GB2122542A - Method of reinforcing textile top fabrics and products thereby - Google Patents
Method of reinforcing textile top fabrics and products thereby Download PDFInfo
- Publication number
- GB2122542A GB2122542A GB08316443A GB8316443A GB2122542A GB 2122542 A GB2122542 A GB 2122542A GB 08316443 A GB08316443 A GB 08316443A GB 8316443 A GB8316443 A GB 8316443A GB 2122542 A GB2122542 A GB 2122542A
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- United Kingdom
- Prior art keywords
- net
- heat sealing
- sealing layer
- heat
- layer
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/10—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by a fibrous or filamentary layer reinforced with filaments
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- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
- A41D27/00—Details of garments or of their making
- A41D27/02—Linings
- A41D27/06—Stiffening-pieces
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- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
- A41D31/00—Materials specially adapted for outerwear
- A41D31/04—Materials specially adapted for outerwear characterised by special function or use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/32—Layered products comprising a layer of synthetic resin comprising polyolefins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/024—Woven fabric
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/02—Physical, chemical or physicochemical properties
- B32B7/027—Thermal properties
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- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
- D06M17/00—Producing multi-layer textile fabrics
- D06M17/04—Producing multi-layer textile fabrics by applying synthetic resins as adhesives
- D06M17/06—Polymers of vinyl compounds
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/08—Reinforcements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/38—Meshes, lattices or nets
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/31—Heat sealable
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/718—Weight, e.g. weight per square meter
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2309/00—Parameters for the laminating or treatment process; Apparatus details
- B32B2309/02—Temperature
Abstract
A method of reinforcing a textile top fabric by applying to a surface of the top fabric a heat fusible interlining comprising a thermoplastic polymeric resin net and fusing the net to the surface of the top fabric under heat and pressure characterised in that the heat fusible interlining is a multi-layered composite net comprising a heat sealing layer of polymeric resin and a substrate layer of different polymeric resin which has a melting temperature higher than that of the heat sealing layer said method being carried out at a temperature such that the heat sealing layer melts but the substrate layer does not melt and reinforced top fabrics made thereby are described. <IMAGE>
Description
1 GB 2 122 542A 1
SPECIFICATION
Method of reinforcing textile top fabrics and products made thereby The invention relates to a method of reinforcing a textile top fabric and reinforced top fabrics made thereby. A top fabric is the outer fabric layer of garments such as coats, shirts, dresses, blouses or parts thereof; curtain material, drapery headers, ties, upholstery and the like made of natural or synthetic fibres.
Save for certain so-called unconstructed garments, practically all apparel needs to have some areas or parts of the garment reinforced, in order to stiffen, support, stabilise or provide body to a textile top fabric. For example, shirt collars and cuffs require bodying linings. A jacket chest needs additional reinforcement so that it may be shaped. A waistband may need the firm support of a lining. Coat lapels have to be supported in order for them to hold their shape.
Until about 1940, all such reinforcing of textile materials was done with stiffened interlinings or buckrams, which were sewn into the garment at required stiffening points. This reinforcing was never of the whole garment but always of selected portions thereof. Dur- ing the 1 940s, a labour saving technique came into use whereby these reinforcements of interlining pieces were no longer being sewn into the garments but rather were being used on selected garment surfaces. The con- ventional interlinings gradually became obsolete and were replaced by fabrics coated with thermoplastic, thermofusible chemicals which were resistant to washing and/or dry cleaning. Thus, a new industry, that of fusible linings and interlinings was created.
The evolution and refinement of this new art is well documented in the literature. Representative of descriptions found in the prior art are the following: Stukenbrock, Bekleidung und Waesche, Heft 3, pages 142 to 153 (February 8, 1968); Report on Fusing in the Apparel Industry S.6 published by the Apparel Research Foundation Incorporated, Washington, D.C. (1970); Skoka et al., Hand- book of Fusible Interlinings (1980); and Chemical Principles of Heat Sealing Adhesives for Fusible Interlinings, Textilverdlung 6, pages 459- 468 (1971).
