[0001] The present invention relates to adhered surface coverings, and more particularly
to adhered surface coverings which will be suitable for use over stable or unstable
subsurfaces.
[0002] Surface coverings for walls, floors, ceilings and the like have traditionally been
adhered to subsurfaces such that the surface coverings are fixed and immobile. Adhesion
is required for ceilings and walls because of gravitational effects, but floor coverings
are held to a subfloor by gravity and, thus, the use of an adhesive is not always
necessary. The criteria under which a floor covering may be loose-laid are discussed
in parent European Application Serial No. 823069091, published on July 6, 1983, as
No. 83220, the contents of which are incorporated herein by reference. This application
is referred to herein as the "Parent Application."
[0003] The present application relates to processes for adhering surface coverings to subsurfaces
using an adhesive whereby subsurface movement will not cause the adhesive bond to
fail.
[0004] Accordingly, one objective of the present invention is to provide a method by which
a surface covering can be selected, and a suitable adhesive can be selected for use
with the surface covering. The selection of the adhesive will depend on the dimensional
stability of the subsurface and the performance characterstics of the surface covering.
[0005] Another objective of the present invention is to provide methods by which products
comprising one or more reinforcing layers may be modified in situ to provide buckling
characteristics which allow the products to be used as adhered surface coverings in
combination with appropriate adhesives.
[0006] These and other advantages of the present invention will become apparent from the
detailed description of the preferred embodiments which follow.
[0007]
FIGS. lA and 1B illustrate a diagram of a computer program which may be used to calculate
the bending stiffness and/or relaxed compressive stiffness values according to the
present invention.
FIG. 2 illustrates an example of a continuous modification pattern as used in the
examples.
FIGS. 3A and 3B illustrate a diagram of a modified computer program, comparable to
FIGS. lA and 1B, which may be used to calculate the adhered basis weight and/or strain
according to the present invention.
[0008] The present invention concerns surface coverings which are adhered to subsurfaces
using an adhesive. A process is provided whereby an adhesive can be selected for use
with an unmodified surface covering such that subsurface movement will not cause adhesive
failure. Processes are also provided whereby modified surface coverings may be adhered
using a similarly selected adhesive, or whereby adhesives may be selected and the
surface coverings modified such that the adhesives will not fail due to subsurface
movement.
[0009] In one embodiment, the present invention comprises a process for adhering a surface
covering to a subsurface having an ascertainable subsurface dimensional change such
that said surface covering will accommodate subsurface movement without buckling,
said process comprising the steps of (a) selecting a surface covering, the critical
buckle strain of the selected covering being less than the subsurface dimensional
change; (b) selecting a target critical buckle strain which is greater than the subsurface
dimensional change; (c) measuring the relaxed compressive stiffness, the bending stiffness,
and the basis weight of said selected covering; (d) calculating the adhered basis
weight for a surface covering having the measured bending stiffness, the measured
relaxed compressive stiffness, and a critical buckle strain which is equal to the
target critical buckle strain; (e) calculating the minimum adhesive strength which
will be necessary to adhere said surface covering to said subsurface in a manner which
will prevent buckling; (f) selecting a suitable adhesive, and (g) adhering said surface
covering to said subsurface.
[0010] In a second embodiment, the present invention comprises a process for modifying a
surface covering comprising at least one reinforcing layer whereby it can be adhered
without buckling to a subsurface having an ascertainable subsurface dimensional change,
said process comprising the steps of (a) selecting a surface . covering comprising
at least one reinforcing layer, the critical buckle strain of said selected covering
being less than the subsurface dimensional change; (b) selecting an adhesive having
a determined adhesive strength; (c) measuring the basis weight, the bending stiffness
and the relaxed compressive stiffness of said selected covering; (d) selecting a target
critical buckle strain which is greater than the subfloor dimensional change; (e)
calculating the adhered basis weight which would be obtained if said selected covering
were adhered to said subsurface using said adhesive; (f) calculating the relaxed compressive
stiffness for a modified surface covering having the measured bending stiffness, the
calculated adhered basis weight, and a critical buckle strain which is equal to the
target critical buckle strain, and (g) modifying said covering in situ such that it
has a relaxed compressive stiffness which is not greater than the calculated relaxed
compressive stiffness value, whereby when the modified surface covering is adhered
to said subsurface using said adhesive, it will accommodate subsurface movement without
buckling. This embodiment also comprises a process for the manufacture of a composite
structure by adhering the modified surface covering to the sub-surface using said
adhesive, and the resulting composite structure.
[0011] In a third embodiment, the present invention comprises a process for modifying a
surface covering comprising at least one reinforcing layer, the modified covering
being suitable to accommodate the subsurface movement of a subsurface having an ascertainable
subsurface dimensional change when said modified covering is adhered to said subsurface,
said process comprising the steps of (a) selecting a surface covering comprising at
least one reinforcing layer, the critical buckle strain of said selected covering
being less than the subsurface dimensional change; (b) modifying said covering in
situ such that the critical buckle strain of the modified covering is greater than
the initially measured critical buckle strain, but less than the critical buckle strain
which would equal or exceed the subsurface dimensional change; (c) selecting a target
critical buckle strain which is greater than the subsurface dimensional change; (d)
measuring the bending stiffness, relaxed compressive stiffness and basis weight of
said modified covering; (e) calculating the adhered basis weight for a covering having
the measured bending stiffness, the measured relaxed compressive stiffness, and a
critical buckle strain that is equal to the target critical buckle strain; and (f)
calculating the minimum adhesive strength necessary to adhere said modified covering
to said subsurface, whereby when a suitable adhesive having an adhesive strength at
least as great as said calculated adhesive strength is selected, said modified structure
can be adhered to said subsurface in a manner which will prevent buckling. This embodiment
also comprises a process for the manufacture of a composite structure by adhering
the modified surface covering to the sub-surface using said adhesive, and the resulting
composite structure.
