Floor covering with inorganic wear layer

BACKGROUND OF THE INVENTION
The invention relates to a floor covering. More particularly, the invention relates to a floor covering having an inorganic wear layer which preferably has been deposited on a support structure by a low pressure environment deposition technique. Further, the invention is directed to a multilayered floor covering in which each layer contributes to the wear performance and installation characteristics and affects the performance of the other layers.
Floor coverings having wear layers are well known in the art. Such wear layers protect the decorative layer of the floor coverings and lengthen the useful life of the floor covering. With the exception of ceramic tile which are rigid and must typically be installed on a mortar bed and metal floors such as steel plates, neither of which have a wear layer per se, inorganic material is not used as the wear surface of floor coverings. Inorganic materials are typically considered too brittle to be walked on; particularly if a "thin" layer were to be placed over a flexible or conformable support layer. Further, low pressure environment deposition techniques have not been applied to the manufacture of floor coverings.
Reduced pressure environment techniques for depositing films of hard inorganic materials include sputtering, plasma polymerization, physical vapor deposition, chemical vapor deposition, ion plating and ion implantation. Hard inorganic materials which can be prepared using these techniques include metals, metal oxides, metal nitrides and mixtures thereof; such as aluminum oxide, silicon oxide, tin and/or indium oxide, titanium dioxide, zirconium dioxide, tantalum oxide, chromium oxide, tungsten oxide, molybdenum oxide, aluminum nitride, boron nitride, silicon nitride, titanium nitride, and zirconium nitride, as well as metal halides, metal pnictides and metal chalogenides.
Often the partial pressures of key gases in the deposition environment are controlled to effect chemical reactions between depositing metal species. Therefore, a film formed on a substrate by reactive sputtering or reactive deposition can be a compound derived from a metal and a controlling gas, i.e., aluminum oxide produced by sputtering aluminum in oxygen. Sometimes the controlling gases are used to sustain a plasma in the deposition environment. Ion assisted deposition is a technique in which the controlled gas is ionized and is used to bombard the deposition surface to modify the morphology and physical properties of the resulting film.
A critical review of vapor deposition technology related to hard coatings was presented by J. E. Sundgren and H. T. C. Hentzell in J. Vac. Sci. Tech. A4(5), September/October 1987, 2259-2279. A more complete review of techniques involved in formation of thin films in reduced pressure environments is the book edited by J. L. Vossen and W. Kern, Thin Film Processes, Academic, New York, 1978.
Recent articles on thin film preparation include Yabinouitch, E., Gmitter, J. P., Haubison, J. P. and Bhat, R., Appl. Phys. Letter, 51(26), Dec. 28, 1987, 2222-2224 on etching Al/As to form free standing GaAlAs films; Clevenger, L. A., Thompson, C. V. and Cammarata, R. C., Appl. Phys. Letter, 52(10), Mar. 7, 1988, 795-797 on using commercial photoresists as supports; Ryszard Lamber, Thin Boehmite Films: Preparation and Structure; Journal of Materials Science Letters, 5(1986), 177-178; and Huling and Messing, J. Am. Ceram. Soc., 71(4), 1988, C222-C224, on coating on camphor and subliming to obtain free standing mullite.
Patents dealing with thin film deposition include: U.S. Pat. No. 4,604,181 and 4,702,963.
Reduced pressure environment techniques have been used to coat plastics materials such as plastic bags to improve gas impermeability. However, such coatings have been limited to about 0.5 microns in thickness.
While reduced pressure environment techniques have been used to form hard coatings on surfaces such as automobile parts, there has been no suggestion that such coatings could be successfully used as wear surfaces for floor coverings. In fact, such coatings tend to be brittle when applied in a substantial thickness. Thus, one skilled in the flooring art would not expect reduced pressure environment deposited materials to function adequately as a floor covering, particularly in the thickness deemed necessary to protect the decorative layer of a floor covering.
Alliance Wall manufactures and sells wall coverings in which porcelain enamel is fused to a steel sheet. However, use of a material as a wall covering does not suggest that it would be acceptable as a floor covering. Again, one skilled in the flooring art would not expect a thin sheet of ceramic to withstand the long term abuse to which flooring is subjected, particularly when laid over a resilient support structure and walked on by a woman in high heels.
SUMMARY OF THE INVENTION
An object of the invention is to provide a floor covering that has the appearance retention of ceramic tile (including stain resistance and gloss retention), and resists cracking and brittle failure.
A further object is to provide a floor covering having an inorganic wear layer which is flexible enough to be rolled around a reasonably sized mandrel and therefore can be installed in a manner similar to present resilient floor coverings.
Another object is to provide a floor covering laminate having the above listed features and which is conformable to the subfloor on which it is laid.
Such a floor covering has been made by depositing a wear layer of a hard inorganic material on a support by a reduced pressure environment technique. The preferred reduced pressure environment technique is ion assisted physical vapor deposition; and the preferred support is multilayered.
The preferred hard inorganic material is a metal oxide or metal nitride, most preferably aluminum oxide, silicon oxide and silicon nitride. Aluminum oxide, silicon oxide and silicon nitride form films which are colorless, clear and of hardness similar to the dirt to which the floor covering is normally subjected.
Preferred supports include a metal component such as a foil, a film or a sheet. The metal support may be from 0.001" to 0.25" thick, preferably 0.003" to 0.1" thick. The preferred support is a stainless steel sheet of at least 0.007 inches in thickness. Although a low carbon steel may be used its performance is poorer. Preferably, the support includes a decorative layer of fused glass or ceramic frit overlying the metal component.
Since the glass or ceramic is a metal oxide which can be deposited by a reduced pressure environment technique, the wear layer can be formed from a glass or ceramic material. That is, the decorative layer can be the wear layer.
Depositing a hard inorganic material on surface of a plastic, rubber or mineral/binder system support substrate improves the wear resistance and falls within the scope of the present invention. The plastic may be either a thermoset or thermoplastic. The preferred thermoplastic is polyethylene terephthalate. The preferred thermoset plastic is a crosslinked reinforced polyester such as polyester sheet molding compound sold by Premix, Inc. The thickness of the support should be between 0.0005" and 0.25".

BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a perspective view of a first embodiment of the present invention.
FIG. 2 is a perspective view of a second embodiment of the present invention.
FIG. 3 is a perspective view of a third embodiment of the present invention.
FIG. 4 is a cross-sectional view taken along line 4--4 in FIG. 3.
FIG. 5 is a cross-sectional view of a fourth embodiment of the present invention.
FIG. 6 is a schematic representation of test setup to measure rupture strain.

DETAILED DESCRIPTION OF THE INVENTION
Broadly, the invention is a floor covering having a hard inorganic material wear layer and a support including metal or plastic. While the preferred floor covering is a flexible laminate which has been deposited on a support by a reduced pressure environment technique and which permits installation similar to conventional resilient flooring, including resilient tiles; the invention is intended to include rigid floor coverings having a wear layer of reduced pressure environment deposited hard inorganic material, and conformable floor coverings having a glass or ceramic material applied to a metal support by means other than a reduced pressure environment technique.
Metals and hard inorganic materials such as ceramics have unique properties. Properly selected ceramics are hard enough to resist being scratched by the grit particles in dirt. Properly selected metals should be hard enough to support the ceramic and yet be flexible. Such a laminate can be made in an atomistic deposition chamber by depositing on a thin, properly tempered steel. This laminate could then be mounted on an organic-polymer support layer to form a flooring structure. The support layer conforms to the subfloor irregularities and accommodates lateral movement of the subflooring structure. Although vacuum techniques could be used in making such a flooring structure, current technology would enable it to be made on a continuous, air-to-air production line.
No organic surface, either currently in existence or envisioned, possesses sufficient resistance to loss of gloss and to other physical damage to fully meet desired performance. Thick (1/4inch), hard ceramic tiles (Mohs hardness of at least 7 and preferably 8.5) resist loss of gloss and other physical damage extremely well.
The Mohs hardness of grit particles in dirt probably ranges between 6 (silicates) and 7 (silica). A rule of thumb among tribologists is that if a surface is 1.5 Mohs units harder than a grit particle, the surface will not be scratched by the grit particle. This applies when the grit particle is between two surfaces of equal hardness. In a flooring situation, the grit particle is usually between the relatively soft bottom surface of a shoe and the floor surface. Therefore, the maximum downward force on the grit particle is the resistance the bottom of the shoe offers to penetration by the grit particle. The softer the bottom of the shoe, the less downward force exerted on the particle. Consequently, the difference in hardness between the grit particle and the flooring surface may not need to be quite as large as 1.5 Mohs units. In any case, a Mohs hardness of 8.5 is a reasonable goal for the ceramic film. However, wear layer of Mohs hardness of about 5 or 7 have been shown to retain gloss level despite larger scratches. Prior art organic wear layers have a Mohs hardness of less than 3. Therefore a Mohs hardness of 3 or greater will yield an improvement.
If formed by atomistic deposition, the ceramic-film wearlayer envisioned for the laminate structure would be expected to be essentially stain proof and to retain its gloss extremely well. The film would be expected to be essentially stain proof because such films provide excellent corrosion resistance for the substrates on which they are deposited. The film retains its gloss and resists damage from grit particles because it can be made sufficiently hard, approaching the hardness of the grit particles in dirt, and may be supported on a support having proper stiffness.
Although ceramic film has both stain resistance and gloss retention, its brittleness has prevented it from being used as a wear layer in a resilient floor covering. Brittleness makes the ceramic film susceptible to serious damage. However, by combining the ceramic film with a support such as a sheet of metal or plastic with the proper characteristics, a ceramic film may be used. If the support is sufficiently strong to give the floor covering the ability to support a uniform 125 lbs/sq ft load with a deflection of not more than one-five hundredths of the span, the floor covering may be free standing. The ceramic tile does not have the ability to perform when supported in a free standing manner. Laminate must have the necessary physical properties as discussed below.
In order to understand why such a laminate should solve the problem of brittle damage, it is useful to divide the types of forces causing damage into two categories: (1) localized pressure and (2) impact.
Localized pressure occurs when a grit particle is pressed downward against the ceramic surface. If the particle can force the ceramic film down into the support layer on which it has been deposited, the ceramic film is put into tension and fails. Ceramics, although strong in compression, are weak in tension. To avoid such failure in tension, the support layer must resist being indented when the grit particle is pressed against the ceramic film. Actually, all the ceramic film does in protecting the support layer from indentation is to spread the force over a greater area before that force reaches the support layer. Hardened steel appears to combine the desired hardness (up to a Mohs of almost 7) and flexibility. Although lacking the hardness of steel, some organic polymers, particularly engineering polyesters, have provided adequate support.
A ceramic/metallic laminate also possess the properties needed to resist impact. Impact occurs when a heavy object strikes the floor. Damage is most likely to occur when the pressure (that is force per unit area) is large enough to cause an indentation. Here the tensile strength of the steel should resist putting the ceramic in tension.