Thermofusible chemicals served a dual function, first as an adhesive and then as a bodying agent, the weight and volume of the chemicals making it possible to use lighter substrate cloths. The earliest thermofusible coatings were knife or roller coat continuous coatings such as plasticized cellulose acetate or mixtures of novolac and polyvinyl acetate. In the manufacture of shirts, polyvinyl chloride plastisol coatings were first used to be followed by polyethylene extruded films.
These continuous coatings in turn were re- placed by sintered powders (either polyethylene, polyvinyl acetate or terpolyamide) in order to make the resultant interlinings more air porous and flexible. Where it was desired to have a more regular pattern than provided by the randomly distributed sintered powders, various printing techniques were developed, i.e.; paste printing through rotary screens, usually a regular dot pattern ranging from 9 to 30 mesh screens, the chemicals employed being usually polyvinyl chloride plastisols, aqueous or solvent based dispersions or finely divided (under 80 Mu) polyethylene or polyamide powders. Polyethylene and polyamide powders (200 Mu) as well as polyester powders are now being applied to substrates by a dry "powder point coating" technique. The powders are knife coated into dot depressions which. have been engraved onto a metal print- ing roll. Controlled temperature heating of the roll causes the powders in the engravings to partially coalesce to form powder point agglomerates, which can then be transferred to preheated cloth substrates which are pressed against the printing roller. The process is completed when the substrate passes through a heating tunnel (infra red), which completes the compacting of the fusible dots onto the cloth.
British Patent Specification No. 1,088,555 describes a unique method of application of a regular pattern of closely spaced, thermofusible chemical dots of high density polyethylene onto a suitable substrate textile. Non-woven, plastic nets are produced by the bi-axial stressing of a thermoplastic material having a regular pattern of embossments on at least one surface according to the methods of British Patents Nos. 914,489 and 1,055,963.
These nets may be affixed to a cloth substrate by heat and pressure. Depending on the degree of heat and pressure, the net form may be retained or, more normally, the net strands may degenerate, retracting into the bosses and leaving a pattern of discrete closely spaced dots.
All of the foregoing examples of the prior art consist of two elements which comprise the fusible interlining. These two elements consist of the base cloth or substrate, which may be woven, non-woven, knitted, felt or even paper-like. The fibers employed in these base cloths are generally cotton, wool, rayon, synthetic fibers or blends thereof. The second element consists of a fusible chemical coating. In some cases double sided fusibles were used, wherein the substrate fabric was coated on both sides, i.e.; continuously coated, powder sintered, printed, etc. Furthermore the two elements of these prior art fusible interlinings are formed in separate operations for example by coating the thermofusible element on a preformed substrate element. As a consequence these fusible interlinings are relatively expensive to manufacture and use. This ap- 2 GB 2 122 542A 2 plies in particular to porous fusible interliners and thermofusible elements of which are made by special coating processes. It would therefore be advantageous to have a method of reinforcing textile top fabrics which employs a fusible interlining in which the thermofusible elements and substrate element are formed during the same process.
An alternative method was proposed for eliminating the base cloth element from these fusible interlinings in West German Deutsches Offen legu n gssch rift 25 52 878, 1974. This method comprises printing upon a selected portion of a top fabric requiring stabilization, an aqueous polyacrylic resin compound and a catalyst for its cross-linking. The machinery required is rather elaborate amd consists of a printing head, dryer and curing section. This elaborate machinery is required to cure the polyacrylic resin in-situ.
British Patent No. 1,427,281 discloses multi-layer nets which have two or more layers of different polymers. British Patent No. 1,427,281 discloses that the nets of that patent can be used as an adhesive in bonding together other materials under heat and pressure. When used as an adhesive the nets melt and either break up into globules or become weakened. British Patent No. 1,427,281 therefore does not suggest a method of heat bonding the multi-layer nets disclosed therein to a textile top fabric in such a manner as to provide an interlining reinforcement therefor.