[0012] In a fourth embodiment, the present invention relates to a surface covering which
is suitable to be adhered with an adhesive to a subsurface without buckling, said
surface covering comprising (a) a matrix material, and (b) at least one reinforcing
layer disposed therein which has been modified in situ such that said surface covering
has a critical buckle strain which is less than the subsurface dimensional change
of said subsurface, the difference between said buckle strain and said subsurface
dimensional change being such that the adhesive strength of a selected adhesive in
combination with the basis weight of said surface covering will be sufficient to provide
an adhesive bond having a strength which is not less than the adhered basis weight
calculated for said surface covering.
[0013] In a fifth embodiment, the present invention . relates to a composite structure comprising
a surface covering, a subsurface and an adhesive which adheres said surface covering
and said subsurface together, said surface covering comprising (a) a matrix material,
and (b) at least one reinforcing layer disposed therein which has been modified in
situ, the critical buckle strain of said surface covering being less than the subsurface
dimensional change of said subsurface, the difference between said critical buckle
strain and said subsurface dimensional change being such that the adhesive strength
of said adhesive in combination with the basis weight of said surface covering provides
an adhesive bond having a strength which is not less than the adhered basis weight
calculated for said surface covering.
[0014] As used herein, "loose-lay floor structure" is a floor structure which will lie flat
on a stable or unstable subfloor, which will resist doming, curling, buckling, or
movement under a rolling load, which preferably has a low structural stability value,
and which need not be held in place using adhesives.
[0015] As used herein, "accommodating surface covering" is a surface covering which will
accommodate or alter its size and shape to match that of an unstable subsurface, even
when it is adhered to the subsurface.
[0016] As used herein, "subsurface dimensional change" is a measure of the change in length
of a subsurface material under the conditions of its environment. This change is expressed
herein as change per unit length.
[0017] As used herein, "critical buckle strain" is the strain at which a surface covering
that is compressed in a planar fashion will buckle.
[0018] As used herein, "adhered critical buckle strain" is the strain at which a surface
covering that is adhered to a subsurface with a given adhesive will buckle when compressed
in a planar fashion. An adhered critical buckle strain value is usually applicable
only to the surface covering/adhesive/subsurface system for which it is measured.
[0019] As used herein, "relaxed compressive stiffness" is the approximate compressing force
per inch (centimeter) of width divided by the induced strain, the value of said relaxed
compressive stiffness being projected to a 1000-hour load relaxation and the compressive
force being applied in a planar fashion, the measurement being taken in the linear
portion of the stress-strain curve.
[0020] As used herein, "relaxed tensile stiffness" is the approximate stretching force per
inch (centimeter) of width divided by the induced strain, the value of said relaxed
tensile stiffness being projected to a 1000-hour load relaxation and the stretching
force being applied in a planar fashion, the measurement being taken in the linear
portion of the stress-strain curve.
[0021] As used herein, "basis weight" is the weight in pounds per square yard (kilograms
per square meter) of a surface covering material..
[0022] As used herein, the term "adhered basis weight" describes the calculated value which
is the minimum strength necessary to adhere a surface covering to a subsurface. This
value is a composite of the adhesive strength of an adhesive and the actual basis
weight of a material, as will be explained in detail below.
[0023] As used herein, "matrix material" comprises all components of a surface covering
material excluding the reinforcing material.
[0024] As used herein, "bending stiffness" is the resistance to bending demonstrated by
a surface covering material as measured in inch-pounds (Newton-meters) using a cantilever
beam or equivalent method.
[0025] As used herein, "bending resistance" is a material parameter used in the theoretical
derivation of the potential energy expression, and characterizes the resistance of
the surface covering material to bending.
[0026] As used herein, "structural stability" is a . measure of the change in length in
percent of a surface covering sample which has been heated at 180°F (82.2°C) for six
hours and reconditioned at 73.4°F (23°C) and 50% relative humidity for one hour.
[0027] A surface covering should be expected to maintain within acceptable limits the shape
and dimensions of the subsurface to which it is adhered, and it should not shrink
leaving unsightly gaps. This requirement applies regardless of the nature of the subsurface.
Therefore, a desirable trait for such a covering is that it have a structural stability
under normal conditions of not more than 0.5% and preferably not more than 0.1%.
[0028] If the surface to which the surface covering is to be adhered is stable, the characteristics
which must be demonstrated by the surface covering are less stringent than for an
unstable subsurface since a minimal dimensional change of the surface covering results
in minimal planar compressions of the surface covering. Nevertheless, problems can
still be encountered which relate to doming, curling, and adhesive failure.
[0029] Conversely, unstable subsurfaces such as particleboard dramatically increase the
requirements for a surface covering because such subsurfaces tend to expand and contract
depending on the temperature and relative humidity conditions within the structure
in which the subsurface resides. During winter months, dry furnace-heated air tends
to shrink unstable subsurfaces, whereas during humid summer months such subsurfaces
tend to expand. A surface covering which is adhered to such a subsurface at its maximum
expanded position experiences a variety of stresses when the subsurface changes its
dimensions. Thus, many surface coverings having the required structural stability
will nevertheless be unable to accommodate these stresses, and will show doming, buckling
or other failure of the adhesive bond.