An additional property that the support layer should possess is the ability to produce a gradual contour rather than an abrupt contour, both when a grit particle exerts a force on it through the ceramic film and when it is subjected to impact. Calculations nave shown that for a given vertical displacement, a gradual contour subjects the ceramic film to less tension than does the abrupt contour. In order to produce a gradual contour, the support layer should be flexible but not limp. Two materials that possess the desired properties are properly tempered spring steel and polyester based sheet molding compounds.
The ceramic film should have hardness at least of about 6 Mohs and good strength. To possess these attributes, the ceramic must have the proper microstructure. In films formed by atomistic deposition, desirable microstructure can be attained by increasing the temperature and the bombardment energy. One of the advantages of using a steel support layer is that a high enough temperature can be used to get optimum microstructure.
The ceramic film should be applied so that it is under compression. This can be accomplished by depositing the metal-atom portion of the ceramic first and then adding the other element later, either in the same step or in a second step. Using a two-step process allows better control for deposition of the nonmetallic atoms.
The ceramic/metallic laminate is preferably adhered to a conformable support layer. This support layer must be hard enough to support the ceramic/ metallic laminate but must also be able to conform to any irregularities in the subfloor. To perform in a superior manner, the conformable support layer should be capable of inelastic deflection, i.e., capable of permanent deflection with or without residual forces such as applied by adhesives.
In addition, if used in resilient sheet goods it must accommodate some lateral movement of the subfloor. To be able to perform over all subfloors including particleboard, the floor covering should have a rupture strain in excess of 0.3%. Due to seasonal changes including temperature and humidity, particleboard subfloors expand and contract about 0.3% during the year. Plywood expands and contracts about 0.15%. Therefore, to perform adequately over a wooden subfloor, the floor covering including the wear layer should have a critical buckle strain of at least 0.1% and preferably at least 0.3%. Floor coverings of the present invention having plastic support structures meet this requirement.
The support layer preferably is typically made from an organic polymer. It is desirable to select the polymer so that its viscoelastic character will allow it to conform to the floor and still enable it to resist indentation by a rapid impact.
Surface contours can readily be incorporated by embossing the metallic substrate layer before application of the ceramic film. Incorporation of a pattern could be done most readily by printing the pattern on the metallic substrate before deposition of the ceramic film. Some of the ceramic films that can be deposited atomistically are colored, and they may be applied in patterns by use of stencils.
Although the focus of this invention is on atomistically deposited ceramics, the concept of a thin flexible metallic substrate layer could be used with other types of ceramics. Colored ceramic glazes or inks used in conventional ceramic technology could be applied in a pattern on the metallic substrate layer to form a wearlayer in place of the atomistically deposited ceramic film.
The basic concept is combining thin, hard wear surfaces with decorative, support structures to produce unique wear-resistant flexible flooring products. The flooring products have the appearance retention approximating that of ceramic tile but are light weight and easier to install.
A series of inorganic oxides and nitrides (including aluminum oxide and silicon oxide) has been used as the thin, hard inorganic wear layer. The variety of materials used for the support layers include combinations of metals, plastics, rubber and mineral/binder systems. The means of decoration include glass frits, holograms, sublimable dyes and pigmented inks. The plastics, rubber and mineral/binder systems may be through color. Outstanding performance has been demonstrated in an embodiment consisting of three microns aluminum oxide over ten microns glass decorative layer on seven mils tempered steel shim stock bonded either to a filled vinyl tile or a layer of rubber, and also in an embodiment consisting of three microns of aluminum oxide over a sublimable ink decorated polyester sheet molding compound (PSMC). Aluminum oxide coated PSMC resists scratches better than any organic or organic/inorganic coating tested.
Since each layer of the floor covering laminate affects performance, a layer of rotogravure ink will change the appearance retention of a wear layer on a plastic support. Therefore, inks, such as sublimable inks, which will diffuse into the support layer are preferred.
The advantages of the flooring products of the present invention include an appearance retention in traffic environments in a product which can be light in weight, which can be either rigid or conformable, which can be thinner than products currently in the market place, which can be flexible, which can be more resilient than ceramic tile, and which can be installed with conventional resilient-flooring tools.
One preferred embodiment of the floor covering 1 is shown in FIG. 1. The support 2 is a metal, plastic, rubber or mineral/binder system. A wear layer 3 of hard inorganic material is deposited on the support by a reduced pressure environment technique. A decorative layer 4 is deposed between the support layer and the wear layer. The preferred metal is stainless steel. While such metals as ferroplate, brass/ferroplate, steel/ferroplate, chromium-plated brass and 01 steel have been used, any flexible but stiff support can be used.
The preferred thickness of the support is from about three to about nine mil, most preferably about five to about seven mil. Two and four micron alumina wear layers on three, five and seven mil tempered shim steel did not crack even when the resulting laminate was supported by a deformable rubber of Shore hardness 70 and walked on by women in high heels. The three-mil substrate could be pierced by high heels.
The preferred Young's modulus is about 3.times.10.sup.7 lbs./inch.sup.2. A modulus of this value or less ensures that the laminate is sufficiently flexible to bend around a 2-inch mandrel without the wear layer cracking, even when the wear layer is on the convex side. Preferably, the floor covering is sufficiently flexible to bend around a 20-inch mandrel without cracking.
The support substrate may also be a decorated or undecorated plastic, rubber or mineral/binder system provided the support layer is sufficiently rigid. The support layers tested include a polyester sheet molding compound (PSMC), rigid polyvinylchloride (PVC) on a tile base, polyethersulfone on a glass base, glass fiber reinforced polyester, fiber filled phenolic, polyetheretherketone with and without a glass base, polyimide on a glass base, polymethylmethacrylate, a photographic polyester on a glass base, Teflon, and PVC on PSMC. A preferred polyester support substrate material is PSMC or polyethylene terephthalate. A fiber filled polyester is more stable and yields fewer cracks.
The thickness of the wear layer must be at least one micron. Preferably the thickness of the wear layer is at least about three microns. Thickness of less than three microns tend to fail more frequently.
Hardness of the wear layer equal to and preferably greater than that of silica also is desirable. Preferably the hardness is at least 6 Mohs, and more preferably 8.5 Mohs.
The invention includes wear layers of metal, metal oxides and metal nitrides. The preferred compositions include Al.sub.2 O.sub.3, SiO.sub.x, AlN, Si.sub.3 N.sub.4 and TiN. Flooring structures with five to eight microns of Al.sub.2 O.sub.3 and SiO.sub.x supported on an undercoated, reinforced polyester substrate had gloss retention superior to currently marketed wear layer materials. Although individually visible scratches were apparent, the scratches did not affect gloss retention. The scratches can be eliminated or at least minimized by obtaining a good match between the mechanical properties of the substrate and the wear layer. Gloss retention and overall appearance retention is increased by increasing wear layer hardness and substrate hardness. Therefore, Si.sub.3 N.sub.4 may be a superior wear layer to Al.sub.2 O.sub.3.
The decorative layer 4 is a glass or ceramic frit, or pigment. The use of printable inks enables the creation of intricate designs. However, since the wear layer materials may be colored, the wear layer and decorative layer may be combined and a multi-colored wear layer can be deposited with a low pressure environment technique with the use of stencils.
The structure of the FIG. 1 embodiment is acceptable for a resilient flooring structure which is rolled for storage and transport to the installation site, provided the laminate is sufficiently flexible. However, if the flooring structure is a 12.times.12 inch tile having a rigid support structure, the tile may not be capable of conforming to the irregularities of a wood subfloor and therefore may require installation procedures similar to ceramic or marble.
To overcome this disadvantage the laminate may be bonded to a resilient or conformable layer 5 as shown in FIG. 2. The conformable layer 5 has dimensions slightly greater than the laminate. This allows for the difference in thermal expansion between the subfloor and the laminate. The conformable layer is capable of inelastic deflection under gravitational forces so that over a reasonable length of time, the lower surfaces of the laminate contacts the subfloor over substantially the entire surface area. The conformable layer is capable of conforming to the contour of the subfloor, including a 1/16" ledge between two plywood sheets forming the subfloor.
The sharp corners of the FIG. 2 embodiment may cause problems since the tiles cannot be laid in a perfectly flat plane. Therefore, the corners tend to snag the soles of shoes. To avoid this problem, the tile may be formed as shown in FIGS. 3 and 4. The laminate of support structure 2, decorative layer 4 and wear layer 3 is formed. Then the laminate is press molded into a cup-shape and bonded to the resilient support base 6. The sides 7 of the laminate are substantially perpendicular to the plane of the conformable layer and are adjacent the sides of the conformable layer.
In another embodiment shown in FIG. 5, the conformable layer 8 has alignment marks 9 on the upper exposed surface. The tiles 1 are bonded to the conformable layer in alignment with the marks to give a pleasing decorative appearance and a discontinuous wear surface. The discontinuities improve flexibility of the floor covering and may extend down to a micron scale.
The following examples, while not intended to be exhaustive, illustrate the practice of the invention. Procedure for the Preparation of Vapor Deposited Coatings Coating Materials. Metals and metal oxides were obtained in 99.9% nominal purity from standard industrial sources. Water was removed from gases using molecular sieve traps. Al.sub.2 O.sub.3 (99.99%) and SiO.sub.2 (99.99%) were obtained from E. M. Industries; ZrO.sub.2 (99.7%) and Ta.sub.2 O.sub.5 (99.8%) was obtained from Cerac, Inc.; TiO.sub.2 (99.9%), was obtained from Pure Tech, Inc.
Apparatus.
The deposition system (Denton DV-SJ/26) included a 66 cm wide high vacuum bell-jar assembly; a high speed pumping system (CTI Cryogenics CT-10 cryopump and Alcatel ZT 2033 mechanical pump); an electron-beam vaporization source (Temescal STIH-270-2MB four-hearth "Supersource", with an 8 kWatt Temescal CV-8 high-voltage controller and e-beam power supply and Temescal XYS-8 sweep control); a resistively heated vaporization source (Denton Vacuum, 4 kWatt); a cold cathode ionization source (Denton Vacuum model CC101 with both CC101BPS and CC101PS biased and unbiased power supplies); a residual gas analyzer (Inficon Quadrex 200); a quartz crystal type deposition rate controller (Inficon IC6000); four eight inch circular deposition targets affixed to a planetary rotation sub-system; and a 10" diameter stainless steel aperture for focusing the e-beam (or thermally) evaporated material and the ion plasma on the same deposition surface. The various power supplies, pressure and gas flow monitors were operated either automatically using Denton's customized process control system, or manually. Typically, a deposition run began with an automated pump-down process, was followed by a deposition process controlled by the IC6000 and ended with an automated venting cycle.
Deposition Process.
