addition: Tolylene diisocyanate and benzoyl per-
mixtures .
[013 0] Subsequently, they were mixed thoroughly and then
coated on aluminium strips (for flammability testing) accord-
ing to the procedure described above.
[0131] The following Table summarizes the BSS7230
flammability test results for the reference compositions.
Compositions
CS8 CS9 CS10 CS11 CS12 CS13 CS14 CS15
Weight(g)
2.14 1.06 1.06 0.54 0.54
15.56 16.50 8.45
15.00 15.38
3.70 3.94 3.94 4.08 4.08
10.00
10.00
11.00
11.00
1.26 1.26
0.12 0.12
5.30
3.63
3.00
0.60
0.33
0.92 0.92 0.92 0.92 0.86
2.14 2.16 2.16 2.16 2.00
3.06 3.08 3.08 3.10 2.86
3.06 3.08 3.08 3.10 2.86
US 2010/0056687 A1
TABLE 10
Mar. 4, 2010
Compositions
BSS7230Test CS1 CS2 CS3
Extinction time 0 0 0 0 19 0 22 3
(sec)
Burn length (cm) 15.0 3.0 16.0 3.0 >20 2.0 >20 6.0
Dripping 0 0 0 0 0 0 8 0
extinction time
(sec)
Afterglow (sec) 0 0 0 0 0 0 0 0
Smoke level 4 1 4 2 5 2 5 3
[0132] In the case of blending carbon- and silicon-based
platforms followed by subsequent crosslinking of both or at
least one i.e. in the case one of the two polymers is not
functional, it becomes evident that even when extremely low
amounts of silicone are used (down to 3% w/w) and even
without the introduction of any organic/inorganic additives
(compositions CS9 and CS11) a dramatic decrease in the
extinction time compared with the reference R1 composition
was achieved.
Example 66
[0133] In order to assess the physical/mechanical proper-
ties of the compositions of the present application, a commer-
cially available and non-flame retarded, two component
epoxy-based adhesive the EPIBOND 1590® ((Trade Mark,
Vantico Ltd.) was reformulated (Adhesive 1) according to the
claimed compositions and its flame retardancy along with an
array of physical/mechanical properties was recorded.
[0134] Procedure:
[0135] Preparation of Part A of the Adhesive 1
[0136] The resin part of the EPIBOND 1590® (70 g) and
Cloisite 10A® (7.25 g) were mixed in a high shear mixer for
4-6 h. Subsequently, 7.00 g of Grafguard 220B, 3.00 g of
ammonium octamolybdate, 10.00 g of Firebrake-ZB and
10.00 g of Apyral-22 were added to the mixture and mixing
was continued in a low shear mixer for about an hour.
[0137] Preparation of Part B of the Adhesive 1
[0138] The hardener part of the EPIBOND 1590® (70 g)
and 7.00 g of Grafguard 220B, 3.00 g of ammonium octamo-
lybdate, 10.00 g of Firebrake-ZB and 10.00 g of Apyral-22
were mixed in a low shear mixer for about an hour.
[0139] The two components of the Adhesive 1 were mixed
in a mixing ratio of 1.95:1 w/w (Part A: Part B). The curing
process of the samples prepared was: a) 7 days @ 23° C.
(Adhesive 1-23C) and 4 h @ 60° C. (Adhesive 1-60C)
[0140] The following Table depicts the physical/mechani-
cal properties of the Adhesive 1-23C and the Adhesive 1-60C.
The flame retardancy of the both samples was tested accord-
ing to the flame retardancy method described in the Experi-
mental and in a “blue” flame.
TABLE 11
Adhesive Adhesive EPIBOND
Physical/Mechanical Properties 1-23C 1-60C 1590 ®
Glass transition temperature (° C.) 58 72 n.d.
by DSC
Glass transition temperature (° C.) 60 82 n.d.
by TMA
CS4 CS5 CS6 CS7 CS8
CS9 CS10 CS11 CS12 CS13 CS14 CS15
24 3 27 3 4 0 0.00
>20 2.5 >20 6.0 10.0 3.5 3.5
12 0 16 0 0 0 0
0 0 0 0 0 0 0
5 3 5 3 2 0 0
TABLE 1 1 -continued
Adhesive Adhesive EPIBOND
’hysical/ Mechanical Properties 1-23C 1-60C 1590 ®
Glass transition temperature (° C.) 146 143 n.d.
3y DMA*
Thermal expansion coefficient (10’° - 78 82 n.d.
(4) below glass transition
Thermal expansion coefficient (10’° - 110 124 n.d.
(4) above glass transition
Young’s storage modulus (MPa) @ 775 567 n.d.
23 ° C.
Charpy impact strength (KI/m2) n.d. 3 n.d.
:racture energy (J/m2) 438 1263 n.d.
:racture toughness (MPa - mm) 1 2 n.d.
Compression strength (MPa) 38 57 n.d.
Compression modulus (MPa) 123 8 1440 n.d.
nap shear strength (MPa) 14 18 n.d.
Average peel load (N) 24 n.d. n.d.
Extinction time (sec) 0 0 15
Dripping (sec) 0 0 0
3urn length (cm) 2 2 18
Smoke 1 1 5
*The samples were tested after been remained at 23° C. for 6 months.
Example 67
[0141] In order to assess the thermal insulation potential of
the compositions of the present application, the Adhesive
1-23C prepared as mentioned in Example 66, was tested
according to the thermal insulation assessment method.