[0030] Surprisingly, we have discovered that the principles set forth in the parent application
are applicable to a variety of surface coverings such as sheet flooring, floor tile,
wall tile, ceiling tile, and the like, wherein these surface coverings are adhered
to subsurfaces using an adhesive. The same basic principles which apply to loose-lay
flooring also apply to adhered surface coverings. Thus, the terms "subsurface dimensional
change" and "accommodating surface covering" have the meanings set forth above.
[0031] One major modification in terminology concerns the basis weight. In the case of loose-lay
flooring, the flooring is held to the subsurface by its own weight. In a ceiling tile,
however, the tile would tend to be separated from the ceiling subsurface by its weight;
i.e., gravity would tend to make it fall. This gravitational pull is offset by the
adhesive; thus, for purposes of this application of the invention, the adhesive strength
of an adhesive should be considered concurrently with the effect of gravity on the
basis weight.
[0032] Several possible aspects of this are envisaged. For example, if a floor covering
is considered, the adhesive strength will be enhanced by the gravitational effect
on the covering; if a ceiling covering is considered, the gravitational effect will
detract from the adhesive strength; and if a wall covering is considered, the adhesive
strength will be relatively unaffected because the gravitational pull will tend to
shear in a direction perpendicular to the adhesive strength, a situation which may
be ignored for purposes of the present invention.
[0033] Because of these considerations, the term "adhered basis weight," as previously defined,
is adopted herein. Although'the adhered basis weight is a composite of the adhesive
strength of an adhesive and the actual basis weight of a surface covering, in actual
practice, the adhered basis weight usually will be due almost entirely to the adhesive.
For example, a typical floor covering may have a basis weight of two to three pounds
per square yard (1 to 2 Kg/m
2), whereas a typical adhesive may have an adhesive strength of two to three pounds
per square inch (0.4 to 0.6 Kg/cm
2). Accordingly, in many instances the basis weight of the surface covering will be
quite small in comparison to the adhesive strength. As will be more fully explained
below, the adhered basis weight may be calculated by substituting appropriate values
for relaxed compressive stiffness, bending stiffness, and target critical buckle strain
into the standard equation, or it may be determined by adding the actual basis weight
to, or substracting it from, the adhesive strength.
[0034] Other aspects of adhesives which should be considered are their interactions with
the surface coverings, the subsurfaces, and the environment in which they are used.
Adhesives are often formulated for specific uses. Therefore, for purposes of the present
invention, it is assumed that the artisan has the skill to select an adhesive which
will show long-term compatibility with the surface covering, the subsurface, and the
environment in which it is used. It must be emphasized, however, that the accurate
determination of adhesive strength is very important and, for that reason, the directions
for use provided by the manufacturer of the adhesive should be precisely followed.
Furthermore, the application should be made in the same way for the test and for field
installation; e
.g., if the directions specify that an adhesive should be applied in a particular manner
with a trowel having specified groove dimensions, the application of the adhesive
should be performed exactly in that manner both for the test and when the surface
covering is installed over a subsurface. If the installation is not performed in the
same way, the predictions obtained according to the present invention may, in many
instances, be invalid.
[0035] An adhesive which is used to adhere two surfaces together has, after appropriate
aging, an initial adherence strength; however, an adhesive bond usually diminishes
in strength under load with time and, thus, it may eventually rupture. Because of
the potential for a decrease in adhesive strength with time, it has been found that
the adhesive strength which should be used when practicing the present invention is
the adhesive strength under load in a given environment. This value is defined as
the approximate force per square unit of measure (inch
2, yard
2, centimeter
2, or meter
2) at which the adhesive will fail. It preferably is calculated using the bending stiffness,
relaxed compressive stiffness and actual basis weight of a given surface covering
in combination with the adhered critical buckle strain, as previously defined.
[0036] Although adhesive strength may be determined in a number of different ways, the adhesive
strength of an adhesive may be conveniently determined for a given surface covering/subsurface
system by preparing test strips of surface coverings adhered to subsurface materials
which have been conditioned at high relative humidity and temperature. When the adhered
systems are subjected to drying conditions at low relative humidity, a strain is induced
in the surface covering material. The tendency to buckle caused by the compressive
strain which is introduced into the surface covering by subsurface shrinkage is usually
compensated for by the adhesive; however, in many situations the adhesive eventually
fails and the surface covering buckles. The strain at which this occurs is the adhered
critical buckle strain of the system, and it is a measurable value. Consequently,
it may be used to calculate the adhesive strength as illustrated in the examples.
In appropriate circumstances, the adhesive strength value may also be projected mathematically
or graphically from other adhesive strength data.
[0037] Three types of rupture are possible, namely, rupture of the adhesive itself, which
is a loss of cohesive strength; rupture of the bond between the adhesive and the test
subsurface; and rupture of the bond between the test surface backing and the adhesive.
A determination of the type of rupture is not a feature of the present invention;
however, it is information which is often useful to the artisan.