The following general procedure was followed for all deposition runs. Following evacuation to .ltoreq.1.0.times.10.sup.-5 Torr the temperature of the chamber, as measured by a centered thermocouple at planet level, was adjusted to the desired deposition temperature and the planetary rotation was started. Next, Ar gas was admitted to increase the chamber pressure to about 1.times.10.sup.-4 Torr, and a plasma 300-600 mAmps/300-600 Volts was initiated at the cold cathode source (current density between 95 and 500 u-amps//cm.sup.2) which was used to sputter-clean the substrates, in situ, for five minutes. The deposition process was thereafter controlled by an IC6000 process which typically included parameters such as heating rates and times, material densities, desired deposition rates and thicknesses, and the number of layers desired. Prior to deposition, the substrates were shielded from the metal, or metal oxide source. Ion bombardment with an ion plasma began and the shields were removed simultaneously when the IC6000 signaled that the metal or metal oxide had been heated to the temperature appropriate for vaporization. A quartz crystal microbalance provided input for the IC6000 feedback loop system which provided deposition rate control for the remainder of the process. After deposition of a specified thickness, the ion source was turned off, the shields replaced, and the vapor sources allowed to cool.
Rupture Strain Test for Thin Ceramic Coatings
One surprising feature of the present invention is the rupture strain of the thin hard inorganic coatings of the present invention. Obtaining the rupture strain of a thin, hard inorganic film or coating such as a ceramic is a difficult task as the coating is not thick enough to be self-supporting to be tested with conventional apparatus. Among the properties of yield stress, yield strain, modulus of elasticity, rupture or ultimate strain and Poisson's ratio, the yield strain is of most importance as the wear layer will undergo strain as determined by the underlying load support structure. To create a support structure, it is necessary to determine how much strain can be tolerated by the wear layer and then make design adjustments of the support parameters so that this strain will not be attained in service.
Ceramics are brittle and characteristically, the yield strain is close to, and in a practical sense, is equal to the ultimate or rupture strain. A ductile region does not exist between yield and rupture. This condition makes the test more definitive as rupture is more readily detected than yield, i.e., a crack is observed at the ultimate strain or rupture.
An evaluative test for measuring the ultimate strain to brittle fracture in a thin ceramic film was developed. The test is parasitic in that it relies on a host to produce the elongation strain in the ceramic coating. A thin, highly tempered steel strip is coated with a very much thinner coating of the wear layer (ratio of thicknesses of 250 to 1). The steel strip is bent in a cantilever fashion and being so thick compared to the coating, its bending performance is not affected by the presence of the coating. By measuring the deflection of the cantilever, the surface strain of the bent steel can be calculated by elastic mechanics equations. The coating will experience the same elongation strain as the surface of the steel. The beam is progressively deflected increasing the surface strain of the steel. When the rupture strain of the coating is attained, the coating ruptures by cracking which is visually evident. Measurement of the deflection of the beam and the position along the beam where the crack occurred are sufficient data to calculate the strain when the crack occurred.
The credibility of the test is dependent upon the following items: (1) the coating must be 100% and adhered to the cantilever surface, (2) the deflection of the beam must be small to insure accuracy with use of elastic beam formulae and (3) the yield strain of the cantilever beam must be greater than the rupture strain of the coating.
The detection of a crack and its position must be accurately determined. Detection of a crack in a three micron transparent film requires scrutiny. Observance at 40.times. magnification and illumination by collimated light appears to be necessary to discover the existence of a typical tension crack.
FIG. 6 depicts the instrument setup to detect and measure the position of the rupture cracks in the wear layer coating. The clamp 10 holds the specimen 11- in a horizontal reference plane indicated by dashed line 12. Micrometer 13 both deflects and measures the distance of deflection ye. The cracks 14 in the wear layer 15 are observed with the aid of microscope 16 and collimated light source 17.
The length of the beam and its thickness are inter-related and wide variations of the two are possible. A length of two inches and a thickness of 0.030 inches has been found suitable for creating observable strain cracking of the wear layer. The test procedure is also usable in evaluating compressive surface strains by simply mounting the beam so that the bending places the coating in compression, i.e., inverting. The unit then deflects up, not down. The percent surface strain at position X, ex, is calculated by the following formula: ##EQU1##
Test evaluation of the method and instrumentation was done on one half inch wide specimens with a standard coating of 3 microns of Al.sub.2 O.sub.3. Specimens 1 to 4 were coated by the procedure set forth above. A glass decal was also fused to a 0.031 inch thick 302 stainless steel strip to form Sample 5 which had a coating thickness of 10 microns.
Specific values of these coating operations are as follows:
______________________________________ Crack Observed Length Thickness % Strain @ RuptureSpecimen inch inch (Calculated)______________________________________1 1.75 0.030 0.60%2 1.75 0.030 0.71%3 2.50 0.024 0.56%4 2.25 0.030 0.33%5 2.50 0.031 >0.58%______________________________________
Two factors that contribute to the high strain value are:
1. The coating is not a single crystal as it is deposited in a layer form which builds in some form of voids. This is evidenced by repeated measurements of deposit density of 160 lbs. per cubic ft. as contrasted to 247 lbs. per cubic ft. for single crystal sapphire. The coating structure conceivably has more extensibility before rupture.
2. This test detects elongation strain-to-rupture on the as-deposited-coating. The deposited coating may not and probably is not residual-strain-free. Other sources of information and papers on deposition cite conditions creating high compression or tension deposition strains. If the coating is deposited with compressive strains, these strains must be diminished to zero by bending before actual tension strains are created. Thus if the coating were under compression from deposition, this test would measure the sum of the residual compressive strain plus the actual tension strain to failure.
Samples 1 to 4 present a range of as-deposited strain-to-rupture of 0.3 to 0.7%. The variation of strain of several samples from any one coating operation has been experimentally found to be =0.1%. This suggests that there were either variations in the coating structure or residual strains in the samples tested.
Analysis of the cracking behavior and patterns discloses characteristics of the coating. The observed cracking has been "instantaneous" which is typical of a brittle ceramic so that one can conclude that cracks will propagate once started. The cracks for these samples produced under progressive deflection were all perpendicular to the generated tensile stress, were all parallel, and were surprisingly uniformly spaced one from the other. The spacing was small averaging four tenths of a mil apart. This indicates a tightly bonded, uniform coating as no delamination occurred and the cracking progressed in repetitive fashion.
The cracks in the samples 1 and 2 were evident in the deflected beam but could not be observed (at 40.times.) when the beam was removed from the instrument and returned to the flat condition. Having cracked and being a ceramic, the cracks cannot heal to a once-again continuous surface. A machinist's dye on the surface did not make the cracks visible. This suggests that the cracks were pushed together tightly when the specimen was returned to flat and that there was no debris thrown off from the edges of the crack. It could be surmised that the coating was under residual compression strains when deposited.
EXAMPLES 1-1 TO 1-36
The following are examples of hard inorganic materials which have been deposited on various substrates:
TABLE 1______________________________________ No. ofExample Film Substrate Thickness FilmNo. Mat'l. Material (u) Layers______________________________________1-1 SiO.sub.2 SS.sup.1 foil 10.4 111-2 SiO.sub.2 SS foil 7.9 11-3 ZrO.sub.2 SS foil 2.5 11-4 Al.sub.2 O.sub.3 SS foil 0.5 11-5 Al.sub.2 O.sub.3 SS foil 1.5 21-6 ZrO.sub.2 SS foil 4.8 11-7 Al.sub.2 O.sub.3 SS foil 5.4 11-8 Al.sub.2 O.sub.3 Ferroplate 11.3 321-9 Al.sub.2 O.sub.3 Ferroplate 3.2 261-10 Al.sub.2 O.sub.3 Ferroplate 6.7 521-11 Al.sub.2 O.sub.3 Ferroplate <1.0 11-12 Al.sub.2 O.sub.3 Ceramic Tile 1.0 11-13 Al.sub.2 O.sub.3 Ceramic Tile 321-14 Al.sub.2 O.sub.3 Brass Ferroplate 1.0 11-15 Al.sub.2 O.sub.3 Brass Ferroplate 201-16 Al.sub.2 O.sub.3 Brass/Ferroplate 291-17 Al.sub.2 O.sub.3 Steel/Ferroplate 11-18 Al.sub.2 O.sub.3 Steel/Ferroplate 201-19 Al.sub. 2 O.sub.3 Steel/Ferroplate 291-20 Al.sub.2 O.sub.3 1/8" Thick 01 Steel 11-21 Al.sub.2 O.sub.3 1/8" Thick 01 Steel 291-22 Al.sub.2 O.sub.3 1/8" Thick 01 Steel 321-23 Al.sub.2 O.sub.3 TEOS.sup.2 /Ceramic Tile 0.1 11-24 Al.sub.2 O.sub.3 TEOS/Ceramic Tile 0.2 11-25 Al.sub.2 O.sub.3 TEOS/Ceramic Tile 0.5 101-26 ZrO.sub.2 on Ferrosteel 0.1 1 Al.sub.2 O.sub.31-27 Al.sub.2 O.sub.3 Ceramic Tile 1.2 31-28 Al.sub.2 O.sub.3 Brass Ferroplate 1.2 31-29 Al.sub.2 O.sub.3 Brass Ferroplate 1.0 11-30 TiN.sub.x Ferro Steel 0.3 11-31 TiN.sub.x Ferro Steel 1.0 11-32 TiN.sub.x Ferro Steel 1.9 11-33 SiO.sub.2 Ferro Steel 1.1 11-34 Al.sub.2 O.sub.3 Marble 3.0 11-35 TiN.sub.x Marble 2.4 11-36 TiN.sub.x on Marble 1/3 2 Al.sub.2 O.sub.3______________________________________ .sup.1 Stainless Steel .sup.2 Tetraethylorthosilicate
Samples approximately six inches square were tested in the Walkers Test in which six female walkers reached a total traffic count of 1200.
On matte finish, hard (manufacturer's ratings of Mohs 6.5 and 8.5) ceramic tiles, aluminum oxide coating did not scratch to a significant extent. Increased damage occurred in samples where the aluminum oxide was deposited onto ceramic substrates with Mohs hardness less than 6.5.
On hard, shiny ceramic tile, aluminum oxide performed well. On softer, unglazed tile, the coating appeared to provide protection against large scratches during the first half of the test, and at the end of the test there were fewer (but noticeable) scratches on the coated than on the uncoated samples. The aluminum oxide coating prevents the formation of haze (multiple fine scratches) on brass ferroplate. On ferroplate, application of aluminum oxide at 140.degree. C. produced a coating that performed as well as one applied at 250.degree. C. The best ferroplate samples were ones coated when other types of samples were not in the chamber.
When aluminum oxide was applied to a shiny ceramic tile that was essentially not scratched in its uncoated state (and on which scratches, if present, could be readily seen), the coating performed almost as well as the uncoated tile. The coated tile had two fairly large, almost scuff-like scratches but otherwise was essentially as good as the uncoated tile.