The present invention obviates many difficulties of the prior art and economically makes possible reinforced, textile materials, including portions or select areas of garments. The possibility of using multilayered nets of different polymeric resins where one surface becomes fused as a replacement for conventional, fusible interlinings for clothing and textile applications has not been described in the prior art literature yet responds to the industry needs so cogently described by D. Miles in his article "Fusible Future" British Clothing Manufacturer May 1980. The present invention has many advantages, which will be appreciated by those skilled in the art, reading the following description.
The present invention provides a method of reinforcing a textile top fabric by applying to a surface of the top fabric a heat fusible interlining comprising a thermoplastic polymeric resin net and fusing the net to the surface of the top fabric under heat and pressure characterised in that the heat fusible interlining is a multi-layered composite net comprising a heat sealing layer of polymeric resin and a substrate layer of different polymeric resin which has a melting temperature higher than that of the heat sealing layer said method being carried out at a temperature such that heat sealing layer melts but the substrate layer does not melt.
The method of the invention, in conse- quence of reinforcing the top fabric, also stabilise the fabric. The net used in the invention can have more than two layers for example a net having an intermediate sub- strate layer between two outer heat sealing layers. However it is preferred that the net consists essentially of a substrate layer and a heat sealing layer. It is one of the considerable advantages of the method of this inven- tion that such effective reinforcement can occur using such simple materials.
The method of the invention can be used to make reinforced textile top fabrics. Accordingly in another aspect the invention provides a reinforced textile top fabric which has a heat fusible interlining comprising a thermoplastic polymeric resin net heat sealed to the surface of the fabric characterised in that the heat fusible interlining is a multi-layered composite net comprising a heat sealing layer of polym6ric resin and a substrate layer of different polymeric resin which has a melting temperature higher than that of the heat sealing layer said net having been heat sealed to the sur- face of the fabric at a temperature at which the heat sealing layer melts but the substrate layer does not melt.
The composite, multi-layered polymeric net used in the invention may be prepared by any one of a number of known techniques; see for example general methods of preparation described in British Patents Nos. 1,075,487; 1,427,281 and 1, 427,282. In such methods of preparation the net is formed by stretching a composite multi-layer embossed sheet which has at least two layers of different polymeric resin. The multi-layer embossed sheet can be conveniently made by coextrusion or lamination of the different polymeric resin layers. A suitable method of forming a laminated multilayer embossed sheet comprises bringing a polymer film in contact with a molten film of a different polymer during the embossing stage for example by feeding the films into the nip of the embossing rollers. In general therefore such nets may be prepared by the lamination or coextrusion of at least two different synthetic, polymeric resin layers in a net form. One layer forms a substrate layer and one the meltable, heat sealing layer for lamination to a textile fabric. Thus, the net employed in the invention will always include at least one heat sealing layer and a substrate layer which, although in theory is heat sealable because it is thermoplastic, has a melting point higher than that of the heat sealing layer so that it does not melt when the net is fused to the surface of the fabric and which therefore in practice behaves as a nonheat sealing layer.
The composite multi-layer nets, prepared by the methods described above, have net substrate and heat sealing layers which have been formed in the same process such heat fusible therefore will be more economical to prepare and use than comparable prior art t 3 GB 2 122 542A 3 fusible interlinings in which the substrate and heat sealing layers are formed separately. Fur thermore the nets prepared by such methods will have oriented strands which can provide a degree of resiliency to the reinforced textile fabric.
