EP0073313A2 - A stitch bonded fabric for reinforcing coated abrasive backings - Google Patents
A stitch bonded fabric for reinforcing coated abrasive backings Download PDFInfo
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- EP0073313A2 EP0073313A2 EP82105651A EP82105651A EP0073313A2 EP 0073313 A2 EP0073313 A2 EP 0073313A2 EP 82105651 A EP82105651 A EP 82105651A EP 82105651 A EP82105651 A EP 82105651A EP 0073313 A2 EP0073313 A2 EP 0073313A2
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- European Patent Office
- Prior art keywords
- yarns
- yarn
- fabric
- stitch
- warp
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Classifications
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- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
- D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
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- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04B—KNITTING
- D04B21/00—Warp knitting processes for the production of fabrics or articles not dependent on the use of particular machines; Fabrics or articles defined by such processes
- D04B21/14—Fabrics characterised by the incorporation by knitting, in one or more thread, fleece, or fabric layers, of reinforcing, binding, or decorative threads; Fabrics incorporating small auxiliary elements, e.g. for decorative purposes
- D04B21/16—Fabrics characterised by the incorporation by knitting, in one or more thread, fleece, or fabric layers, of reinforcing, binding, or decorative threads; Fabrics incorporating small auxiliary elements, e.g. for decorative purposes incorporating synthetic threads
- D04B21/165—Fabrics characterised by the incorporation by knitting, in one or more thread, fleece, or fabric layers, of reinforcing, binding, or decorative threads; Fabrics incorporating small auxiliary elements, e.g. for decorative purposes incorporating synthetic threads with yarns stitched through one or more layers or tows, e.g. stitch-bonded fabrics
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- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2403/00—Details of fabric structure established in the fabric forming process
- D10B2403/02—Cross-sectional features
- D10B2403/024—Fabric incorporating additional compounds
- D10B2403/0241—Fabric incorporating additional compounds enhancing mechanical properties
- D10B2403/02412—Fabric incorporating additional compounds enhancing mechanical properties including several arrays of unbent yarn, e.g. multiaxial fabrics
Definitions
- the present invention relates to stitch-bonded fabrics which are especially suitable for reinforcing the backings of coated abrasives.
- Stitch-bonded fabrics in general have been known for at least the last twenty years. However, it has not been appreciated that such fabrics could confer special advantages when used as the reinforcing substrate for coated abrasive backings. Thus no fabrics explicitly suitable for such purposes were known to the applicant from prior art.
- the preferred machines for the fabrics of the present invention are those of the Malimo type.
- the description of mechanical characteristics of Malimo machines given immediately below condenses from this publication those characteristics believed by the applicant to be most relevant to design of fabrics suitable for use in coated abrasives.
- Malimo machines have three principal mechanical characteristics which limit the variety of fabric constructions available from them. The first of these limits is provided by a group of several matched mechanical structures which fix a maximum "gauge" or number of yarns per 25 mm of width for the warp yarn and stitching yarn assemblies which can be used with the machine. Twelve possible gauges from 3 to 22 are available from the manufacturer.
- the second of the principal mechanical limitations of the Malimo machine is its stitch length. This can be adjusted in 20 steps within a range of 0.7 to 5 mm. It should be noted that this nominal "stitch length" is actually the projected length in the direction of the warp yarns. When a tricot style stitch is used, as was the case for the fabrics to be described here, the actual spatial orientation of the stitch is at a substantial angle to the warp yarns, and the actual length is correspondingly longer than the nominal length. In addition, because the stitch yarns form loops, the length of yarn consumed for each stitch is generally considerably longer than either the nominal or actual lengtho With the fabrics described below, stitch yarn length consumption was about four times warp yarn length consumption.
- hooks which hold the fill yarns in tension until they can be stitched to the warp.
- Hook units are available in linear densities from 8 to 48 hooks per 25 mmo Under the normal conditions of use as contemplated by the instructions furnished by the manufacturer, no more than one bend of fill yarns around each hook is accommodated during fabric assembly operations.
- this result is preferably attained by the use of warp arrays with yarns of high denier, high tenacity synthetic multifilament or glass in a number of at least 12 yarns per 25 mm of fabric width, fill yarn arrays of smaller denier texturized multifilament or staple synthetic yarn in a number of at least 64 per 25 mm of fabric length, and by fine denier stitch yarns with a breaking strength of at least 0.007 dekanewtons per denier.
- Malimo machines with model numbers 14010 or 14011 were preferred for making the fabrics of the present invention. Liba machines and Raschel knitting machines make equally satisfactory fabrics but are limited to lower speeds of operation and thus are less economicalo
- high tenacity yarns are very effective in providing warp tensile strength, they provide relatively little cover or opportunity for facile mechanically aided adhesion of cloth finishing adhesives, which are needed to complete the final backings on which coated abrasives are to be made. I have found it possible to compensate for these deficiencies by using high linear densities of relatively small spun staple or textured multifilament fill yarns. The greater surface area per unit mass of these yarns, as compared with the warp yarns, provides superior possibilities for mechanical adhesion of the finishing adhesives and ready achievement of adequate cover, when combined with suitable processing techniques for the finishing.