Under the same test conditions, the coated ferroplate samples--although exhibiting complete resistance to multiple fine scratches--had a number of large scratches on them. The ferroplate samples with the most scratches were those prepared at the same time as samples other than ferroplate. These results hint that the coating may be adversely affected by contaminants from the other samples.
On softer, unglazed tile, the coating appeared to protect the tile from large scratches during the first half of the test. At the end of the test, there were fewer but more noticeable scratches on the coated, with coating removed along the scratches.
EXAMPLES 2-1 TO 2-8
Performance of vapor-deposited aluminum oxide was evaluated using the Walker Test. Under these test conditions, the aluminum-oxide-coated ferroplate samples with the thicker coatings were the best performing flooring prototypes. The only samples to retain their gloss in all areas were those with vapor-deposited aluminum oxide coatings at least 2.5 microns thick on ferroplate. The principal damage to these samples consisted of medium and large scratches.
Samples approximately six inches square were tested in the Walkers Test in which six female walkers reached a total traffic count of 1236.
Because the samples were only six inches square, the walkers either placed a single foot on each sample or had to make a special effort to place both feet on each sample. It was observed that when they placed both feet on a sample, they usually placed their feet on diagonally opposite quadrants of the sample. This produced on most samples two areas which were much more worn than other areas. See results in Table 2.
TABLE 2__________________________________________________________________________Example Support Wear No. of Al.sub.2 O.sub.3 ThK.No. Substrate Layer Layers Total, u Comments__________________________________________________________________________2-1 Brass Al.sub.2 O.sub.3 1 0.3 Purple-blue color; many Ferroplate fine scratches and very dull sections throughout sample; Al.sub.2 O.sub.3 appeared to be removed by traffic in 2 quadrants2-2 Brass Al.sub.2 O.sub.3 1 0.5 Green to colorless; some Ferroplate fine scratches, some larger scratches, no dull areas Al.sub.2 O.sub.3 appears to be intact2-3 Brass Al.sub.2 O.sub.3 1 1.0 Pink to colorless; many Ferroplate fine scratches, Al.sub.2 O.sub.3 partly removed (uniformly)2-4 Brass Al.sub.2 O.sub.3 5 2.0 Some fine scratches, Ferroplate most damage was large- sized scratches; good gloss retention2-5 Brass Al.sub.2 O.sub.3 2 2.0 More fine scratches than Ferroplate 2-4; some large size scratch damage2-6 Brass Al.sub.2 O.sub.3 1 3.2 Almost no fine Ferroplate scratches, some large size scratches2-7 Brass Al.sub.2 O.sub.3 -- 2.5 Almost no fine Ferroplate scratches, all damage2-8 Brass Al.sub.2 O.sub.3 1 3.2 medium to large Ferroplate scratches__________________________________________________________________________
The performance of aluminum-oxide-coated ferroplate with a coating at least 2.5 microns thick was superior to commercial wear layers. The only samples to retain their gloss in all the pivot areas were those with aluminum oxide coatings at least 2.5 microns thick on ferroplate. The principal damage to these samples consisted of a number of medium and large scratches, each one of which is individually visible.
Indentations produced by spike heels on the aluminum-oxide-coated ferroplate did not cause macrocracking. Small parallel cracks were formed in the indentation but do not extend appreciably beyond the indentation.
EXAMPLE 3
In this example, use of an ion gun during Al.sub.2 O.sub.3 deposition did not significantly affect gloss retention--for these flooring structures. Use/nonuse of the ion gun during Al.sub.2 O.sub.3 depositions on ceramic decal/steel substrates generally has no significant effect on Walker Test performance.
The performance level of the Al.sub.2 O.sub.3 coated ceramic decal decorated steel structures was limited by the spalling of the ceramic decal at its interface with the steel support. Three-layer ceramic decal samples on 7-mil steel had fewer scratches than the coated single layer ceramic decal/steel samples. The triple-decal samples were more severely marred due to their greater tendency toward spalling.
Samples approximately six inches square were tested in the Walkers Test. Table 3 lists average gloss readings.
Al.sub.2 O.sub.3 wear layers were evaporated by the e-beam gun without the use of crucible liners. The chamber was baked out at 250.degree. C. for 1 to 3 hours prior to each deposition to minimize water vapor contamination. The substrate temperature was allowed to "float" starting at 30.degree.-90.degree. C. during the deposition runs. For depositing done without the ion gun an O.sub.2 atmosphere of approximately 2.3.times.10.sup.-4 Torr was maintained.
The Decal used was #A2894 with ceramic overglaze colors, obtained from Philadelphia Decal. The steel was 7 mil stainless steel, obtained from Lyon Industries.
TABLE 3__________________________________________________________________________ Single Decal Single Decal Triple Decal Triple DecalNo. of Ion Gun No Ion Gun Ion Gun No Ion GunPasses Initial Final Initial Final Initial Final Initial Final__________________________________________________________________________ 0 -- 81.3 -- 81.1 -- 96.6 -- 96.9 24 84.5 75.8 83.4 72.3 97.1 92.3 99.4 93.5 48 84.1 83.8 81.6 78.6 96.4 96.0 96.4 97.8102 79.0 77.2 82.3 82.7 96.0 97.9 94.7 95.1204 85.2 83.4 83.1 83.2 97.9 97.2 95.9 95.4402 75.1 76.8 75.9 73.9 94.5 88.4 95.8 95.0804 80.5 79.9 80.0 78.8 95.8 98.7 96.4 91.31200 80.5 81.0 81.4 76.6 98.2 88.3 100.0 91.6__________________________________________________________________________
EXAMPLES 4-1 TO 4-23
Evaluations were made of (a) alumina on a stiff but flexible substrate, (b) coatings prepared with and without the ion gun, and (c) layered coatings.
Alumina (2-4 microns) on a flexible but stiff substrate (3-, 5-, or 7-mil tempered steel) did not crack in the Walkers Test when (1) the resulting laminate was supported by a deformable rubber (Shore hardness 70) and (2) even when high heels were included in the Walkers Test. The laminate resisted fine scratches, in a manner similar to ferroplate tested earlier, but the severity of individually visible scratches was accentuated by failure of adhesion. The failure was not, however, between the substrate and coating but rather between the substrate and a purplish layer that was formed on the substrate.
The performance in the Walkers Test of alumina on ferroplate was greatly improved by use of the ion gun during deposition.
The standard, single-layer, alumina coating retained its appearance better than any of the layered coatings. The 18-layer chromium/alumina coating was a brilliant magenta.
In Table 4 are listed the substrates and comments on the appearance of the samples after trafficking.
TABLE 4__________________________________________________________________________ Total ThicknessExample Support Film No. of (SEM,No. Substrate Layer Material Layers microns) Comments__________________________________________________________________________Control 5-mil Shim Silicone Uncoated Matted. A number4-1 Rubber of individual scratches. A few heel dents.Control 7-mil Shim Silicone Uncoated Matted. A number4-2 Rubber of individual scratcnes. No heel dents.Control 5-mil Shim Tile Uncoated Similar to above4-3 5-mil control.Control 7-mil Shim Tile Uncoated Similar to above4-4 7-mil control.4-1 3-mil Shim Silicone Al.sub.2 O.sub.3 1 4.0 Two-piece sample. Stock Rubber No matting. A number of indivi- dual scratches. Some delamination along center seam. Scratches accentu- ated by adhesive failure. One heel penetration.4-2 5-mil Shim Silicone Al.sub.2 O.sub.3 1 4.0 No delamination. Stock Rubber No matting. Much less scratching than Example 4-1. Only a few barely discernible heel dents. Scratches accentuated by adhesive failure.4-3 7-mil Shim Silicone Al.sub.2 O.sub.3 1 4.0 No delamination. Stock Rubber No matting. Fewer scratches than Example 4-2. No discernible heel dents.4-4 Steel Tile Al.sub.2 O.sub.3 1 4.0 No matting. A Ferro number of heel dents. Number of scratches less than Example 4-2 but more than Example 4-1.4-5 3-mil Shim Silicone Al.sub.2 O.sub.3 1 4.1 Two-piece sample. Stock Rubber No matting. No delamination. Slightly fewer scratches than Example 4-2. Scratches accentu- ated by adhesive failure. A number of heel dents.4-6 5-mil Shim Silicone Al.sub.2 O.sub.3 1 4.1 Similar to Example Stock Rubber 4-2.4-7 7-mil Shim Silicone Al.sub.2 O.sub.3 1 4.1 No matting, no de- Stock Rubber lamination. Many scratches which are accentuated by adhesive failure.4-8 Steel Tile Al.sub.2 O.sub.3 1 4.1 Similar to Example Ferro 4-4.4-9 3-mil Shim Tile Al.sub.2 O.sub.3 1 2.1 No matting. Stock Slight delamina- tion at multiple scratches. Signi- ficantly more scratches than Example 4-5. Scratches accentu- ated by adhesive failure.4-10 5-mil Shim Tile Al.sub.2 O.sub.3 1 2.1 Similar to Example Stock 4-6, but slightly fewer scratches.4-11 7-mil Shim Tile Al.sub.2 O.sub.3 1 2.1 No matting, no de- Stock lamination. Few- est scratches of any shim stock sample. Scratches accentuated by adhesive failure.4-12 Steel Tile Al.sub.2 O.sub.3 1 2.1 Similar to Example Ferro 4-4.4-13 3-mil Shim Tile Al.sub.2 O.sub.3 1 3.1 No matting, some Stock delamination. Second most scratches.4-14 5-mil Shim Tile Al.sub.2 O.sub.3 1 3.1 Most scratches of Stock any shim stock sample4-15 7-mil Shim Tile Al.sub.2 O.sub.3 1 3.1 More scratches Stock than Example 4-11.4-16 Steel Tile Al.sub.2 O.sub.3 1 3.1 Similar to Ferro Example 4-4.4-17 Steel Tile Al.sub.2 O.sub.3 1 3.0 Similar to Ferro Example 4-4.4-18 Steel Tile Al.sub.2 O.sub.3 1 3.0 Similar to Ferro Example 4-4.4-19 Steel Tile Al.sub.2 O.sub.3 1 3.0 Large areas delam- Ferro inated (before test). Delamina- tion along scratches.4-20 Steel Tile SiO/Al.sub.2 O.sub.3 5/5 2.0 Some matting, many Ferro scratches.4-21 Steel Tile SiO/Al.sub.2 O.sub.3 5/5 2.0 No matting but Ferro many deep scratches.4-22 Steel Tile Cr/Al.sub.2 O.sub.3 9/9 5 Magenta. Worn Ferro thru on a pivot point. Delamina- tion around pivot point.4-23 Steel Tile Al/Al.sub.2 O.sub.3 3/3 1.5 Matted areas. Ferro Many scratches in- cluding very fine scratches.__________________________________________________________________________
The Al.sub.2 O.sub.3 metallic laminate was sufficiently flexible that it could be bent around a 2-inch mandrel without the Al.sub.2 O.sub.3 cracking, even when the Al.sub.2 O.sub.3 was on the convex side. The optimum thickness of the substrate layer appears to be 5 to 7 mils; the 3-mil substrate could be pierced by high heels.