Suitable thermoplastics which may be used for the construction of a composite net used in the invention include the following syn thetic polymers which may be used advanta geously as a substrate layer, high density polyethylene, linear low density polyethylene, polypropylene and copolymers thereof, poly amides including polyetheramides and poly esteramides, co-polyamide, polyester, co-poly ester, polybutylene, polystyrene, polycarbo nate and the like and blends thereof. The heat sealing thermoplastic layer may be made of ethylene vinyl acetate co-polymers, saponified ethylene vinyl acetate copolymers, high den sity polyethylene, low and medium density polyethylene, linear low density polyethylene polypropylene and copolymers thereof, co and terpolyamides, co-polyester, polyure thane, ethylene ethyl acrylate copolymers and 90 the like and blends thereof. The co-extruded or laminated net materials are preferably so chosen that the substrate layer has a melting temperature of more than about BOT and the heat sealing layer a melting temperature of less than 1 50'C. The melting temperature of the substrate layer will be at least 1 OC higher desirably at least 20C and preferably at least 30'C higher than the melting temperature of the heat sealing layer. The heat sealing layer can suitably have a melting temperature of 80C to 1 50C and can preferably have a melting temperature of 11 OC to 1 35'C. The substrate layer can suitably have a melting temperature of 110 deg C to 250'C and can preferably have a melting temperature of 1 50C to 250'C. In order to lower the melting point of the heat sealing layer made out of high density polyethylene, for example, suit- able elastomers may be added.
Preferably the substrate layer comprises a polypropylene. Suitable polypropylenes include propylene homopolymers and copolymers of propylene with a minor amount (< 10% by weight) of ethylene which have a melting temperature of approx. 1 60C to 1 70C. Apt polypropylenes of this type are Profax 6524 (density 0.90 melt flow index 4) available from Hercules Inc. and Solvay HW 609 (density 0.90 melt flow index 18) available from Solvay et Cie SA.
Preferably the heat sealing layer comprises polyethylene. Suitable polyethylenes have melting temperature of 11 OC to 140'C.
Such polyethylenes include low density polyethylene made by the high pressure process, linear low density Polyethylene. An apt high density polyethylene and high density polyethylene. Preferred polyethylenes are linear low density polyethylene is known as Solvay A3180 (melting point approximately 135'C, density 0,96 melt flow index 18) available from Solvay et Cie SA. Apt linear low density polyethylenes include MW 1210 (melting temperature approximately 1 25'C, density 0.94 melt flow index 20) and MW 1350 (melting temperature approximately 11 5'C, density 0.92, melt flow index 20) available C.D.F. Chemie EP.
The use of linear low density polyethylene has been found to be a surprisingly effective heat sealing layer as particularly favourable processing is achieved and a highly favoured product results.
A preferred net for use in the invention has a substrate layer which comprises polypropylene and a heat sealing layer which comprises polyethylene which polyethylene is preferably linear low density polyethylene.
Where adhesion is not sufficient between the substrate layer and the heat sealing layer, an intermediary layer in the form of an adhesive layer may be required for improving adhesion. Suitable materials for the intermediary layer include, for example, ethylene co-polymers which contain one or a plurality of monomers with functional groups and polyolefines having grafted functional groups for example, CXA-resins (DuPont) ionomer resins, for example, Surlyn (DuPont) which is made of ethylene co-polymer with carboxyl group containing monomers, or Admer resins (Mitsui Petrochemicals) 4,hich are modified polyolefins. Other suitable materials include ethy- lene methyl acrylate copolymers, ethylene vinyl acetate copolymers and co- polyamides and co-polyesters. Such intermediary layers are not generally necessary in this invention and it is one of the considerable advantages of using the previously mentioned preferred polymers that an excellent product can be achieved without recourse to use of an intermediary layer.