[0038] Because, in this aspect of the invention, the surface coverings are adhered to a
subsurface with an adhesive, several of the calculation limits suggested for loose-lay
flooring no longer apply. For example, floor tile and wall tile normally would not
be rolled, and the suggested bending stiffness upper limit of ca 9 inch-pounds (1
Newton-meter) for loose-lay flooring would not be applicable to tile. Bending stiffness
values in excess of 20 inch-pounds (2.3 Newton-meters) have been measured for flooring
tiles; however, by extending the bending stiffness limits used in the calculations,
suitable adhesive strengths have been determined. From this it will be apparent that
the suggested ranges used in the calculations may be expanded as necessary to be compatible
with the materials under consideration, and that the extensions of these ranges will
not adversely affect the calculated results.
[0039] The potential energy,π, of a surface covering after buckling may be calculated as
described in the parent application according to the formula:

where C = bending resistance
e = angle of lift-off of the buckle
Q = basis weight
K = relaxed compressive (or tensile) stiffness
Lo = one half the length of the buckled area prior to application of the strain that
caused the buckle
E =. the compressive strain applied to create the buckle
[0040] The bending resistance, C, may be calculated from the bending stiffness measured
according to the Olsen Stiffness Test, ANSI/ASTM D 747, using the following equation

where M
w = the measured bending stiffness
S = the span used in the test
b = the width of the test specimen
= the angle in radians at which the measurement was taken
[0041] The critical buckle strain may be calculated mathematically by, applying the principle
of minimum potential energy. Bending stiffness values, M
w, are converted to bending resistance values, C. Upon setting the derivatives of π
with respect to 0 , and of n with respect to L
o, equal to zero, assigning values for
E and Q, and varying C and K within known limits, (or, conversely, varying E and Q
and assigning values to C and K), the equation may be solved. For example, this may
be accomplished by using the Newton-Rathson Method of solving non-linear simultaneous
equations. Flow charts for computer programs which may be used to effect these calculations
are illustrated in FIGS. 1A and 1B, and 3A and 3B.
[0042] In practicing the present invention, a number of alternatives are possible, as suggested
by the following hypothetical situations: (1) a situation where the surface covering
is used as is, and the minimum strength of the adhesive is calculated to ensure firm
adherence; (2) a situation where an adhesive is selected and the surface covering
is then modified to provide at least minimal performance characteristics in combination
with the adhesive; and (3) a situation where a surface covering is selected and modified,
and the minimum adhesive requirement is determined so that an appropriate adhesive
can be selected. Of course, these situations are provided by way of illustration,
and not by way of limitation.
[0043] In the first-described hypothetical situation, no modification occurs to the surface
covering and it is adhered to the subsurface by using an adhesive having appropriate
strength. In the past, the selection of an appropriate adhesive was quite difficult
to achieve. As explained above, although an adhesive may initially perform suitably
in a given environment, the adhesive may fail under load with time. This may be due
to a number of factors, such as changes in the adhesive or adhesive strength caused
by the environment (e.g., dampness), or to the buckling tendencies of certain surface
coverings when placed over unstable subsurfaces. For these reasons, actual testing
of adhered surface covering/subsurface systems will preferably be conducted as previously
described during which the climate is changed from humid, summer-like to dry, winter-like
conditions. These determinations can be made even for adhesives which change substantially
with time, provided that the manner of change can be quantified, and in addition,
the present invention will also permit one skilled in the art to find other alternatives
if a suitable adhesive cannot be found.
[0044] To practice this first-described aspect of the invention, it is first necessary to
estimate what subsurface dimensional change is anticipated, and then to assess the
performance characteristics of the surface covering by measuring its bending stiffness,
basis weight and relaxed tensile stiffness. The critical buckle strain of the covering
is then calculated in the usual manner. If the critical buckle strain is greater than
the subsurface dimensional change, the situation falls within the scope of the loose-lay
flooring situation described in the parent application; i.e., no adhesive would be
necessary unless the surface covering were to be used as a ceiling or a wall covering.
However, if it is less than the subsurface dimensional change, the necessary minimum
adhesive strength can be calculated. This may be done by selecting a target critical
buckle strain in excess of the subsurface dimensional change; then, using this target
value and the measured bending stiffness and relaxed compressive stiffness values,
the adhered basis weight of the structure is calculated.
[0045] As applied to this hypothetical situation, the adhered basis weight is a value which
incorporates two parameters, the actual basis weight of the surface covering and the
minimum required adhesive strength of the adhesive. For example, if the structure
is a ceiling tile, the basis weight of the tile would act counter to the adhesive;
thus, the minimum adhesive strength required for the adhesive would be the calculated
adhered basis weight plus the actual basis weight. Conversely, if the structure is
a floor structure, the basis weight would act in concert with the adhesive; thus,
the minimum adhesive strength would be the calculated adhered basis weight less the
actual basis weight. As an added consideration, it should also be recognized that
the calculated adhesive strength is that which is necessary to minimally overcome
the factors which would tend to cause the surface covering to separate from the subsurface.
Accordingly, in this, as well as other situations, it may be advisable to select an
adhesive having a greater-than-required adhesive strength so as to overcome unforeseen
factors such as detrimental environmental effects, loss of strength due to plasticizer
migration, and the like.
[0046] In the second hypothetical situation, the surface covering and the adhesive are selected,
and the adhesive strength is determined as previously described. The bending stiffness,
basis weight and relaxed compressive stiffness are measured for the unmodified surface
covering, and an appropriate target critical buckle strain, in excess of the subsurface
dimensional change, is selected. The adhered basis weight is determined depending
on the intended use by combining the basis weight and the strength of the adhesive
in an appropriate manner, as referred to above. The desired relaxed compressive stiffness
can then be calculated using these data. From this information, the surface covering
is modified in situ to give, ideally, a structure having the calculated relaxed compressive
stiffness. Information relating to in situ modification was previously described in
the parent application. Of course, safety factors may be included in these calculations,
as previously suggested.