- Hooks 5 mm high were used for all constructions shown except those with 500 denier fill yarns; with these larger yarns the 7 mm size hooks gave better results.
- Medium size sliding needles and closing wires, 1.8 mm diameter stitching yarn guide holes, and round rather than oval retaining pins among the choices offered by the manufacturer were preferred for the fabrics shown.
- Both fill yarn carrier reeds and hook carriers with 32 openings per 25 mm were used for fabrics with 64 or 128 fill yarns per 25 mm, while carrier reeds and hook carriers with 24 openings per 25 mm were used for achieving 96 fill yarns per 25 mm.
- stitch yarns Additional possibilities for adhesion and cover are provided by the stitch yarns.
- synthetic multifilament yarns in deniers from 70 to 220 very satisfactory as stitch yarns for these fabrics.
- the primary requisite from the stitch yarn for the ultimate coated abrasive is sufficient strength to resist rupture between the warp and fill arrays of yarns under use conditions.
- 70 denier polyester yarn with a breaking strength of at least 0.008 daN per denier was found to be adequate for most purposes.
- Each stitch normally forms a loop around only one warp yarn (unless more than one yarn is fed through a single opening as noted above), but the number of fill yarns inside a stitch loop can vary from none to several, depending on how many fill yarns happen to occupy the space inside the fixed stitch length.
- a random pattern of short, relatively open spaces may often be observed in the fabric produced, as a result of greater or lesser than average number of fill yarns being caught inside the loops of particular stitches. Within the limits described herein, this pattern has not been found to cause any difficulty in the coated abrasives produced with such fabrics as substrates.
- the cover factor for the fill yarn array noted in Table 1 is the same as the value often called "fractional coverage" by others; i.e., the fraction of the total area enclosed within the borders of a sample of the fabric which is covered by the fill yarn array therein. In principle, this value could be easily calculated from a knowledge of the linear density and the diameter of the fill yarns: If n is the number of fill yarns per unit length of the fabric and d is the diameter of each yarn in the same units, the cover factor is 100nd%. In practice, measuring the diameter of yarn precisely is very difficult, and in conformance with common textile art practice, the cover factor used herein was determined by an indirect calculation making use of the density and denier size of the yarn. From the definition of denier (cf.
- the density of a yarn in turn depends on the fundamental density of the fibers which compose it and on how tightly the fibers are packed.
- the latter characteristic of the yarn is quantified as a packing fraction, which when multiplied by the fiber density gives the yarn density.
- the following values in gm/cm for fiber density of the fill yarn fibers listed in Table 1 were taken: polyester, 1.3; cotton, 1.56; and polyamide, 1.14. Packing fractions taken were: textured polyamide, 0.80; textured polyester, 0.70; staple polyester, 0.59; and mixed yarn, 1.0.
- the fabrics specified in Table 1, or other fabrics constructed using the same principles, may be finished in a variety of ways to make suitable backings for coated abrasives. These backings in turn may be coated with any of the variety of maker adhesives, abrasive grits, and sizer adhesives, well known in the art. Some specific examples of these ways to use my invention are given below, and others will be readily apparent to those skilled in the art of manufacturing coated abrasives, upon considering the teachings herein in combination with those of the aforesaid copending application.
- Standard sizing rolls are employed to apply the following composition in the amount of 40 to 60 grams per square meter.
- the fill yarn side of the fabric was facing up.
- the fabric Upon completion of the application of the saturant the fabric is dried on a tenter frame for at least 3 minutes in a hot air oven in which the temperature in the entry zone is 96°C., and the temperature at the exit zone is 177°C. A tension of at least 3.5 Newtons per centimeter (N/cm) of width is maintained on the fabric during its travel through the oven. This process not only dries the saturant but also heat-sets the fabric.
- composition of the frontfill coating applied to the fill yarn side in this example, but which can instead be applied to the warp yarn side if desired, is as follows:
- the front fill coating composition is applied with a knife in the amount of 150-165 dry grams per square meter (gm/m 2 ), and water may be added as necessary to maintain the required viscosity for proper coating.
- the coated cloth is again dried on a tenter frame with a tension of at least 3.5 N/cm of width by passing through a hot air oven in which the entry temperature is 96°C. and the exit zone temperature is 150°C.
- composition is applied by knife coating in the amount of 140-165 gm/m 2 and dried in an oven having an entry zone temperature of 66°C. and an exit zone of 93°C.
- a suitable formulation to be applied to the frontsized side of the backing is as follows:
- a size coat (about 160 gm/m2 dry) of the same composition as the maker coat, except of lesser viscosity, is then applied according to usual techniques.