Favoured composite multi-layered nets for use in the invention have a regular pattern of intersecting strands and openings which can provide a similar regular pattern of reinforcement of the textile top fabric. Preferred regular nets are nets which have at least one set of parallel strands. Such nets can have two or more sets of parallel strands which intersect to define openings of geometric shape which include shapes such as a square, rectangles, triangles, a rhombus, parallelograms trapezi- ums and hexagons. Preferred nets of this type have a first set of parallel strands which intersect at 90'C with a second set of parallel strands to define square or rectangular openings. In such nets the first set of parallel strands may extend in the machine direction of the net and the second set of parallel strands may extend in direction which is transverse to the machine direction to form a grid pattern net. Alternatively both sets of parallel strand may extend in directions which 4 GB 2 122 542A 4 are at an angle to the machine direction to form a diamond pattern net. The regular pattern nets described above may have thicker strands or a higher density of strands in one direction than in another direction to provide higher directional reinforcement of the textile top fabric.
The composite multi-layer nets used in the invention which comprise intersecting strands can suitably have 2 to 20 intersections per cm of strand and preferably 3 to 8 intersections per cm of strands in any one direction. In preferred nets of the invention which have a first and second set of parallel intersecting strands it is desirable that these nets have 2 to 20 intersections per cm of strand and preferably 3 to 8 intersections per cm of strand in the direction of both sets of strands.
The weight per unit area of composite multi-layered net used in the method of the invention can suitably be 5 to 50 g/sq.m and can more suitably be 10 to 40 g/sq.m. The weight per unit area of net used to reinforce a top fabric can be different for different types of top fabric. The preferred weight per unit area of net for reinforcing a light weight (1 50g/sq.m) shirting material, a medium weight (680 g/sq.m) suiting material and a heavy weight (850 g/sq.m) overcoat material, is 6 to 12 g/sq.m, 12 to 25 g/sq.m, and 22 to 34 g/sq.m respectively.
The weight of the heat sealing layer of the composite multi-layer net used in the invention will be sufficient to enable the net to be heat sealed to the chosen top fabric. The heat sealing layer can suitably be 10% to 50% by weight and can preferably be 25% to 45% by weight of the weight of the net. In nets which have an intermediate adhesive layer between the heat sealing layer and the substrate layer the intermediate adhesive layer can suitably be 1 % to 5% by weight of the total weight of the net. The heat sealing layer can have a colour, provided for example by the inclusion of coloured pigment in the polymeric resin, which is different from that of the substrate layer to aid identification of the heat sealing layer prior to heat sealing.
The thickness of the composite multi-layer nets can suitably be 25 micrometres to 500 micrometres and can preferably be 50 micrometres to 250 micrometres.
The process as described here is so versatile in choice of chemical components, c9nfiguration of the net, bulk and volume of the composite, as to permit virtually a wide range of textile and reinforcement. The net materials may be handled as conventional interlinings, i.e.; laid up, die cut and shaped as desired.
The net material may be fused to the textile material under heat and pressure, using existing plant lamination apparatus and techniques providing that the temperature used does not exceed the melting point of the substrate layer.
The invention will now be illustrated by reference to the following drawings.
Figure 1 is an isometric view of a reinforced top fabric of the invention.
Figure 2 is a cross-sectional, side elevation of the top fabric of the invention seen along lines 2-2 of Figure 1.
Figure 3 is an isometric view of a top fabric of the invention similar to that of Fig. 1 reinforced with an alternative composite multilayer net.
Referring now to the accompanying drawings, one can see in Fig. 1 an isometric view of a representative textile top material 8 which has been reinforced with a composite multilayered net material 10. The net material 10 as shown in Fig. 2 comprises a substrate layer 12 as described above and a heat sealing layer 14 as also described above. The woven fabric 8 comprises warp yarns 18 and weft yarns 20 which are bonded to the net 10 through heat sealing layer 14 by known lamination techniques, under heat and pressure. The composite multi-layered net (10) used to reinforced the woven textile top fabric (8) as shown in Fig. 3 has a first set of parallel strands (15) which intersect at 90 with a second set of parallel strands (16) to form a square grid pattern net.