The alumina prevented the formation of fine scratches on the shim steel. The severity of individually visible scratches was accentuated on the coated samples by adhesive failure.
The use of the ion gun during deposition improved the performance of alumina on ferroplate. The sample prepared without the ion gun had many more scratches, significant adhesion failure along the scratches, and an area about 1.times.21/2 inches that delaminated before the test.
The 18-layer chromium/alumina coating was a brilliant magenta. The coating was 5 microns thick, so this situation was different than one in which thin coatings exhibit interference patterns.
The standard coating retained its appearance better than any of the layered coatings (Examples 4-20 to 4-23).
EXAMPLES 5-1 TO 5-15
Outgassing during the deposition process was demonstrated to adversely effect the scratch performance Al.sub.2 O.sub.3 thin films. The outgassing species was tentatively identified as water. This problem may be eliminated by addition of a high temperature bake-out cycle to the deposition procedure. Outgassing was shown to affect the scratch performance, and may greatly reduce scratch resistance.
For Al.sub.2 O.sub.3 deposition, a 3-hour plateau style bakeout at 250.degree. C. suppressed the outgassing sufficiently to prepare films which had reproducible scratch resistance. In the absence of a bakeout, severe outgassing occurred which adversely affected scratch resistance in the Al.sub.2 O.sub.3 films produced. The outgassing was probably due to thermal desorption of water from Al.sub.2 O.sub.3 on the walls of the deposition chamber. Direct identification of the outgassing material must await installation of a pressure adapter for the Residual Gas Analyzer. If the bakeout is not feasible due to thermal limitations of the substrate material, then the chamber should be freshly cleaned and lined with new aluminum foil immediately prior to deposition on that substrate.
When the Al.sub.2 O.sub.3 coated glass substrates from deposition SERIES A (See Table 1) were evaluated in the diamond stylus scratch test, two major observations were noted: both the Load to Incipient Damage (LID), and the type of damage at the LID changed from the first member of the series to the last. The changes were not monotonic from the beginning of the series to the end. For example, the first member of the series (Specimen 10) gave a LID of 50 g due to the appearance of birefringeance along the scratch track made by the diamond in the surface of the alumina. Scratching at loads of up to 95 g showed an increase in the birefringeance, but at no point was any film delamination observed. In contrast, for the second member of the series, birefringeance occurred at an LID of 40 g; at 50 g film delamination began and cracks appeared normal to the scratch direction; and at 70 grams chipping was observed. For the third member of the series, delamination and cracking were both observed at an LID of only 25 g, and film decohesion occurred at 40 g. The remaining members of the series were also characterized by low LID's due to delamination, cracking and film decohesion. These observations exemplify a progressive decrease in adhesion between the vapor deposited Al.sub.2 O.sub.3 and the glass substrates.
TABLE 5______________________________________Film Data, Physical and Mechanical Properties______________________________________SERIES A:Example 5-1 5-2 5-3 5-4 5-5 5-6 5-7 5-8NumberLID.sup.a (grams) 50 40 25 30 15 20 15 20Thickness.sup.c 3.17 3.74 3.55 4.03 3.89 4.03 4.22 3.70(.mu.)Wt. Dep. 15.0 17.3 16.1 1.85 1.68 1.69 1.69 1.64(mg)SERIES B:Example Number 5-9 5-10 5-11LID.sup.a (grams) 45 40 45Thickness.sup.c (.mu.) 3.31 2.98 3.31SERIES C:Example Number 5-12 5-13 5-14 5-15LID.sup.a (grams) 50 45 45 45Thickness.sup.c (.mu.) 4.08 3.65 3.70 3.50______________________________________ .sup.a Load to Incipient Damage: Damage in excess of simple indentation .sup.b Calculated, based on SEM thickness and a coated area of 16.75 cm.sup.2 .sup.c Obtained by Scanning Electron Microscopy
SERIES A
Eight consecutive deposition runs were performed. In each case, substrates in addition to glass substrates were present in the chamber. These substrates included Ferrosteel, 5 mil spring steel, chromed spring steel, thick "01" steel plate (both chromed and untreated), stainless steel, and several engineering plastics. In all but two of the runs in this series, the samples were loaded into the deposition chamber in late afternoon of the working day before the run. For the Examples 5-5 and 5-7, however, the samples were loaded into the deposition chamber in the morning and the system was allowed to pump down over the lunch hour.
SERIES B
Three consecutive deposition runs were performed. These runs contained only glass substrates. The procedure was the same as that for SERIES A except that Example 5-11 was subjected to a three hour bakeout cycle at 250.degree. C. while pumping overnight.
SERIES C
Four consecutive deposition runs were performed. These runs contained additional substrates capable of withstanding a 250.degree. C. heat treatment. For each of these runs the procedure included an overnight bakeout at 250.degree. C.
Diamond stylus scratch test results are reported here as Load to Incipient Damage (LID) to the nearest five grams of stylus weight loading. Because the mechanism of scratching hard inorganic materials does not include any macroscopically observable "recovery" mechanism, Load to Incipient Damage is defined as that weight loading, in the LOM equipped with a 45.times. objective, where damage other than a simple indentation is observed. For example: the LID may be due to the observation of birefringeance at the edge of the scratch track, by delamination of the film, chipping, or the development of cracks.
Density measurements were obtained by dividing the weight gain of a Ferrosteel slide by the area exposed for deposition (16.75 cm.sup.2) and the film thickness as determined by SEM. Control experiments showed that there was no detectable weight loss due to sputtering even after 20 minutes exposure to a 600 mA/600 V Ar+ ion plasma. In addition, a Ferrosteel slide subjected to the entire deposition cycle but shielded from deposition experienced no detectable weight change.
A clue into the cause of these adhesive differences was offered by a qualitative comparison of Ion Gun voltage during the first few moments of several of the SERIES A deposition runs. A high bombardment voltage was attained immediately at the start of the deposition run and the voltage was sustained throughout the run. However, voltage dropped at the onset of deposition, and progressively longer times were required to reach and sustain an ion voltage of 600 volts. Two important facts are associated with this observation. First, the ion gun voltage is inversely proportional to the chamber pressure. Thus a voltage drop is accompanied by a pressure surge. Second, Al.sub.2 O.sub.3 films prepared using a high voltage ion assist outperform those prepared with no ion assist. Therefore, a pressure surge accompanied by a voltage drop will adversely effect the wear performance of such a film.
The progressive nature of the deterioration in LID performance suggested an impurity buildup as a function of chamber use. Thus it was proposed that excess alumina deposited on the chamber walls gettered water vapor from the laboratory atmosphere whenever the chamber was opened to install or remove substrates. Aluminum oxide is a well known desiccant which is activated by heat treatment in a vacuum. Radiation from the e-beam evaporation source probably "activated" alumina which had accumulated on the chamber walls during previous runs and caused the observed pressure surges. Direct verification of this hypothesis using the Residual Gas Analyzer (RGA) was not possible because of its pressure limitation.
The first indirect confirmation that water vapor was being desorbed was obtained using the RGA under predeposition conditions. The RGA, upon evacuation of the chamber to a pressure of 10.sup.-6 Torr showed a constant (uncalibrated) water vapor pressure of 5.times.10.sup.-5 Torr. When the quartz heaters in the chamber were energized, however, an immediate pressure surge due to an increase in water vapor pressure was observed. Unfortunately, the cutoff pressure for the RGA is 10.sup.-4 Torr, which is the vapor pressure in the chamber during most deposition runs. Therefore, the RGA cannot be used during the runs to directly confirm the water vapor hypothesis.
A second indirect confirmation of the role of water vapor during the deposition process was obtained by examination of the scratch test results obtained from deposition SERIES B (see Table 5). The first two depositions in this series were run on consecutive days, under the same conditions as the first two members of SERIES A. For the first two deposition runs in both SERIES A and SERIES B, trends showing a decrease in scratch LID, and an increase in voltage stabilization time was observed (the magnitude of the pressure surge was mitigated by the chamber operator decreasing the flow rate through the ion gun). Addition of a bakeout cycle to the deposition procedure for the third deposition run in SERIES B resulted in recovery of the scratch behavior observed in the first members of both SERIES A and B, and decreased the time required to obtain a stable ion gun voltage.
SERIES C was run in order to test the reproducibility of scratch tests obtained from runs which included the bakeout cycle. In contrast to SERIES A, no significant change in scratch performance from the beginning of SERIES C to the end was observed.
The early moments of the deposition runs in SERIES C were not accompanied by the voltage drops and pressure surges that were observed in SERIES A. Also no change was shown in the type of scratch damage observed at the LID.
EXAMPLES 6-1 TO 6-14
Increasing the thickness of the decorative layer improved the performance of the glass and ceramic decals, both coated and uncoated except that of the 20-micron thick glass decorative layers. Coating the decorative layer with aluminum oxide improved the overall appearance retention in all cases. The failure mode for the glass and ceramic decals appears to be different. Diamond stylus scratch tests show that the glass decorative layer crumbles under relatively high stylus load where the ceramic decorative layer chips.
In previous Walkers Tests, the decorative layer which consisted of 5-micron-thick glass decals, showed large individually discernible scratches that broke through to the metal substrate. Since the decorative layer also supports the aluminum oxide layer a thicker glass layer should provide better support. Samples made by layering glass decals were run in the Walkers Test to test this idea.
The glass-ink decal has a nano-hardness of 6 Gpa. The best aluminum oxide has a nano-hardness of 10 Gpa. There exist ceramic inks which form harder decorative layers than the glass inks. These ceramic inks have a nano-hardness value of 11 Gpa. Decals made from these ceramic inks not only should provide better support for the aluminum oxide layer but conceivably could act as a wear layer itself. Single and multiple layer samples were prepared to evaluate the effect of thickness on performance.
Samples approximately six inches square were tested in the Walkers Test. The samples were supported by a vinyl base tile to which they were attached by adhesive transfer tape. Six walkers reached a total traffic count of 1200.
Before and after trafficking, sixty-degree gloss measurements were made with the Mallinckrodt Glossmeter. A measurement was made at the center and at the center of each of four quadrants of the sample for a total of five measurements.
Sample descriptions and gloss values are listed in Table 6. The glass decals were 5 microns thick. The ceramic decals were 10 microns thick.