- the wet adhesive layer is then dried: 25 minutes at 52°C., 25 minutes at 57°C., 18 minutes at 82°C., 25 minutes at 88°C., and 15 minutes at 107°C., after which final cure at 110°C, for 8 hours is given.
- the coated abrasive material is then ready to be converted according to usual techniques, into belts, discs, and other desired abrasive products.
- Cloth of the construction described with the identifying number 3 in Table 1 was coated by the dip and squeeze method with a two roll padder, using the following saturant:
- the fabric was held in a tenter frame to prevent width shrinkage and dried by passing for 3.75 minutes through an oven with an entry zone temperature of 135°C. and an exit zone temperature of 240°C. Sufficient saturant to give a dry add-on of 52 + 7 gm/m 2 was used.
- the ingredients are added in the order listed, with continuous stirring.
- the adhesive is coated on the saturated fabric by a knife over roll technique in sufficient quantity to give 175-225 gm/m 2 of adhesive after drying.
- the coated fabric is again tentered to eliminate any possible loss in width and is passed for 3.75 minutes through an oven with an entry zone temperature of 65°C. and an exit zone temperature of 107°C.
- the backfilled fabric was then frontfilled on the opposite side from backfilling with the same adhesive composition as used for backfilling, in sufficient quantity to give 120-180 gm/m 2 of dried frontfill. Coating of frontfill could be accomplished either by knife or roll techniques with approximately equal facility. Oven conditions for drying frontfill were the same as for backfill, but satisfactory results in drying at this stage could be achieved without tentering if desired.
- the finished backing was then ready for making and sizing steps to convert it to a coated abrasive by conventional means as described briefly in Example 1.
- Table 2 shows physical properties of the coated abrasives prepared in Examples 1-3 and compares them against the same measurements on commercial coated abrasive products with woven cloth backings.
- the tensile strength of the products described herein is closely comparable to the commercial products for Example 1 and superior for Examples 2 and 3.
- the burst strength which is generally correlated with resistance to many environmental hazards during use of coated abrasives, is quite notably superior for Example 2 and closely comparable for the others. Elongation is higher for Examples 1 and 2 but lower or comparable for Fabric 3.
Abstract
Description
- The present invention relates to stitch-bonded fabrics which are especially suitable for reinforcing the backings of coated abrasives.
- Stitch-bonded fabrics in general have been known for at least the last twenty years. However, it has not been appreciated that such fabrics could confer special advantages when used as the reinforcing substrate for coated abrasive backings. Thus no fabrics explicitly suitable for such purposes were known to the applicant from prior art.
- In order to produce stitch-bonded fabric in large volume at low cost, it is necessary to use one of the special machines designed for such purposes. A wide variety of machines are available commercially, including those supplied under the trade name Malimo (short for MALIMO Type Malimo) by Unitechna Aushandelgesellschaft mbH of Karl Marx Stadt, DDR, those with the trade name Weft/Loc made by Liba Maschinenfabrik GmbH, D-8674 Naila, FRG, and Raschel knitting machines. (A list of suppliers of Raschel machines is given on pages 31-38 of Volume 43, No. 35 of Knitting Times, the official publication of the National Knitted Outerwear Assoc., 51 Madison Avenue, New York, New York, 10010.)
- These commercially available machines are normally limited to a maximum number of about one wrap yarn per millimeter (mm) of fabric width. This limitation is believed to be necessary to accommodate a sufficient number of stitch or loop forming devices in the machine to form bonds across the entire width of the fabric substantially simultaneously. Because conventional woven fabrics for coated abrasives mostly contain at least twice this many warp yarns, no simple adaptation of the woven fabric designs to the requirements of stitch bonding machines was feasible.
- It should be noted that it is possible to feed more than one warp yarn through each of the machine openings for such yarns provided in many of these machines. However, any such multiplicity of yarns fed through one opening will be bonded by the machine as if it were a single yarn. Thus the practical effect achieved by a multiplicity of yarns fed through one opening is essentially the same as that from using one plied yarn with a number of plies equal to the multiplicity of single unplied yarns. In both woven and stitch bonded fabrics, the results achieved from use of such plied yarns are not generally as satisfactory for fabric cover and for the desirable combination of strength with flexibility as can be achieved with evenly spaced finer yarns which give the same total warp tensile strength.
- As noted below, the preferred machines for the fabrics of the present invention are those of the Malimo type. A publication by the manufacturer of Malimo machines, VEB Nahwirkmaschinenbau Malimo, Karl Marx Stadt, DDR, No. 24-2/3, "Sewing-Knitting Machines MALIMO Technical Possibilities and Technology", Part 2, (identified at the end as Ag 07/010/77. III 3 1 74/8900/77 1,0), describes the general range of operating conditions possible for machines of this particular type. The description of mechanical characteristics of Malimo machines given immediately below condenses from this publication those characteristics believed by the applicant to be most relevant to design of fabrics suitable for use in coated abrasives. In this condensation, the term "weft" has been changed to "fill" in accordance with common United States practice, and the term "hook needle" has been shortened to "hook"; all other terms describing the mechanical parts of the machines have been taken directly from the referenced publication.