It has been found that method of the invention provides reinforced textile top fabrics which have a better feel and handle than top fabrics reinforced with prior art fusible fabric interlinings which have a woven or knitted substrate layer. It has also been found that the use of composite nets with at least one set of oriented parallel strands can provide the reinforced top fabric with a degree of resiliency which makes the fabric highly suitable for use in waist bands. Furthermore, satisfactory reinforcement of the top fabrics can be obtained with low weights per unit area of composite multi-layered net as described hereinbefore. The invention therefore provides a method of reinforcing textile top fabrics which is -relatively simple and more economical than prior art fusible interlining reinforcing methods.
The invention is illustrated by the following examples. In examples 1 to 4 the muiti-layer nets of polymeric resin were laminated- to a variety of textile top fabrics, employing a Ducker press.
EXAMPLE 1
A co-extruded bilayer net having a substrate layer of polypropylene (melting point about 165C, density 0.90, melt index 14 and layer thickness 40 micrometres) and a heat-sealing layer of low pressure polyethylene (melting point about 130C, density 0. 96, melt index 40 and layer thickness 15 micrometres) is laminated to a shirt fabric made of 100% woven cotton with a weight of 150 g/sq.m under the following conditions:
GB2122542A 5 sealing pressure 300 Wa sealing temperature 145C sealing time 18 seconds The product pxhibits high resistance to delamination and stability in all directions. This reinforcement material can be used as a collar liner, cuff liner, jacket liner and front strapp- ing liner. The same material may also be used as a replacement for the build-up collar patch material as is used in conventional top fused European shirt construction.
EXAMPLE 2
A co-extruded bilayer net of a substrate material polypropylene (melting point about 165C, density 0.90, melt index 14 and layer thickness of 50 micrometres) and a heat seal- ing layer of terpolyamide material (nylon 6-6.6-12) melting point about 120'C and a layer thickness of 15 micrometres is laminated to garmet materials where reinforcement and stabilization is required as in for example chest fronts, lapels, etc.
sealing pressure 300 kPa sealing temperature 1 2W-1 WC sealing time 12 seconds EXAMPLE 3
Same as Example 2 substituting a suitable polyester material for the terpolyamide ma- terial.
EXAMPLE 4
A co-extruded tri-layer net A-B-A where the substrate material is polypropylene, melt- ing point about 165'C, density 0.90 and the heat sealing layers are top and bottom is medium density polethylene, melt index 36, said heat sealing layers being 10 micrometres thick, said product for use in automatic shirt neck banding collar making machines.
EXAMPLE 5
A composite two-layer net (40 g/sq.m) having layers formed by coextrusion consisting of substrate layer (32g/sq.m) of polypropylene (Solvay HW 609, melting temperature approx. 167'C, density 0.90, melt flow index 18) and a heat sealing layer (8 g/sq.m) of linear low density polyethylene (reference MW 1210, melting temperature approx. 125 C, density 0.94, melt flow index 20) was laminated to a worsted wollen fabric (680 g/sq.m) in a fusion press (ref M 8 Reliant Tooling Company Limited) under the following conditions:
The net used in this example had a first set of parallel strands (150 micrometres thick, 6 per cm) in the machine direction of the net and a second set of parallel strands (50 micrometres thich, 16 per cm) in a transverse direction which intersected at 90'. to give rectangular openings.
The reinforced woollen fabric of this example had good drape and handle was found to be highly suitable for overcoats.
EXAMPLE 6
A composite two layer net (20 g/sq.m) having layers formed by lamination consisting of a substrate layer (14 g/sq.m) of polypropylene (Solvay HW 609, melting temperature approx. 167'C, density 0.90, melt flow index 18) and a heat sealing layer (6 g/sq.m) of high density polyethylene (Solvay A3180 melting temperature approx. 135C, density 0. 96 melt flow index 18) was laminated to woven polyester shirting fabric (210 g/sq.m) in a fusion press in the same manner as Example 5 using a temperature of 140C to 145'C.
The net used in this example was 100 to 150 micrometres thick and had two sets of similar parallel strands (6 per cm) which intersect at 90' to give square openings.