Example 68
[0142] The thermal insulation of a specimen of EPIBOND
1590® cured at 23° C. for 7 days was also assessed according
to the thermal insulation assessment method. In its case the
flame applied for only 165 sec because the specimen was
completely burned out after this time.
Example 69
[0143] FIG. 1 depicts the results recorded by the thermal
insulation assessment method for the Adhesive 1-23C and the
EPIBOND 1590® prepared and tested in Examples 67 and
68, respectively. After 165 see the specimen of EPIBOND
1590® was completely burned out with maximum recorded
temperature of approx. 565° C., exceeding by much the mate-
rials initial decomposition temperature. In contrast Adhesive
1-23C remained dimensionally intact after approx. 260 sec.
Above 180-200 sec, the temperature of the Adhesive
1-23Cremained almost levelled (maximum temperature
recorded: 226° C.).
US 2010/0056687 A1
1-29. (canceled)
30. A composition comprising (a) at least one expandable
particulate material which expands on the application of heat
and (b) at least one particulate intercalated nano-clay,
together with at least one polymer and/ or at least one curable
monomer or oligomer.
31. The composition according to claim 30, which also
comprises at least one other particulate material having fire
retardant properties.
32. The composition according to claim 31 wherein the
particulate material having fire retardant properties is a metal
oxide/ acid, a hydrate, a hydroxide, a carbonate, a sulphate, a
silicate, a nitride, a molybdate or a stearate.
33. The composition according to claim 31 wherein the
particulate material having fire retardant properties is a zinc
or calcium borate, starmate or molybdate, a zinc or magne-
sium stearate, an ammonium molybdate, a calcium hydrox-
ide, an aluminum trihydroxide, a silicon oxide, a silicon
nitride, a boron nitride, a sodium metalsilicate pentahydrate,
a potassium tetraborate tetrahydrate, a magnesium hydrox-
ide, a magnesium silicate, a titanium oxide, a ferric oxide, a
molybdenum oxide, a lead phthalate, a stannous chloride, or
a complex thereof.
34. The composition according to claim 30 which com-
prises two or more particulate materials having fire retardant
properties.
35. The composition according to claim 31 wherein the
particulate material having fire retardant properties is present
in an amount of from 1 to 95% w/w based on the total weight
of the composition.
36. The composition according to claim 30 wherein the
polymer and/or curable monomer or oligomer contains one or
more epoxy, acrylic, methacrylic, amine, hydroxyl, carboxyl,
anhydride, olefinic, styrenes acetoxy, methoxy, ester, cyano,
amide, imide lactone or urethane groups.
37. The composition according to claim 30 wherein the
intercalated nano-clay is present in an amount of from 0.1 to
95% w/w based on the total weight of the composition.
38. The composition according to claim 30 wherein the
expandable particulate material is present in an amount of
from 0.1 to 95% w/w based on the total weight of the com-
position.
39. The composition according to claim 30 which is an
adhesive, sealant or coating composition.
40. A cured article which comprises a polymer matrix in
association with at least one expandable particulate material
which expands on the application of heat and at least one
intercalated nano-clay.
Mar. 4, 2010
41. A process for the manufacture of a cured article which
comprises admixing at least one expandable particulate mate-
rial which expands on the application of heat with at least one
intercalated nano-clay and at least one curable monomer,
oligomer and/ or polymer to form a mixture and subsequently
curing the mixture.
42. A method of making an adhesive bond, seal or coating
comprising applying a composition according to claim 30 to
a substrate and curing the composition.
43. A composition comprising (i) one or more reactive
monomers, oligomers and/or polymers containing reactive
species selected from the group consisting of:
a. epoxy-functional compounds and resins in combination
with amino-functional compounds, resins, oligomers, or
polymers;
b. hydroxy-functional compounds, oligomers, polymers in
combination with isocyanate-functional monomers,
dimers, oligomers, or polymers;
c. methacrylic or acrylic functional monomers in combi-
nation with methacrylic or acrylic functional oligomers
or polymers;
d. amino-functional polyorganosiloxane in combination
with epoxy-functional compounds, resins or oligomers;
e. hydroxy-functional polyorganosiloxane in combination
with isocyanate-functional monomers, dimers or oligo-
mers;
f. methacrylated or acrylated polyorganosiloxane;
g. epoxy-functional compounds and resins and amino-
functional compounds, resins, oligomers, orpolymers in
combination with amino -functional polyorganosiloxane
and epoxy-functional compounds, resins or oligomers;
h. hydroxy-functional compounds, oligomers, or polymers
and isocyanate-functional monomers, dimers, oligo-
mers, or polymers in combination with hydroxy-func-
tional polyorganosiloxane and isocyanate-functional
monomers, dimers or oligomers; and
i. methacrylic or acrylic functional monomers, oligomers
or polymers in combination with methacrylated or acry-
lated polyorganosiloxane;
(ii) expandable graphite; (iii) intercalated nano-clay; and
optionally (iv) one or more flame retardant additives and
smoke suppressants selected from the group consisting of
zinc borate, aluminum trihydroxide, and ammonium octamo-
lybdate.
44. The composition according to claim 43, wherein the
polyorganosiloxane is polydimethylsiloxane.
45. The composition according to claim 43 wherein the
clay is montmorillonite.
* >X< * >X< *
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