- Malimo machines have three principal mechanical characteristics which limit the variety of fabric constructions available from them. The first of these limits is provided by a group of several matched mechanical structures which fix a maximum "gauge" or number of yarns per 25 mm of width for the warp yarn and stitching yarn assemblies which can be used with the machine. Twelve possible gauges from 3 to 22 are available from the manufacturer.
- The second of the principal mechanical limitations of the Malimo machine is its stitch length. This can be adjusted in 20 steps within a range of 0.7 to 5 mm. It should be noted that this nominal "stitch length" is actually the projected length in the direction of the warp yarns. When a tricot style stitch is used, as was the case for the fabrics to be described here, the actual spatial orientation of the stitch is at a substantial angle to the warp yarns, and the actual length is correspondingly longer than the nominal length. In addition, because the stitch yarns form loops, the length of yarn consumed for each stitch is generally considerably longer than either the nominal or actual lengtho With the fabrics described below, stitch yarn length consumption was about four times warp yarn length consumption.
- The third of the principal mechanical limitations of the machine is provided by the assemblies of hooks which hold the fill yarns in tension until they can be stitched to the warp. Hook units are available in linear densities from 8 to 48 hooks per 25 mmo Under the normal conditions of use as contemplated by the instructions furnished by the manufacturer, no more than one bend of fill yarns around each hook is accommodated during fabric assembly operations.
- It should be noted that it is an inherent characteristic of Malimo machines to lay fill yarns in two distinct groups of symmetric small angles on opposite sides of an imaginary line perpendicular to the warp yarn array. All fill yarn counts in this description are to be understood as including both of these fill yarn groups in the count.
- The above referenced and incorporated Malimo publication gives some specifics of the construction of several fabrics suitable for other uses than coated abrasives. This is the largest such description of specific stitch-bonded fabrics known to applicant.
- In accordance with the present invention, by careful selection and combination of particular types and sizes of yarn, and by the operation of commercially available machines outside the scope of the operating instructions furnished by their suppliers, it has been found possible to manufacture economical and effective fabrics for a wide variety of coated abrasives. In general, a satisfactory fabric will result if the warp yarn array has a tensile strength of at least 30 dekanewtons per centimeter of fabric width, the fill yarn array has a cover factor as defined below of at least 40%, and the stitching yarns have a tensile breaking strength of at least 0=5 dekanewtons each. For most purposes, this result is preferably attained by the use of warp arrays with yarns of high denier, high tenacity synthetic multifilament or glass in a number of at least 12 yarns per 25 mm of fabric width, fill yarn arrays of smaller denier texturized multifilament or staple synthetic yarn in a number of at least 64 per 25 mm of fabric length, and by fine denier stitch yarns with a breaking strength of at least 0.007 dekanewtons per denier.
- Malimo machines with model numbers 14010 or 14011 were preferred for making the fabrics of the present invention. Liba machines and Raschel knitting machines make equally satisfactory fabrics but are limited to lower speeds of operation and thus are less economicalo
- It was considered desirable to provide reinforcing fabrics of my new type with tensile strengths at least equal to those of conventional coated abrasives with woven cloth substrates. Two of the most important classes of these conventional abrasives, commonly designated in the trade as X weight and Y weight, have tensile strengths of about 30 and 38 dekanewtons per centimeter (daN/cmi of width respectively We have found that this level of tensile strength with stitch bonded fabrics can be achieved by using warp gauges from 12 to 22 with synthetic multifilament or glass yarns having breaking tenacities of at least 0.007 dekanewtons per denier. Using a coarser gauge can also achieve adequate tensile strength with high denier yarns.
- Although high tenacity yarns are very effective in providing warp tensile strength, they provide relatively little cover or opportunity for facile mechanically aided adhesion of cloth finishing adhesives, which are needed to complete the final backings on which coated abrasives are to be made. I have found it possible to compensate for these deficiencies by using high linear densities of relatively small spun staple or textured multifilament fill yarns. The greater surface area per unit mass of these yarns, as compared with the warp yarns, provides superior possibilities for mechanical adhesion of the finishing adhesives and ready achievement of adequate cover, when combined with suitable processing techniques for the finishing.