TABLE 6______________________________________Sample Gloss ValuesNo. Sample Descriptions Initial Final______________________________________6-1 1 layer glass decal/7 mil 302 steel 70 606-2 Aluminum oxide coated 1 layer glass 53 54 decal/7 mil 3026-3 2 layer glass decal/7 mil 302 steel 96 706-4 Aluminum oxide coated 2 layer glass 63 59 decal/7 mil 3026-5 3 layer glass decal/7 mil 302 steel 110 866-6 Aluminum oxide coated 3 layer glass 86 85 decal/7 mil 3026-7 4 layer glass decal/7 mil 302 steel 83 376-8 Aluminum oxide coated 4 layer glass 73 58 decal/7 mil 3026-9 1 layer ceramic decal/7 mil 302 steel 78 67 6-10 Aluminum oxide coated 1 layer ceramic 78 72 decal/7 mil 302 6-11 2 layer ceramic decal/7 mil 302 steel 87 84 6-12 Aluminum oxide coated 2 layer ceramic 90 90 decal/7 mil 302 6-13 3 layer ceramic decal/7 mil 302 steel 89 80 6-14 Aluminum oxide coated 3 layer ceramic 92 91 decal/7 mil 302______________________________________
Increasing the thickness of the decorative layer improved the performance of the glass and ceramic decals, both coated and uncoated. The sample with the best appearance and gloss retention was the aluminum oxide-coated triple-layer (30 micron) ceramic-decal sample. In general, the multilayer ceramic decals resisted large scratches better than the multilayer glass decals.
Coating the decorative layer with aluminum oxide improved the overall appearance and gloss retention in all cases except that of the 5- and 10-micron thick glass decorative layers. The aluminum oxide coating improved the gloss retention of both systems, with the coated ceramic decal having the best gloss retention. On the ceramic decals, the aluminum oxide reduced the number of large scratches. On the glass decals, the aluminum oxide reduced the number of small scratches. With the ceramic decals, some of the scratches appeared confined to the aluminum oxide coating.
The ceramic decals appeared to adhere less well to the steel than did the glass decals. At 10 microns, the ceramic decals resisted fine scratches better than the glass decals but had more scratches to the metal. At 20 microns, the ceramic decals resisted both fine and large scratches better than the glass decals but still had more scratches to the metal. The chipping around the area of the scratches in the ceramic decals, seems to indicate an adhesion failure, possibly due to differences in the coefficient of thermal expansion.
The failure mode for the glass and ceramic decals appeared to be different. Diamond stylus scratch tests on the same samples that made up this Walkers Test showed that at relatively high loads (60-95 grams), the glass decals tended to crumble where the ceramic decals did not. The crumbling decal left granules of material on either side of the scratch. In the multi-layer ceramic decal samples any failure noted could be described as a chipping failure. The scratch from the stylus looked similar to aluminum oxide scratches but had intermittent areas where the ceramic ink chips away from the rest of the coating. It appeared that the ceramic ink in the decorative layer had a greater inherent strength than the glass ink. However, when stressed to the point of failure, the ceramic ink exhibited a brittle failure where the glass crumbled.
EXAMPLES 7-1 TO 7-8
Addition of a ceramic primer to the composite structure eliminated the spalling of the decorative layer seen in previous walker testing. Damage was limited to large, individually visible scratches and can be grouped into three types: (a) damage to the Al.sub.2 O.sub.3 layer only; (b) damage to the decorative layer; and (c) damage to the metal substrate. There was no deglossing due to fine scratches. The two ceramic primers performed equally well.
Samples were tested in the Walkers Test. Table 7 lists the sample data and the gloss values as measured. Two ceramic/metal composite categories were tested. They were: (1) Al.sub.2 O.sub.3 -coated ceramic decal on H34001 primer on 7 mil 302 steel; and (2) Al.sub.2 O.sub.3 -coated ceramic decal on J-M600001 primer on 7 mil 302 steel.
TABLE 7______________________________________ Al.sub.2 O.sub.3 Sample Thk..sup.3 Walker 60.degree. GlossDescription No. (micron) Cycles Initial Final______________________________________Al.sub.2 O.sub.3 /Ceramic 7-1 4.8.sup. 400 89.4 81.0Decal/ 7-2 4.8.sup. 800 88.8 79.3H34001 Primer.sup.1 7-3 4.8.sup. 1200 86.1 84.4 7-4 3.8.sup.3 1200 85.6 80.8Al.sub.2 O.sub.3 /Ceramic 7-5 4.3.sup.4 400 98.2 91.9Decal/ 7-6 3.8.sup.3 800 94.2 90.1J-M600001 Primer.sup.2 7-7 4.3.sup.4 1200 97.5 90.0 7-8 4.3.sup.4 1200 95.6 89.7______________________________________ .sup.1 Manufactured by Heraeus, Inc. .sup.2 Manufactured by Johnson Matthey .sup.3 Light optical microscope thickness determination. .sup.4 Average of four SEM measurements.
EXAMPLES 8-1 TO 8-19
Uncoated and Al.sub.2 O.sub.3 -coated, 30 micron thick decorative layer samples had the very good appearance retention. Al.sub.2 O.sub.3 -coated white H34002 primer (30 micron) samples were marginally better than the 30-micron, white H34002 primer samples. Al.sub.2 O.sub.3 -coated 10-micron ceramic decal on 20 micron of white H34002 primer contained no scratches to the metal substrate.
Six-inch square samples were tested in the Walkers Test. Table 13 shows the sample descriptions and gives the raw data.
Three categories of wear layers were prepared.
1. 30 micron-H34002 primer on 7-mil 302-steel.
2. Al.sub.2 O.sub.3 -coated, 30 micron-H34002 primer on 7-mil 302-steel.
3. Al.sub.2 O.sub.3 -coated, 10 micron-ceramic decal on 20 micron-H34002 primer on 7-mil 302-steel.
All samples tested had fewer scratches to the metal. As previously seen, the presence of the primer coat had eliminated spalling of the ceramic layer from the damage area. The damage of the Al.sub.2 O.sub.3 -coated decal samples was limited to the aluminum oxide layer and the decal only.
TABLE 8______________________________________ Al.sub.2 O.sub.3 Example Thk. Walker 60.degree. GlossDescription No. (Micron) Cycles Initial Final______________________________________30 Micron H34002 8-1 -- 200 89.9 95.5Primer 8-2 -- 400 90.8 93.8 8-3 -- 800 94.7 91.9 8-4 -- 1200 94.1 92.3 8-5 -- 1200 92.2 91.6 8-6 -- 1200 94.4 93.7 8-7 -- 1200 93.3 90.8Al.sub.2 O.sub.3/ 30 Micron 8-8 5.1 200 103.6 105.7H34002 Primer 8-9 5.1 400 102.0 108.1 8-10 5.1 800 100.1 103.3 8-11 5.1 1200 99.1 102.4 8-12 4.8 1200 103.3 106.9 8-13 4.8 1200 102.6 105.6 8-14 4.8 1200 101.2 105.5 8-15 4.8 1200 101.5 102.7Al.sub.2 O.sub.3 /Ceramic 8-16 4.6 200 87.6 96.2Decal/20 Micron 8-17 4.6 400 85.8 94.0H34002 Primer 8-18 4.6 800 90.9 92.7 8-19 4.6 1200 89.6 94.5______________________________________
EXAMPLES 9-1 TO 9-41
Structures were fabricated using Ion Assisted Physical Vapor Deposition (IAPVD) to deposit Al.sub.2 O.sub.3 or SiO.sub.x "ceramic" wear layers onto undecorated plastic substrates. These structures had the same average gloss retention profile as ceramic tile. Scratch and Walkers Tests demonstrated the synergistic relationship between the coating and substrate properties in these composites. Nanoindentation showed relationships between hardness, chemistry and the processes used to prepare the wear layers.
Flooring structures with 5-8 microns of Al.sub.2 O.sub.3 or SiO.sub.x supported by an undercoated, reinforced polyester substrate have gloss retention superior to currently marketed wear layer materials. However, individually visible scratches were apparent in these structures. Although these scratches did not affect gloss retention, the post-trafficking appearance of the coated structures would be improved if all scratches were prevented. The key to that prevention lies in obtaining a good match between the mechanical properties of the plastic substrate and the hard wear layer. In these examples, the aluminum oxide coating provided only limited improvement to the performance of any organic-containing substrate where adhesion failure (aluminum oxide removal) was a major factor.
Diamond stylus scratch testing and nonoindentation were the two main characterization tests to monitor mechanical property response for the title structures. The Al.sub.2 O.sub.3 and SiO.sub.x supported by polyester sheet molding compound (PSMC) show the highest stylus LSP (Load to Substrate Penetration), which is consistent with the superior gloss performance of such structures. Nonoindentation results show that Al.sub.2 O.sub.3 is the hardest wear layer material tested in an actual flooring prototype in which a plastic support was employed. Si.sub.3 N.sub.4 is suggested as an alternative material.
Ion Assisted Physical Vapor Deposition (IAPVD) was used to produce films for wear layers on plastic substrates. Metal or metal oxide vapor was evaporated by heating with an electron beam until it vaporized. When the vapor deposited on a substrate, simultaneous bombardment by an ion beam helped to form a dense, defect free film. Materials deposited onto plastic substrates include Al.sub.2 O.sub.3, SiO.sub.x, AL.sub.2 O.sub.3 -SiO.sub.x, and SnO.sub.x -SiO.sub.x. Test structures prepared by this technique are listed in Tables 9A, 9B and 9C.