[0047] The third hypothetical situation set forth above relates to a comparable situation,
except that the modification is achieved first and then the minimum adhesive strength
is determined by making the necessary calculations.
[0048] The in situ modifications may be be performed in a variety of ways. For example,
modification may be performed on intact coverings or on partially constructed coverings
which are later converted to surface coverings having defined characteristics. Based
on practical performance criteria, it appears to be preferred to modify the structure
and then apply the back coat because the back coat usually seals the structure. This
is especially true where seepage into an open structure might occur. Of course, the
required degree of modification may also be determined by estimating the characteristics
of individual components or combinations of individual components, or it may be achieved
by evaluating composite structures and then back-calculating the characteristics which
will be needed in future structures. As used herein, the term "in situ modification"
means modification of a surface covering by changing the structure of its reinforcement
when the latter is already in place in an at least partly formed covering. A continuous
pattern of modification is one in which there is still a continuum of reinforcing
material in the structure. A modified continuous pattern is one in which though there
is a continuum the linear nature of its pattern is disrupted, while a discontinuous
pattern is one in which there is no continuum of reinforcement. The reader is referred
to Figs. 13 and 14 of the parent application for illustrations. Combinations of continuous,
modified continuous and discontinuous patterns are also possible.
[0049] The present invention has the advantage of providing a relatively reliable way to
predict the characteristics of adhered surface coverings, and it also provides guidelines
by which the various parameters may be modified so as to predictably alter the characteristics
of such surface coverings.
[0050] The following examples will be illustrative to demonstrate, but not to limit, the
advantages of the present invention.
Example 1
[0051] This example illustrates a process for adhering a surface covering to a subsurface
wherein the surface covering is unmodified and the adhesive is evaluated according
to the present invention to ensure that it has adequate adhesive strength.
[0052] Four plastisol compositions were prepared having the formulations listed below. The
molecular weights of the resins are determinable from the specific viscosities (in
parentheses) which were measured according to ASTM D-1243.
[0053] Plastisol A Parts by

[0054] Plastisol B Parts by

[0055] Plastisol C Parts by

[0056] Plastisol D Parts by

[0057] A surface covering was prepared as follows:
A roll of #F7155 glass reinforcing material (mat), commercially available from Manville
Corporation and having a basis weight of 55 grams per square meter, was used as a
reinforcing layer. The glass reinforcing mat was passed through a knife coater where
plastisol A was deposited so as to saturate the mat. The knife coater was adjusted
to provide a gelled saturated glass layer having a thickness of 0.018 inch (0.46 mm).
The structure was passed around a heated drum with the plastisol-coated surface contacting
the drum face. As a result of this procedure, which was conducted at a drum temperature
of 285°F (141°C), the plastisol was gelled.
[0058] A layer of plastisol B 0.005 inch (0.13 mm) thick was applied to the smooth drum-finished
surface by reverse roll coating and the coated mat was gelled by heating in an oven
at 280° F (138°C). The structure was then fed through a rotogravure printer to deposit
a decorative image on the surface of the gelled plastisol B.
[0059] After the decorative printing step, a clear layer of plastisol D was applied over
the printed surface to provide a protective surface 0.010-inch (0.25 mm) thick. The
coated structure was passed through a fusion oven preheated to 380° F (193°C) to:
(1) fuse the plastisol layer D, (2) expand the gelled layer of foamable plastisol
B to about three times its applied thickness, and (3) expand the gelled, saturated
glass layer to about twice its gelled thickness. After exiting from the oven, the
fused structure was mechanically embossed to create depressed areas of about 0.010
inch (0.25 mm) in depth into the decorated surface covering. The structure was then
completed by applying about 0.008 inch (0.20 mm) of plastisol C to the back of the
embossed surface covering and fusing the plastisol around a drum heated at 325° F
(163°C) for approximately 15 to 20 seconds. Finally, the completed structure was cooled
and fed to a windup device. The measured thicknesses of the various layers of the
final structure were as follows:

[0060] The characteristics of this surface covering, measured as previously described, were
as follows:

[0061] Using these data, the critical buckle strain expected for this flooring was calculated
to be 0.0005.
[0062] This material was intended for installation over a subsurface having a subsurface
dimensional change of 0.003; accordingly, a target critical buckle strain of 0.0035.was
selected for use in the calculation. For this purpose, the computer program previously
used was modified to calculate the adhered basis weight, the general modification
being illustrated in FIGS. 3A and 3B. In addition, the upper basis weight limit was
extended to about 150 pounds per square yard (81 Kg/m
2) from the value of 10 pounds per square yard (5 Kg/m
2) previously used for calculating loose-lay flooring parameters. The measured values
for the relaxed compressive stiffness and the bending stiffness, and the desired target
critical buckle strain of 0.0035 were substituted into the equation and the adhered
basis weight was calculated to be 145.4 pounds per square yard (78.9
Kg/
m2)..