- An important feature of the invention, particularly useful for facilitating the achievement of adequate cover in the fabric, was my discovery that it was possible to produce fabrics having two or more fill yarns on each hook by operating outside the range of instructions furnished with the Malimo machine. If the machine gears were chosen so as to advance the fill yarn carrier, which is a mechanical part separate and distinct from the hook carriers, at half the minimum speed recommended by the manufacturer for the combination of hook spacing and number to fill yarns supplied, an average of two yarns would be retained by each hooko Alternatively, the speed of advance could be left the same, but the fill yarn carrier doubled in width. Similarly. advancing the carrier at one quarter of recommended speed or quadrupling its width would result in an average of four yarns retained per hook: Hooks 5 mm high were used for all constructions shown except those with 500 denier fill yarns; with these larger yarns the 7 mm size hooks gave better results. Medium size sliding needles and closing wires, 1.8 mm diameter stitching yarn guide holes, and round rather than oval retaining pins among the choices offered by the manufacturer were preferred for the fabrics shown. Both fill yarn carrier reeds and hook carriers with 32 openings per 25 mm were used for fabrics with 64 or 128 fill yarns per 25 mm, while carrier reeds and hook carriers with 24 openings per 25 mm were used for achieving 96 fill yarns per 25 mm.
- Additional possibilities for adhesion and cover are provided by the stitch yarns. We have found synthetic multifilament yarns in deniers from 70 to 220 very satisfactory as stitch yarns for these fabrics. Aside from the resilience and flexibility needed in the stitch yarn to permit efficient operation of a stitch-bonding machine, the primary requisite from the stitch yarn for the ultimate coated abrasive is sufficient strength to resist rupture between the warp and fill arrays of yarns under use conditions. By experiment, 70 denier polyester yarn with a breaking strength of at least 0.008 daN per denier was found to be adequate for most purposes. For coated abrasives to be used under extremely damage prone conditions, however, it was advantageous to use 110, 140, or even 220 denier stitch yarns.
- In general, shorter stitch lengths will give more uniform appearing fabrics, while longer stitch lengths will give more economy as a result of faster production speeds. For coated abrasive substrate fabrics, it has not been found advisable to use longer stitch lengths than 1.8 mm. The preferred range for most fabrics is 1.2 to 1.8 mm.
- Each stitch normally forms a loop around only one warp yarn (unless more than one yarn is fed through a single opening as noted above), but the number of fill yarns inside a stitch loop can vary from none to several, depending on how many fill yarns happen to occupy the space inside the fixed stitch length. With long stitches and moderate fill yarn densities, a random pattern of short, relatively open spaces may often be observed in the fabric produced, as a result of greater or lesser than average number of fill yarns being caught inside the loops of particular stitches. Within the limits described herein, this pattern has not been found to cause any difficulty in the coated abrasives produced with such fabrics as substrates.
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- The cover factor for the fill yarn array noted in Table 1 is the same as the value often called "fractional coverage" by others; i.e., the fraction of the total area enclosed within the borders of a sample of the fabric which is covered by the fill yarn array therein. In principle, this value could be easily calculated from a knowledge of the linear density and the diameter of the fill yarns: If n is the number of fill yarns per unit length of the fabric and d is the diameter of each yarn in the same units, the cover factor is 100nd%. In practice, measuring the diameter of yarn precisely is very difficult, and in conformance with common textile art practice, the cover factor used herein was determined by an indirect calculation making use of the density and denier size of the yarn. From the definition of denier (cf. footnote 1 in Table 1), it follows that the mass m in grams of a one centimeter length of yarn is equal to the denier (D) divided by 9 x 105. The volume v in cubic centimeters of the same length of yarn is approximated as that of a cylinder of the same diameter,. so that v = (πd2)/4. By definition, the density p = m/v. Combining and rearranging these expressions gives % cover factor = n(4D/90 pπ)½.
- The density of a yarn in turn depends on the fundamental density of the fibers which compose it and on how tightly the fibers are packed. The latter characteristic of the yarn is quantified as a packing fraction, which when multiplied by the fiber density gives the yarn density. The following values in gm/cm for fiber density of the fill yarn fibers listed in Table 1 were taken: polyester, 1.3; cotton, 1.56; and polyamide, 1.14. Packing fractions taken were: textured polyamide, 0.80; textured polyester, 0.70; staple polyester, 0.59; and mixed yarn, 1.0.
- It should be carefully noted that the calculations for cover factor noted above assume that the fill yarns are in position as laid out before stitching. Small variations from this value are expected after the fabric is stitched together. No attempt was made to calculate these latter variations, because they did not appear to affect the performance of coated abrasives made with the fabrics herein described as backing substrates. However, fabrics with fill cover factors of less than 40% as calculated above could not easily be finished suitably for receiving maker adhesive and grain coats in the process of making a coated abrasive with a conventionally continuous backing.
- The fabrics specified in Table 1, or other fabrics constructed using the same principles, may be finished in a variety of ways to make suitable backings for coated abrasives. These backings in turn may be coated with any of the variety of maker adhesives, abrasive grits, and sizer adhesives, well known in the art. Some specific examples of these ways to use my invention are given below, and others will be readily apparent to those skilled in the art of manufacturing coated abrasives, upon considering the teachings herein in combination with those of the aforesaid copending application.