TABLE 9A______________________________________IAPVD Al.sub.2 O.sub.3 Wear layers onNon-decorated Plastic SubstratesSample Wear Thickness LDP.sup.1No. Layer (microns) Support Substrate (grams)______________________________________9-1 Al.sub.2 O.sub.3 1.5 PES.sup.2 2x tape/ 15 glass9-2 Al.sub.2 O.sub.3 4.9 None PSMC.sup.3 --9-3 Al.sub.2 O.sub.3 6.0 None PSMC >359-4 Al.sub.2 O.sub.3 -- PVC.sup.4 WT.sup.5 --9-5 Al.sub.2 O.sub.3 0.480 PVC WT 109-6 Al.sub.2 O.sub.3 0.528 PVC WT --9-7 Al.sub.2 O.sub.3 /SiO.sub.x 0.432 PVC WT --9-8 Al.sub.2 O.sub.3 /SiO.sub.x 0.336 PVC WT --9-9 Al.sub.2 O.sub.3 4.03 None GFRP.sup.6 .about.359-10 Al.sub.2 O.sub.3 3.89 None FFP.sup.7 .about.309-11 Al.sub.2 O.sub.3 4.03 None PSMC >35, <509-12 Al.sub.2 O.sub.3 1.78 None PSMC .about.409-13 Al.sub.2 O.sub.3 1.78 None PEEK.sup.8 309-14 Al.sub.2 O.sub.3 4.5 None Formica 239-15 Al.sub.2 O.sub.3 2.0 None Formica --9-16 Al.sub.2 O.sub.3 2.0 None Formica --______________________________________ .sup.1 Load to Substrate Penetration .sup.2 Polyethersulfone .sup.3 Polyester Sheet Molding Compound .sup.4 Polyvinylchloride .sup.5 Nonasbestos vinyl white tile base .sup.6 Glass Fiber Reinforced Polyester .sup.7 Fiber Filled Phenolic .sup.8 Polyetheretherketone
TABLE 9B______________________________________IAPVD SiO.sub.x Wear Layers onNondecorated Plastic SubstratesSample Thickness LSP.sup.1No. (microns) Support Substrate (grams)______________________________________9-17 2.3 Kapton.sup.2 2x tape/Glass >159-18 1.2 None PMMA 159-19 2.3 None PMMA >159-20 1.1 None PMMA >159-21 1.8 None PMMA 109-22 1.2 Kapton 2x tape/Glass 259-23 1.2 PES.sup.4 2x tape/Glass 159-24 1.2 PEEK.sup.5 2x tape/Glass 159-25 1.2 Cronar.sup.6 2x tape/Glass 259-26 1.2 None Teflon7 <59-27 0.4 PVC.sup.8 WT.sup.9 5-109-28 1.4 PVC WT 109-29 2.3 PVC WT 159-30 3.8 PVC WT 15 g-189-31 3.7 PVC WT 15 g-189-32 2.8 PVC PSMC.sup.10 239-33 5.3 None PSMC .about.28______________________________________ .sup.1 Load to Substrate Penetration .sup.2 DuPont Polyimide .sup.3 Polymethylmethacrylate .sup.4 Polyethersulfone .sup.5 Polyetheretherketone .sup.6 DuPont Photographic Polyester .sup.7 DuPont Polytetrafluroethylene .sup.8 Polyvinylchloride .sup.9 Nonasbestos Vinyl White Tile Base .sup.10 Polyester Sheet Molding Compound
TABLE 9C______________________________________Miscellaneous IAPVD Coatings on Plastic SubstratesSample ThicknessNo. (microns) Structure______________________________________9-34 4.37 Al.sub.2 O.sub.3 /PVC/CWT9-35 4.61 Al.sub.2 O.sub.3 /PVC/CWT9-36 6.00 SiO.sub.x /PVC/CWT9-37 <10 AlO.sub.x /PVC/CWT9-38 .about.3 Al.sub.2 O.sub.3 /PVC/CWT9-39 0.48 SiO.sub.x /Hologram9-40 -- SnO.sub.x /Rigid PVC9-41 -- SnO.sub.x /SiO.sub.x /PVC______________________________________
For flooring structures with Al.sub.2 O.sub.3 or SiO.sub.x thin hard coatings on selected plastic substrates: (1) an increase in wear layer hardness resulted in an increase in gloss retention and overall appearance retention; and (2) an increase in substrate hardness resulted in an increase in gloss retention and overall appearance retention.
Gloss retention for flooring structures with thin hard wear layers occurs because the hard coating resists penetration and subsequent removal. The hard coating serves as a barrier that protects the less scratch resistant plastic material. Therefore, the scratch test results reported here use an alternative term, "Load to Substrate Penetration" (LSP) rather than "Load to Incipient Damage" (LID). The LSP refers to the weight loading at which the diamond stylus penetrates the hard protective layer and enters the substrate below. For example, irreversible damage is caused by a stylus load of 15 grams for a Al.sub.2 O.sub.3 coating on PSMC, and this low LID implies that poor gloss retention will be observed. However, the opposite is true. Gloss retention by thin, hard coatings depends upon both coating and substrate properties, and the LSP reflects that synergistic relationship better than does the LID.
Tables 9A, 9B and 9C contain the LSPs for most of the coatings that have been prepared.
Results from the scratch tests are clearly in agreement with the Walkers Test data regarding the superiority of Al.sub.2 O.sub.3 as a wear layer. The LSP for Al.sub.2 O.sub.3 on PSMC is higher than that of SiO.sub.x.
The results for SiO.sub.x on both PSMC and PVC/CWT show that scratch resistance improves with the thickness of the hardcoat. This is consistent with the observation of improved gloss and appearance retention for thick vs thin coatings on soft plastic supports.
The high LSPs for both SiO.sub.x and Al.sub.2 O.sub.3 on PSMC predict, in agreement with Walkers Test data, that the PSMC should be the best support.
EXAMPLES 10-1 TO 10-4
This Walkers Test demonstrated that good gloss retention is obtained from a flooring structure consisting of a Al.sub.2 O.sub.3 wear layer supported by a rigid plastic, like polyester sheet molding compound (PSMC). The performance rating of the Al.sub.2 O.sub.3 coated metal substrates was complicated by the fact that water vapor contamination was present during some of the runs. The TiN.sub.x, blue-black in color, had gloss performance similar to Al.sub.2 O.sub.3.
A structure consisting of 4-microns of Al.sub.2 O.sub.3 on a thick plate of polyester sheet molding compound (PSMC) remained essentially free of small scratches, showing no hazing and retaining 86% of its measured gloss after 1200 walker cycles. It had, however, a number of individually visible scratches.
Al.sub.2 O.sub.3 wear layers on (a) fabric filled phenolic (FFP), (b) black PSMC, and (c) glass fiber-reinforced polyester retained a lesser but still substantial portion of their original gloss. The uncoated controls, in contrast, were completely deglossed and covered with fine scratches that resulted in a final hazy appearance.
The samples were tested in the Walkers Test. Gloss measurements were obtained for the samples and listed in Table 10.
TABLE 10______________________________________Gloss values for 4 micron thick Al.sub.2 O.sub.3 coated anduncoated rigid polymer substrates before and afterWalkers Test traffickingSampleNo. Description Initial Final Change % Loss______________________________________10-1 Al.sub.2 O.sub.3 /White PSMC.sup.1 46.5 39.7 -6.8 -14.6C10-1 White PSMC 57.5 2.5 -55.0 -95.710-2 Al.sub.2 O.sub.3 /Black PSMC 46.8 37.9 -8.6 -18.4C10-2 Black PSMC 64.2 2.6 -61.6 -96.010-3 Al.sub.2 O.sub.3 /GFP.sup.2 25.1 16.7 -8.4 -33.5C10-3 GFP 20.2 11.6 -8.6 -42.610-4 Al.sub.2 O.sub.3 /FFP.sup.3 69.1 45.6 -23.5 -34.0C10-4 FFP 52.1 9.7 -42.4 -81.4______________________________________ .sup.1 1/4" Thick Polyester Sheet Molding Compound .sup.2 1/4" Thick Glass Filled Polyester .sup.3 1/4" Thick Fabric Filled Phenolic
EXAMPLE 11
Al.sub.2 O.sub.3 and SiO.sub.x wear layers on PSMC showed no significant gloss reduction after 1200 walker cycles, however there were some visible scratches. Test flooring structures using commercial wear layer materials all were completely deglossed and visibly scratched to a matte finish after the same test period. Also between those extremes was a second new flooring structure with a 5-8.mu. wear layer of SiO.sub.x on a relatively non-rigid substrate (non-decorated rigid PVC film laminated to non-asbestos vinyl white tile base). Al.sub.2 O.sub.3 clearly out-performed SiO.sub.x for structures having a common substrate, and comparable wear layer thickness. The observations from this and other Walkers Tests clearly demonstrate that important aspects in the performance of hard inorganic wear layers on plastic substrates include wear layer thickness, wear layer hardness, and support rigidity.
Superior gloss retention and scratch resistance have been observed with new structures consisting of a reinforced plastic support and an inorganic wear layer. The support material was polyester sheet molding compound, and the wear layer consisted of a five to eight micron "thick" film of either Al.sub.2 O.sub.3 or SiO.sub.x, prepared by IAPVD.
The SiO.sub.x and Al.sub.2 O.sub.3 coatings on PSMC were above the critical thickness required for wear resistance applications. Above that thickness limit, further increases in coating thickness have no apparent effect on either gloss retention or scratch resistance. Scratch tests suggest that the crossover point is in the one to three micron range.
Hardness of the coating material is a factor in determining gloss retention and scratch resistance. For example, despite being 2 microns thinner than its SiO.sub.x coated analog, the 5-6 micron "thick" Al.sub.2 O.sub.3 coated PSMC samples started and finished the Walkers Test at higher gloss, and with fewer visible scratches. This is consistent with the previous observation that IAPVD Al.sub.2 O.sub.3 is a harder material than IAPVD SiO.sub.x.
Samples approximately six inches square were tested in the Walkers Test using the serpentine sample arrangement. Tables 11A and 11B list average gloss readings from the Walkers Test.
PSMC was obtained as 12".times.12".times.0.125" panels of L15402 Premi-Glass 1100-05, Cameo Colored, from Premix, Incorporated.
Al.sub.2 O.sub.3 and SiO.sub.x wear layers were evaporated from the e-beam gun without the use of crucible liners, and the chamber was cleaned and refoiled immediately prior to each deposition to avoid water vapor contamination.
TABLE 11A______________________________________Gloss Values for Polyester Sheet Molding Compound(PSMC) and Ceramic Wear Layers on PSMC afterWalkers Test Trafficking 8 micron Thick 5-6 micron ThickControl PSMC SiO.sub.x on PSMC Al.sub.2 O.sub.3 on PSMCPasses Initial Final Initial Final Initial Final______________________________________ 0 60.7 -- 47.9 -- 54.1 -- 24 62.0 51.0 46.6 47.9 53.3 53.7 48 61.5 34.1 48.0 49.1 60.3 60.8102 66.3 15.7 38.5 42.2 46.6 46.9204 58.7 7.8 48.6 50.8 55.4 55.9402 50.5 3.1 53.2 52.6 61.0 61.7804 65.9 3.1 55.2 50.8 43.2 44.81200 60.0 2.8 53.1 49.0 58.7 59.4______________________________________
TABLE 11B______________________________________Gloss values for SiO.sub.x on PVC, and Polyethersulfoneafter Walkers Test Trafficking 4-6 micron Thick 3 mil Thick PES on SiO.sub.x on PVC Citation Tile BasePasses Initial Final Initial Final______________________________________ 0 52.3 -- 98.7 -- 24 52.5 52.8 98.8 22.9 48 59.4 60.3 102.0 20.5102 56.8 42.2 100.1 05.6204 56.8 42.2 109.0 04.5402 53.5 34.9 91.2 01.4804 48.1 21.9 95.5 00.31200 46.1 13.2 94.6 00.4______________________________________
EXAMPLES 12-1 TO 12-28
Samples approximately six inches square were tested in the Walkers Test. Initial and final gloss readings were made using a Mallinckrodt 60.degree. C. Pocket Gloss Meter and B. A. Newman's template. Table 12A lists average gloss readings for the samples. Descriptions of the samples are given in Table 12B.
Alumina wear layers were deposited onto the samples by evaporating Al.sub.2 O.sub.3 from the E-beam gun without the use of crucible liners. The procedure included a bakeout at 250.degree. C. for 1 hour prior to each deposition to minimize water vapor contamination. For most runs, the substrate temperature was allowed to "float" starting at 30.degree.-40.degree. C. during the deposition runs. For depositions done without the ion gun, an O.sub.2 atmosphere of .sup.-2.3.times.10.sup.-4 Torr was maintained. Plasma cleaning, when employed, was for five minutes at a pressure of about 3 -6.times.10.sup.-4 Torr.