[0063] Because this material was intended for use as a floor covering, the actual basis
weight of the material (2.7 pounds per square yard or 1.5 Kg/m
2) would assist in holding the surface covering to the subsurface. Accordingly, the
minimum adhesive force necessary to adhere the surface covering to the subsurface
was calculated by subtracting 2.7 pounds per square yard (1.5 Kg/m
2) from the calculated adhered basis weight of 145.4 pounds per square yard (78.9 Kg/m
2), giving a value of 142.7 pounds per square yard (77.4 Kg/m
2). It is noted that if the surface covering had been intended for use as a ceiling
tile, the basis weight would have detracted from the adhesive strength and the minimum
adhesive strength would have been obtained by adding the actual basis weight to the
adhered basis weight.
[0064] Three adhesive candidates were selected for testing. Adhesives would normally be
selected for long-term use in a given environment; therefore, in addition to strength,
they would also be selected on the basis of their long-term compatibility with the
particle board and with the fused PVC backcoat which were used to construct the surface
covering/subsurface system. When considered on that basis, the three adhesive candidates
normally would not have been selected because their long-term compatibility with these
materials is unsatisfactory. However, because the purpose of this example was to illustrate
the ability of the present invention to differentiate between adhesives on the basis
of strength, and because the incompatibility problems were of little consequence during
the term of the test, the incompatibility problems were disregarded.
[0065] The selected adhesives were Armstrong's commercial adhesives, S-750 and S-242, and
an Armstrong experimental adhesive, referred to herein as EXP. The adhesive strength
of each of these adhesives was measured in relation to the surface covering materials
(the test vinyl backing and the test particle board subsurface) because no single
adhesive strength value is applicable to an adhesive; i.e., the adhesive strength
of an adhesive often varies depending on the materials with which it is used.
[0066] These adhesives were tested in the following manner. Commercial particle board sheets
(4 ft. x 8 ft. x 34" or 1.2 m x 2.4 m x 1.3 cm) were conditioned at 100°F (37.8°C)
and 80% relative humidity (RH) for about two weeks until the length of the boards
(measured daily) remained essentially unchanged for three days. Conditioning was then
discontinued and the temperature and humidity were changed to essentially ambient
conditions (72° F or 22.2°C and 50% RH). Pieces of the test surface covering 14 in.
(36 cm) wide and 8 ft. (2.4 m) in length were prepared, and duplicate samples for
each adhesive were adhered to the particle board sheets. The ends of the test strips
were stapled to the sheets so that the strips would be subjected to a representative
compressive stress during the test. The length of each sheet (L
s) was measured at this time. After the adhesive bond had aged under ambient conditions
for one week, the conditions were adjusted to 20% RH and 70°F (21°C). The samples
were then monitored as the particle board sheets dried out and contracted, thus placing
a compressive force on the eight-foot (2.4 meter) span of the samples. When the surface
covering samples buckled, indicating failure of the adhesive bond, the amount of sheet
shrinkage for the particle board was measured by subtracting the sheet length at failure
(L
f) from the sheet length at the time the samples were adhered to the sheets (L
s). The strain at failure was determined according to the equation
L
s-L
f = strain at failure L
s
[0067] For the purpose of this aspect of the invention, the strain at failure is referred
to as the adhered critical buckle strain, which was defined earlier.
[0068] It was noted that all three adhesives failed differently during the test: The S-750
adhesive lost its cohesive strength and left adhesive residue on both surfaces; the
S-242 adhesive remained on the particle board leaving the backing essentially free
of adhesive residue; and the EXP adhesive remained on the surface of the backing and
left essentially no residue on the particle board.
[0070] These values indicated that the S-750 and EXP adhesives would not perform satisfactorily
because their adhesive strengths were less than the minimum strength as determined
from the earlier calculation (142.7 pounds
[0071] per square yard or 77.4 Kg/m
2). The third adhesive, S-242, had an adhesive strength which was in excess of the
calculated value, indicating that it would be suitable to adhere the test surface
covering to the particle board subsurface.
[0072] To test the validity of this determination, particle board sheets were conditioned
in an environmental test chamber at 80% RH and 72°F (22.2°C) for four weeks, after
which a 12 ft. x 10 ft. (3.7 m x 3.0 m) subsurface was built over a plywood support
surface according to standard NPA installation directions. A 12 ft. x 10 ft. (3.7
m x 3.0 m) piece of surface covering was then adhered to the subsurface using the
S-242 adhesive. It is emphasized that the adhesive was applied exactly as it was for
the above-described strip test, and exactly according to the application directions.
[0073] After the adhesive had aged, a six-week drying cycle was commenced to induce the
particle board to shrink by its subsurface dimensional change factor of 0.003. Although
certain minor deficiencies were noted . during the test, these were not attributable
to the present invention, and the installation was deemed to have performed satisfactorily.
As an example of one deficiency, surface coverings of the type illustrated in this
Example 1 are commonly affected by the presence of bubbles, or air pockets, between
the surface covering and the subsurface. These pockets prevent adequate adhesion in
certain small areas which eventually result in the presence of noticeable bubbles
or blisters. These defects are attributable to the manner in which the test materials
are installed and/or to a lack of initial adhesion, and are not attributable to the
invention itself.
Example 2
[0074] This example will illustrate the situation where an adhesive is selected and a selected
surface covering is modified so that it will be suitable for use with the adhesive
when adhered to a given subsurface.
[0075] A surface covering was prepared essentially as described in Example 1, except that
the glass mat was modified in situ after the embossing step, before the backing coat
(plastisol C) was applied.