- Fabric of the construction with identification number 1 in Table 1 was used. This fabric was then saturated with a resin and acrylic latex composition to prepare it for frontfilling, backfilling, and coating with maker grain and size coat. A heat setting step is combined with the drying of the saturant. The fabric finishing steps will now be described in more detail.
- Standard sizing rolls are employed to apply the following composition in the amount of 40 to 60 grams per square meter. The fill yarn side of the fabric was facing up.
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- Upon completion of the application of the saturant the fabric is dried on a tenter frame for at least 3 minutes in a hot air oven in which the temperature in the entry zone is 96°C., and the temperature at the exit zone is 177°C. A tension of at least 3.5 Newtons per centimeter (N/cm) of width is maintained on the fabric during its travel through the oven. This process not only dries the saturant but also heat-sets the fabric.
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- The front fill coating composition is applied with a knife in the amount of 150-165 dry grams per square meter (gm/m2), and water may be added as necessary to maintain the required viscosity for proper coating. The coated cloth is again dried on a tenter frame with a tension of at least 3.5 N/cm of width by passing through a hot air oven in which the entry temperature is 96°C. and the exit zone temperature is 150°C.
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- The composition is applied by knife coating in the amount of 140-165 gm/m2 and dried in an oven having an entry zone temperature of 66°C. and an exit zone of 93°C.
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- To the adhesively coated fabric is then applied by conventional electrostatic means 520-550 gm/m2 of grit 60 high purity aluminum oxide abrasive grain. The abrasive- adhesive coated backing member is then heated for 25 minutes at 77°C., 25 minutes at 88°C., and 47 minutes at 107°C. to provide a dry adhesive layer (about 260 gm/m2) and to anchor the abrasive grains in the desired orientation=
- Afterwards, a size coat (about 160 gm/m2 dry) of the same composition as the maker coat, except of lesser viscosity, is then applied according to usual techniques. The wet adhesive layer is then dried: 25 minutes at 52°C., 25 minutes at 57°C., 18 minutes at 82°C., 25 minutes at 88°C., and 15 minutes at 107°C., after which final cure at 110°C, for 8 hours is given. The coated abrasive material is then ready to be converted according to usual techniques, into belts, discs, and other desired abrasive products.
- While the above example described finishing the backing with the abrasive coat on the fill side of the cloth, in other cases it may be more desirable to coat on the warp side.
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- Dissolve item 2 in item 1 with stirring, then add item 3 and stir until dissolved, Add item 4 and stir for 5 minutes; weigh out item 5 into separate container and add item 6 while stirring to adjust pH to near that of the RF premix (about 9) then add premix into item 5 with gentle stirring. If foam develops during addition, add small portions of an antifoam agent. (Falcoban S, made by Fallek Chemical Corp., 460 Park Ave., New York, NY 10022, was suitable, but many others should work equally well. If foam develops during coating, additional antifoam may be added.) This mixture should be stirred for at least 15 minutes after the last addition and held for 24 hours before use.
- After coating, the fabric was held in a tenter frame to prevent width shrinkage and dried by passing for 3.75 minutes through an oven with an entry zone temperature of 135°C. and an exit zone temperature of 240°C. Sufficient saturant to give a dry add-on of 52 + 7 gm/m2 was used.
- After saturation and drying as described above, the fabric was backfilled, on the side where warp yarns are most prominently exposed, with the adhesive mixture noted below:
- Resole phenol-formaldehyde resin with formaldehyde to phenol molar ratio of about 2.1 - 394 parts; Resole phenolic resin with F:P molar ratio about 0.95 - 282 parts; calcium carbonate (sized as described in U.S. Patent 2,322,156) - 850 parts; Hycar 2600X138 acrylic latex (previously adjusted to a pH value of 8-9 with 10% aqueous sodium hydroxide solution) - 102 partso
- In preparing this solution, the ingredients are added in the order listed, with continuous stirring. The adhesive is coated on the saturated fabric by a knife over roll technique in sufficient quantity to give 175-225 gm/m2 of adhesive after drying. For drying, the coated fabric is again tentered to eliminate any possible loss in width and is passed for 3.75 minutes through an oven with an entry zone temperature of 65°C. and an exit zone temperature of 107°C.
- The backfilled fabric was then frontfilled on the opposite side from backfilling with the same adhesive composition as used for backfilling, in sufficient quantity to give 120-180 gm/m2 of dried frontfill. Coating of frontfill could be accomplished either by knife or roll techniques with approximately equal facility. Oven conditions for drying frontfill were the same as for backfill, but satisfactory results in drying at this stage could be achieved without tentering if desired.
- If any undesirable surface roughness was apparent on the finished fabric after completion of the steps above, it was calendered at a pressure of about 350 daN/cm of width, using conventional calender rolls heated to a temperature of 63°Co
- The finished backing was then ready for making and sizing steps to convert it to a coated abrasive by conventional means as described briefly in Example 1.
- Fabric number 8 from Table 1 was used for this example. All other steps were the same as for Example 2.