The substrates consisted of about 30 mils of Heraeus H34000 series White Overglaze Frits on a 7 mil stainless steel base. Ink fusion was done using either ovens or moving belt furnace.
Thickness measurements were done using the
Amray Scanning Electron Microscope (SEM) or the Nikon Polarized Light Microscope (PLM).
TABLE 12A______________________________________ 60.degree. Gloss at Walker CountExample No. 0 200 800 1200______________________________________12-1 91.4 -- -- 84.512-2 93.2 -- -- 91.312-3 98.0 -- -- 95.612-4 98.7 -- -- 94.112-5 to -7 108.2.sup.a 106.3 89.3 105.312-8 to -10 103.6.sup.a 100.8 99.9 107.812-11 to -13 99.9.sup.a 105.7 98.3 105.112-14 to -16 101.6.sup.a 70.7 102.6 107.812-17 to -19 95.2.sup.a 100.5 97.0 103.412-20 to -22 86.5.sup.a 94.9 84.1 94.312-23 to -25 88.7.sup.a 100.2 88.6 86.012-26 to -28 90.1.sup.a 81.5 99.5 90.6______________________________________ .sup.a average of three samples
TABLE 12B__________________________________________________________________________ Wear Layer Deposition Deposition Ion O.sub.2 +Example Thickness Rate Temperature Cleaning Ion Al.sub.2 O.sub.3No. (microns) (A/S).sup.c (.degree.C.) Gas Assist Purity__________________________________________________________________________12-1 2.2 7.2 59-196 Ar Yes 99.99%12-2 4.9 31 90-123 Ar Yes 99.99%12-3 3.6 12 113-129 Ar Yes 99.99%12-4 5.3 33 114-134 Ar Yes 99.99%12-5 3.4 15 70-129 Ar Yes 99.8%12-6 3.4 15 70-129 Ar Yes 99.8%12-7 3.4 15 70-129 Ar Yes 99.8%12-8 3.4 15 61-134 Ar Yes 99.5%12-9 3.4 15 61-134 Ar Yes 99.5%12-10 3.4 15 61-134 Ar Yes 99.5%12-11 3.4 15 138-170 Ar Yes 99.99%12-12 3.4 15 138-170 Ar Yes 99.99%12-13 3.4 15 138-170 Ar Yes 99.99%12-14 7.7 17 71-170 Ar Yes 99.99%12-15 7.7 17 71-170 Ar Yes 99.99%12-16 7.7 17 71-170 Ar Yes 99.99%12-17 2.9 40 130-170 Ar Yes 99.5%12-18 2.9 40 130-170 Ar Yes 99.5%12-19 2.9 40 130-170 Ar Yes 99.5%12-20 11.6 40 100-206 Ar Yes 99.5%12-21 11.6 40 100-206 Ar Yes 99.5%12-22 11.6 40 100-206 Ar Yes 99.5%12-23 3.3 30 95-160 Ar No 99.5%12-24 3.3 30 95-160 Ar No 99.5%12-25 3.3 30 95-160 Ar No 99.5%12-26 8.6 60 250 Ar Yes 99.5%12-27 8.6 60 250 Ar Yes 99.5%12-28 8.6 60 250 Ar Yes 99.5%__________________________________________________________________________
The results showed that gloss retention performance is relatively insensitive to Al.sub.2 O.sub.3 deposition parameters. Thickness between 3 .mu. and 12 .mu.; deposition rates between 7.ANG./S and 60.ANG./S; and Al.sub.2 O.sub.3 purity between 99.5 and 99.99% (for isostatically pressed powders or crystals) did not effect Walkers Test performance.
EXAMPLES 13-1 AND 13-2
Samples were tested in the Walkers Test. One sample each was pulled at 200 and 800 counts while two samples were trafficked to 1200 counts.
PBMC was decorated by sublimation imprinting. Al.sub.2 O.sub.3 wear layers were evaporated by electron beam. No bake-out was used prior to evaporation.
Table 13A lists the data and gloss values for the samples tested. Stain resistance tests were done by applying each reagent for a period of four hours. The samples were cleaned with Micro and water followed by acetone. Delta E values were calculated from L, a, b readings on a Hunter Laboratory, Model D25 optical sensor. Table 13B lists the samples tested for stain resistance and their Delta E values.
TABLE 13A______________________________________ Wear LayerExample Thickness 60.degree. Gloss at Walker CountNo. Description (microns) 0 200 800 1200______________________________________13-1 Al.sub.2 O.sub.3 /Sub. 4.7 .+-. 0.3 54.6 45.9 48.8 49.5 Imprint/ PBMC13-2 Al.sub.2 O.sub.3 / 4.0 .+-. 0.3 61.1 56.7 56.5 51.7 Marble PBMC______________________________________
TABLE 13B__________________________________________________________________________ Sanford Shoe Hair BallExample Ink Iodine Polish Dye Point Ink Asphalt TotalNo. Delta E Delta E Delta E Delta E Delta E Delta E Delta E__________________________________________________________________________13-1 9.34 2.17 3.91 2.39 8.77 1.87 28.5313-2 6.75 1.35 2.94 1.30 17.39 2.64 32.37__________________________________________________________________________
No difference was observed in wear performance or adhesion of Al.sub.2 O.sub.3 applied over decorated (sublimation imprint) and non-decorated PBMC. Overall wear performance was good. Wear performance of marbled PBMC with Al.sub.2 O.sub.3 was similar to that of sublimation imprinted PBMC with Al.sub.2 O.sub.3.
The samples maintained a fairly level gloss curve. The samples had very few fine scratches. The large scratches were not numerous. The scratches become readily visible when they penetrated the Al.sub.2 O.sub.3 and destroyed the print. The white color of the scratches was apparently caused by stress whitening of the PBMC.
EXAMPLES 14-1 TO 14-14
Examples 14-1 to 14-7 were formed by depositing two to three microns of SiOx by E-beam evaporation using a Web coater onto the 24-inch wide, 7-mil filled mylar sheets. Coating speed was about 30 ft/min.
Examples 14-8 to 14-14 were formed by depositing 3 microns of SiOx by E-beam evaporation onto back side of samples formed by the procedure of Examples 14-1 to 14-7. The procedure utilized a freshly cleaned and refoiled deposition chamber, an O.sub.2 ion assist, but not a bakeout. The samples were not precleaned prior to loading into the deposition chamber, and were not subjected to a plasma cleaning step after loading.
The SiOx on mylar was adhered to a bulk molding compound using adhesive release tape. Table 14 gives average gloss values at each traffic interval.
TABLE 14______________________________________ 60.degree. Gloss at Walker CountExample No. 0 200 400 800 1200______________________________________14-1 to 14-3 19.1 31.3 -- 17.2 10.314-4 to 14-7 23.7 16.7 14.9 9.9 4.7 14-8 to 14-10 35.4 40.9 -- 27.0 29.514-11 to 14-14 29.2 33.7 26.3 21.2 9.5______________________________________
EXAMPLES 15-1 TO 15-15
Six-inch square samples were tested in the Walkers Test. Table 15 lists the sample descriptions and the respective gloss values.
Examples 15-1 to 15-12 were prepared with 7-mil, 302 stainless steel substrates. Examples 15-13 to 15-15 were prepared with 14-mil cold rolled steel supplied by Chicago Vitreous with their ceramic ground coat. The substrates were coated as follows:
Examples 15-1 to 15-4: 30 micron-H34002 primer and 10 micron-H34002 textured pattern with 20% matting agent H7003.
Examples 15-5 to 15-8: 30 micron-H34002 primer and 10 micron-H34002 textured pattern with 20% matting agent H7003 and a 5.95 micron thick clear, Heraeus H30011, protective ceramic glaze.
Examples 15-9 to 15-12: 30 micron-H34002 primer and 10 micron-H34002 textured pattern with 20% matting agent H7003 and a 2.40 micron thick aluminum oxide layer.
Examples 15-13 to 15-15: 56.6 micron of ground coat, 29.1 micron-H34002 primer as the wear layer.
The primer and matting agent were manufactured by Heraeus.
TABLE 15______________________________________ Total Nominal Al.sub.2 O.sub.3 Enamel Wear LayerExample Thickness Walker 60.degree. Gloss ThicknessNo. (Micron) Cycles Initial Final (Micron)______________________________________15-1 40 200 52.8 67.515-2 40 800 66.5 64.415-3 40 1200 64.8 67.715-4 40 1200 61.0 59.715-5 40 200 57.4 65.6 5.9515-6 40 800 55.2 53.3 5.9515-7 40 1200 65.3 63.5 5.9515-8 40 1200 61.7 64.6 5.9515-9 40 200 71.9 75.1 2.40 15-10 40 800 72.5 71.0 2.40 15-11 40 1200 67.8 73.0 2.40 15-12 40 1200 66.3 66.6 2.40 15-13 86 200 89.8 95.5 15-14 800 90.6 96.0 15-15 1200 88.6 87.1______________________________________
As shown in Table 15, the gloss values of the three stainless-steel-substrate categories are essentially unchanged after a total traffic count of 1200. Appearance retention differences between the categories were noted however. The stainless-steel structure without a wear layer, exhibited more visually objectionable scratches than the glaze-coated and aluminum oxide-coated structures. These later two categories had hard protective wear layers which appear to afford increased scratch resistance.
Although the low-carbon-steel structure exhibited excellent gloss retention, scratch resistance was poor compared to the other structures. Most of the scratch damage was limited to the upper-most ceramic layer which was the Heraeus H34002 system. The type of damage present indicated a poor level of adhesion between the ground coat and the Heraeus ceramic.

Number	Name	Date
4604181	Mirtich et al.	Aug 1986
4614556	Fry et al.	Sep 1986
4702963	Phillips et al.	Oct 1987
4743510	Nemeth	May 1988

Floor covering with inorganic wear layer

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US Referenced Citations (4)

Non-Patent Literature Citations (6)

Entry
Eli Yablonovitch et al., Appl. Phys. Letter, 51(26), Dec. 28, 1987, pp. 2222-2224, Article Entitled "Extreme Selectivity in the Lift-Off of Epitaxial GaAs Films".
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Ryszard Lamber, Journal of Materials Science Letters 5 (1986), pp. 177-178, Article Entitled "Thin Boehmite Films: Preparation and Structure".
J. C. Huling et al., J. Am. Ceram. Soc., 71[4] C-222-C-224 (1988), Article Entitled "A Method for Preparation of Unsupported Sol-Gel Thin Films".
Trade Literature Entitled, "Interior/Wall Facings From AllianceWall", AllianceWall, Norcross, GA 30092.
Trade Literature Entitled, "Armor-Stat Dissipative Floor Tile", 1988, Trio-Tech International Static Systems, San Fernando, CA 91340.