[0076] This surface covering was selected for use over a particle board subsurface having
a subsurface dimensional change of 0.0015. The EXP adhesive was selected and the adhesive
strength of this adhesive was determined as described in Example 1 to be 13.0 pounds
per square yard (7.1
Kg/m
2).
[0077] The basis weight, bending stiffness and relaxed compressive stiffness were measured
for the selected surface covering to give the following values:

From these data, the unmodified surface covering was calculated to have a critical
buckle strain of 0.0005. A target critical buckle strain of 0.002 was selected for
use over the subsurface having an expected subsurface dimensional change of 0.0015.
[0078] The surface covering in this example was also intended for use as a floor covering.
Accordingly, the adhered basis weight was calculated by adding the adhesive strength
of 13.0 pounds per square yard (7.1 Kg/m) for the adhesive and the actual basis weight
(2.6 pounds per square yard or 1.4
Kg/m
2) of the surface covering, giving a value of 15.6 pounds per square yard (8.5
Kg/
m2).
[0079] For this example, the computer program illustrated in FIGS. 1A and 1B was used to
calculate the relaxed compressive stiffness, except that the upper limit for the basis
weight was expanded such that it was in excess of the calculated adhered basis weight
of 15.6 pounds per square yard (8.5 Kg/m
2). The measured bending stiffness, the adhered basis weight, and the target critical
buckle strain were substituted into the equation to provide a calculated relaxed compressive
stiffness value of 648 ppiow (113,500 N/m). Accordingly, modification of the surface
covering was required in order to reduce the relaxed compressive stiffness from the
initially measured value of 1,274 ppiow (223,100 N/m) to a value less than or equal
to 648 ppiow (113,500 N/m).
[0080] The surface covering was modified by cutting 1-inch (2.5 cm) diamond-shaped elements
into the reinforcing layer from the back of the surface covering. The partial structure,
was fed upside down at room temperature through a pair of pinch rolls, the upper roll
being an embossing roll especially designed to perforate the glass reinforcement and
the lower roll being a smooth steel back-up roll. The roll pressure was adjustable
such that modification could be varied from slight modification at low pressure to
substantial modification at higher pressure. For purposes of the present test, the
nip pressure was adjusted to 120 pounds per lineal inch (21.4 Kg/cm).
[0081] The upper embossing roll was designed with a pattern comparable to that shown in
FIG. 2; however, the pattern was angled at 45 degrees to the machine direction to
create a diamond-shaped element pattern. The raised portions of the embossing roll
were 0.045 inch (1.14 mm) high and 0.025 inch (0.64 mm) wide.
[0082] After the material had passed through the nip, a test piece was placed in tetrahydrofuran
solvent to dissolve the polymeric material and recover the modified glass mat. Visual
inspection of the mat showed that the 1-inch (2.5 cm) diamond elements were almost
completely separated from the continuum of glass, but a few strands still held the
elements in place. The structure was completed as described in Example 1 through application
of plastisol coat C. The relaxed compressive stiffness of the completed, modified
structure was found to be 623 ppiow (109,100 N/m).
[0083] To evaluate the effect of this modification, the surface covering was installed over
the selected particle board subsurface in the manner described in Example 1 and the
adhered system was subjected to a six-week cycle during which the particle board shrank
by about a factor of 0.0015, the expected subfloor dimensional change value. The installation
performed satisfactorily and there was no evidence of buckling.
Example 3
[0084] This example will illustrate the modification of a surface covering, followed by
selection of an appropriate adhesive which is compatible with the characteristics
of the modified covering.
[0085] A surface covering was partially prepared, modified, and then completed as described
in Example 2. The following physical properties were measured for the modified structure:

[0086] Using these data, a critical buckle strain of 0.001 was obtained for the in situ
modified structure. A target critical buckle strain of 0.0035 was selected for use
in the calculation based on a proposed particle board subfloor having a subfloor dimensional
change of 0.003.
[0087] The modified computer program illustrated in FIGS. 3A and 3B was used to calculate
the adhered basis weight by inserting the measured relaxed compressive stiffness and
bending stiffness values, and the target critical buckle strain of 0.0035, into the
equation. The adhered basis weight was calculated to be 35.8 pounds per square yard
(19.4 Kg/m
2). This surface covering was also intended for use as a floor covering. Accordingly,
the measured basis weight of 2.6 pounds per square yard (1.4 Kg/m
2) was subtracted from the calculated adhered basis weight of 35.8 pounds per square
yard (19.4 Kg/m
2) in order to give a required minimum adhesive strength of 33.2 pounds per square
yard (18.0 Kg/m
2) for the adhesive.
[0088] The adhesive strengths for each of the three adhesives used in Example 1 were also
applicable in this example because the materials which were being adhered together
were identical. Accordingly, the above calculation indicates that two of the three
adhesives (S-242 and S-750)'would be suitable to adhere the modified structure in
this example to the intended subsurface.
[0089] A 10 ft. x 12 ft. (3.0 m x 3.7 m) surface covering sample was adhered to a particle
board subsurface using the S-750 adhesive and tested as described above for six weeks
under simulated environmental test conditions which would induce a subfloor dimensional
change of 0.003. Satisfactory performance was found and there was no indication of
buckling.
[0090] Our invention is not restricted solely to the descriptions and illustrations provided
above, but encompasses all modifications envisaged by the following claims.