- Table 2 shows physical properties of the coated abrasives prepared in Examples 1-3 and compares them against the same measurements on commercial coated abrasive products with woven cloth backings. The tensile strength of the products described herein is closely comparable to the commercial products for Example 1 and superior for Examples 2 and 3. The burst strength, which is generally correlated with resistance to many environmental hazards during use of coated abrasives, is quite notably superior for Example 2 and closely comparable for the others. Elongation is higher for Examples 1 and 2 but lower or comparable for Fabric 3.
- Excessive elongation, specifically beyond the capacity for adjustment of the particular machine utilizing a coated abrasive belt, is undesirable, but otherwise elongation is not known to have any significant effect on the grinding performance. Thus very stretch-resistant warp yarns such as the glass of Example 3 can be used when needed, and the greater general toughness of a more easily stretched warp yarn type such as polyester can be advantageously used when the highest possible stretch resistance is not needed.
- The adequacy of performance of the coated abrasives made by Examples 1-3 has been confirmed by actual grinding tests in both laboratory and field use.
- It should be noted that by the term "yarn" used herein in the description and claims, we intend to include any continuous linear structures of any type of fiber twisted or laid together, whether made of natural or synthetic fibers, including a single monofilament. However, we do not consider unconsolidated short fibers to qualify as yarn for the purposes of my invention. Thus the fibers in mats or fleeces are not considered yarns by my definition. In particular, for "fill yarns" it is necessary for the structure so-called to be able to sustain tensile forces across the entire width of a fabric. Both fill and warp yarns, although possibly composed of twisted (and thus consolidated) short fibers, will normally be continuous for dimensions many times longer than the width of a fabric, often for hundreds of meters or more. Such continuity may of course be achieved by knotting or otherwise joining previously separate structures during the course of manufacturing a fabric.
Claims (9)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT82105651T ATE24341T1 (en) | 1981-08-31 | 1982-06-25 | STITCHING MATERIAL FOR REINFORCEMENT OF ABRASIVE COATINGS. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29753881A | 1981-08-31 | 1981-08-31 | |
US297538 | 1981-08-31 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0073313A2 true EP0073313A2 (en) | 1983-03-09 |
EP0073313A3 EP0073313A3 (en) | 1984-03-28 |
EP0073313B1 EP0073313B1 (en) | 1986-12-17 |
Family
ID=23146743
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP82105651A Expired EP0073313B1 (en) | 1981-08-31 | 1982-06-25 | A stitch bonded fabric for reinforcing coated abrasive backings |
Country Status (12)
Country | Link |
---|---|
EP (1) | EP0073313B1 (en) |
JP (1) | JPS5841951A (en) |
AT (1) | ATE24341T1 (en) |
AU (1) | AU557338B2 (en) |
BR (1) | BR8204384A (en) |
CA (1) | CA1215242A (en) |
DD (1) | DD202320A5 (en) |
DE (2) | DE73313T1 (en) |
ES (1) | ES8502176A1 (en) |
MX (1) | MX171960B (en) |
YU (1) | YU163282A (en) |
ZA (1) | ZA824506B (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4474585A (en) * | 1983-05-31 | 1984-10-02 | Norton Company | Synthetic yarn-reinforced flexible webs stabilized against elongation, coated abrasive thereon, and process therefor |
DE3339305A1 (en) * | 1983-10-29 | 1985-05-23 | Saerbeck-Textil Wagener KG, 4401 Saerbeck | Flexible coating carrier produced by the stitch-bonding technique |
EP0267030A2 (en) * | 1986-11-05 | 1988-05-11 | E.I. Du Pont De Nemours And Company | Stitched polyethylene plexifilamentary sheet |
WO1994018367A1 (en) * | 1993-02-04 | 1994-08-18 | Minnesota Mining And Manufacturing Company | Stitchbonded articles and method of making same |
US8960248B2 (en) | 2009-10-15 | 2015-02-24 | Michelin Recherche Et Technique S.A. | Method and apparatus for multilayer shear band reinforcement |
US9272576B2 (en) | 2010-03-12 | 2016-03-01 | Michelin Recherche Et Technique S.A. | Structurally supported, non-pneumatic wheel with continuous loop reinforcement assembly |
US9346317B2 (en) | 2010-12-29 | 2016-05-24 | Michelin Recherche Et Technique S.A. | Non-pneumatic tire with reinforcement band spacer and method of manufacturing same |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4725487A (en) * | 1986-03-28 | 1988-02-16 | Norton Company | Flexible coated abrasive and fabric therefor |
DE8912060U1 (en) | 1989-10-10 | 1991-02-07 | Norddeutsche Schleifmittel-Industrie Christiansen & Co (Gmbh & Co), 2000 Hamburg, De | |
BR112013010354A2 (en) | 2010-10-27 | 2016-08-02 | Michelin & Cie | transverse groove tire tread and a method of manufacturing a transverse groove tire tread |
US9555591B2 (en) | 2010-10-27 | 2017-01-31 | Compagnie Generale Des Establissements Michelin | Tire tread with apertures and a method for the manufacture of a tire tread with apertures |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2228876A1 (en) * | 1973-05-08 | 1974-12-06 | Goodyear Tire & Rubber |
-
1982
- 1982-05-21 CA CA000403563A patent/CA1215242A/en not_active Expired
- 1982-06-24 ZA ZA824506A patent/ZA824506B/en unknown
- 1982-06-25 DE DE198282105651T patent/DE73313T1/en active Pending
- 1982-06-25 AT AT82105651T patent/ATE24341T1/en not_active IP Right Cessation
- 1982-06-25 EP EP82105651A patent/EP0073313B1/en not_active Expired
- 1982-06-25 DE DE8282105651T patent/DE3274749D1/en not_active Expired
- 1982-06-29 AU AU85435/82A patent/AU557338B2/en not_active Expired
- 1982-07-21 MX MX193684A patent/MX171960B/en unknown
- 1982-07-27 JP JP57129728A patent/JPS5841951A/en active Granted
- 1982-07-27 BR BR8204384A patent/BR8204384A/en not_active IP Right Cessation
- 1982-07-27 DD DD82241982A patent/DD202320A5/en unknown
- 1982-07-27 ES ES514405A patent/ES8502176A1/en not_active Expired
- 1982-07-27 YU YU01632/82A patent/YU163282A/en unknown
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2228876A1 (en) * | 1973-05-08 | 1974-12-06 | Goodyear Tire & Rubber |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4474585A (en) * | 1983-05-31 | 1984-10-02 | Norton Company | Synthetic yarn-reinforced flexible webs stabilized against elongation, coated abrasive thereon, and process therefor |
DE3339305A1 (en) * | 1983-10-29 | 1985-05-23 | Saerbeck-Textil Wagener KG, 4401 Saerbeck | Flexible coating carrier produced by the stitch-bonding technique |
EP0267030A2 (en) * | 1986-11-05 | 1988-05-11 | E.I. Du Pont De Nemours And Company | Stitched polyethylene plexifilamentary sheet |
EP0267030A3 (en) * | 1986-11-05 | 1989-09-06 | E.I. Du Pont De Nemours And Company | Stitched polyethylene plexifilamentary sheet |
WO1994018367A1 (en) * | 1993-02-04 | 1994-08-18 | Minnesota Mining And Manufacturing Company | Stitchbonded articles and method of making same |
US5543004A (en) * | 1993-02-04 | 1996-08-06 | Minnesota Mining And Manufacturing Company | Stitchbonded articles and method of making same |
US8960248B2 (en) | 2009-10-15 | 2015-02-24 | Michelin Recherche Et Technique S.A. | Method and apparatus for multilayer shear band reinforcement |
US9493045B2 (en) | 2009-10-15 | 2016-11-15 | Michelin Recherche Et Technique S.A. | Method and apparatus for multilayer shear band reinforcement |
US9272576B2 (en) | 2010-03-12 | 2016-03-01 | Michelin Recherche Et Technique S.A. | Structurally supported, non-pneumatic wheel with continuous loop reinforcement assembly |
US9346317B2 (en) | 2010-12-29 | 2016-05-24 | Michelin Recherche Et Technique S.A. | Non-pneumatic tire with reinforcement band spacer and method of manufacturing same |
US9393835B2 (en) | 2010-12-29 | 2016-07-19 | General Electric Company | Annular structure having multiple reinforcement bands |
US9421820B2 (en) | 2010-12-29 | 2016-08-23 | Michelin Recherche Et Technique S.A. | Structurally supported non-pneumatic wheel with reinforcements and method of manufacture |
US9643453B2 (en) | 2010-12-29 | 2017-05-09 | Compagnie Generale Des Etablissements Michelin | Annular structure having multiple reinforcement bands |
Also Published As
Publication number | Publication date |
---|---|
JPH0220744B2 (en) | 1990-05-10 |
ZA824506B (en) | 1983-04-27 |
DE73313T1 (en) | 1983-09-29 |
DD202320A5 (en) | 1983-09-07 |
ES514405A0 (en) | 1984-12-16 |
CA1215242A (en) | 1986-12-16 |
MX171960B (en) | 1993-11-24 |
EP0073313B1 (en) | 1986-12-17 |
AU8543582A (en) | 1983-03-10 |
DE3274749D1 (en) | 1987-01-29 |
EP0073313A3 (en) | 1984-03-28 |
ATE24341T1 (en) | 1987-01-15 |
YU163282A (en) | 1985-03-20 |
ES8502176A1 (en) | 1984-12-16 |
BR8204384A (en) | 1983-07-19 |
AU557338B2 (en) | 1986-12-18 |
JPS5841951A (en) | 1983-03-11 |
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