1. A process for adhering a surface covering to a subsurface having an ascertainable
subsurface dimensional change such that said surface covering will accommodate subsurface
movement without buckling, said process comprising the steps of
(a) selecting a surface covering, the critical buckle strain of the selected covering
being less than the subsurface dimensional change;
(b) selecting a target critical buckle strain which is greater than the subsurface
dimensional change;
(c) measuring the relaxed compressive stiffness, the bending stiffness and the basis
weight of said selected covering;
(d) calculating the adhered basis weight for a surface covering having the measured
bending stiffness, the measured relaxed compressive stiffness, and a critical buckle
strain that is equal to the target critical buckle strain;
(e) calculating the minimum adhesive strength which will be necessary to adhere said
surface covering to said subsurface in a manner which will prevent buckling;
(f) selecting a suitable adhesive, and
(g) adhering said surface covering to said subsurface.
2. A process for modifying a surface covering comprising at least one reinforcing
layer whereby it can be adhered without buckling to a subsurface having an ascertainable
subsurface dimensional change, said process comprising the steps of
(a) selecting a surface covering comprising at least one reinforcing layer, the critical
buckle strain of said selected covering being less than the subsurface dimensional
change;
(b) selecting an adhesive having a determined adhesive strength;
(c) measuring the basis weight, the bending stiffness and the relaxed compressive
stiffness of said selected covering;
(d) selecting a target critical buckle strain which is greater than the subfloor dimensional
change;
(e) calculating the adhered basis weight which would be obtained if said selected
covering were adhered to said subsurface using said adhesive;
(f) calculating the relaxed compressive stiffness for a modified surface covering
having the measured bending stiffness, the calculated adhered basis weight, and a
critical buckle strain which is equal to the target critical buckle strain, and
(g) modifying said covering in situ such that it has a relaxed compressive stiffness
value which is not greater than the calculated relaxed compressive stiffness value,
whereby when the modified surface covering is adhered to said subsurface using said
. adhesive, it will accommodate subsurface movement without buckling.
3. A process for modifying a surface covering comprising at least one reinforcing
layer, the modified covering being suitable to accommodate the subsurface movement
of a subsurface having an ascertainable subsurface dimensional change when said modified
covering is adhered to said subsurface, said process comprising the steps of
(a) selecting a surface covering comprising at least one reinforcing layer, the critical
buckle strain of said selected covering being less than the subsurface dimensional
change;
(b) modifying said covering in situ such that the critical buckle strain of the modified
covering is greater than the initially measured critical buckle strain, but less than
the critical buckle strain which would equal or exceed the subsurface dimensional
change;
(c) selecting a target critical buckle strain which is greater than the subsurface
dimensional change;
(d) measuring the bending stiffness, relaxed compressive stiffness and basis weight
of said modified covering;
(e) calculating the adhered basis weight for a covering having the measured bending
stiffness, the measured relaxed compressive stiffness, and a critical buckle strain
that is equal to the target critical buckle strain; and
(f) calculating the minimum adhesive strength necessary to adhere said modified covering
to said subsurface, whereby when a suitable adhesive having an adhesive strength at
least as great as said calculated adhesive strength is selected; said modified structure
can be adhered to said subsurface in a manner which will prevent buckling.
4. A surface covering which is suitable to be adhered with an adhesive to a subsurface
without buckling, said surface covering comprising
(a) a matrix material, and
(b) at least one reinforcing layer disposed therein which has been modified in situ
such that said surface covering has a critical buckle strain which is less than the
subsurface dimensional change of said subsurface, the difference between said critical
buckle strain and said subsurface dimensional chanqe being such that the adhesive
strength of a selected adhesive in combination with the basis weight of said surface
covering will be sufficient to provide an adhesive bond having a strength which is
not less than the adhered basis weight calculated for said surface covering.
5. The invention as set forth in claim 4 hereof wherein said surface covering is obtained
by the process set forth in claim 2 or claim 3.
6. A composite structure comprising a surface covering, a subsurface and an adhesive
which adheres said surface covering and said subsurface together, said surface covering
comprising
(a) a matrix material, and
(b) at least one reinforcing layer disposed therein which has been modified in situ,
the critical buckle strain of said surface covering being less than the subsurface
dimensional change of said subsurface, the difference between said critical buckle
strain and said subsurface dimensional change being such that the adhesive strength
of said adhesive in combination with the basis weight of said surface covering provides
an adhesive bond having a strength which is not less than the adhered basis weight
calculated for said surface covering.
7. The invention as set forth in claim 6 hereof wherein said composite structure is
obtained by the process set forth in claim 2 or claim 3 and subsequently adhering
said surface covering to said subsurface using said selected adhesive.
8. The invention as set forth in claim 1 hereof wherein said surface covering comprises
at least one reinforcing layer.
9. The invention as set forth in any one of claims 2 to 7 hereof wherein said modification
is achieved using a continuous modification pattern.
10. The invention as set forth in any one of claims 2 to 7 hereof wherein said modification
is achieved using a modified continuous pattern.
11. The invention as set forth in any one of claims 2 to 7 hereof wherein said modification
is achieved using a discontinuous modification pattern.
12. The invention as set forth in any one of claims 2 to 7 hereof wherein said modification
is achieved using a discontinuous modification pattern in combination with a continuous
or a modified continuous pattern.
13. The invention as set forth in any one of claims 2 to 12 hereof wherein said reinforcing
layer is a glass reinforcing layer.
14. The invention as set forth in any one of claims 2 to 13 hereof wherein each said
reinforcing layer has a basis weight of from 15 to 160 grams per square meter, especially
from 20 to 80 grams per square meter.