The reinforced polyester fabric of this example had good drape and handle was found to be highly suitable for shirt cuffs.
EXAMPLE 7
A composite two layer net (20 g/sq.m) having layers formed by coextrusion consisting of a substrate layer (13 g/sq.m) of polypropylene (Profax 6524, melting temperature approx. 167C, density 0.90 melt flow index 4) and a heat sealing layer (7 g/sq.m) of linear low density polyethylene (ref. MW 1210, melting temperature approx. 125 C, density 0.94 rnelt flow index 20) was laminated to a woven suiting fabric (20% poly- ester, 80% wool, weight approx. 410 g/sq.m) in a fusion press in the same manner as Example 5.
The net used in this example was 100- 150 micrometres thick and had two sets of similar parallel strands (4 per cm) which intersect at 90' to give square openings.
The reinforced polyester/wool fabric of this example had good drape and handle and was found to be highly suitable for the fore-parts of jackets.
sealing pressure sealing temperature sealing time 4.2 Kgf/cm2 1WC to 14WC secs
Claims (13)
1. A method of reinforcing a textile top fabric by applying to a surface of the top fabric a heat fusible interlining comprising a thermoplastic polymeric resin net and fusing the net to the surface of the top fabric under heat and pressure characterised in that the heat fusible interlining is a multi-layered corn- posite net comprising a heat sealing layer of GB2122542A 6 polymeric resin and a substrate layer of different polymeric resin which has a melting temperature higher than that of the heat sealing layer said method being carried out at a temperature such that the heat sealing layer melts but the substrate layer does not melt.
2. A method as claimed in claim 1 in which the net comprises coextruded polymer layers.
3. A method as claimed in either claims 1 or 2 in which the net consists essentially of a substrate layer and a heat sealing layer.
4. A method as claimed in any of claims 1 to 3 in which the substrate layer has a melt- ing temperature of more than 80C and the heat sealing layer has a melting temperature of less than 1 50C.
5. A method as claimed in any of claims 1 to 4 in which the substrate layer has a melt- ing temperature of 1 50T to 250C and the heat sealing layer has a melting temperature of 11 OC to 135C.
6. A method as claimed in any of claims 1 to 5 in which the substrate layer comprises polypropylene and the heat sealing layer comprises polyethylene.
7. A method as claimed in any of claims 1 to 6 in which the heat sealing layer comprises a linear low density polyethylene.
8. A method as claimed in any of claims 1 to 7 in which the net has a weight per unit area of 10 to 40 g/sq.m.
9. A method as claimed in any of claims 1 to 8 in which the heat sealing layer comprises 25% to 40% by weight of the net.
10. A method as claimed in any of claims 1 to 9 in which the net has a regular pattern of intersecting strands and openings and and comprises a first set of parallel strands which intersect with a second set of parallel strands to give 3 to 8 per cm intersections per strand in the direction of both sets of strands.
11. A method as claimed in any of claims 1 to 10 in which the heat sealing layer has a colour which is different from that of the substrate layer to aid identification of the heat sealing layer.
12. A reinforced textile top fabric produced by a method as claimed in any of claims 1 to 11.
13. A reinforced textile top fabric which has a heat fusible interlining comprising a thermoplastic polymeric resin net heat sealed to the surface of the fabric characterised in that the heat fusible interlining is a multilayered composite net comprising a heat sealing layer of polymeric resin and a substrate layer of a different polymeric resin which has a melting temperature higher than that of the heat sealing layer said net having been heat sealed to the surface of the fabric at a temperature at which the heat sealing layer melts but the substrate layer does not melt.
Printed for Her Majesty's Stationery Office by Burgess Et Son (Abingdon) Ltd.-1 984. Published at The Patent Office, 25 Southampton Buildings, London, WC2A 1AY, from which copies may be obtained.
k& R Ili
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US38971582A | 1982-06-18 | 1982-06-18 |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8316443D0 GB8316443D0 (en) | 1983-07-20 |
GB2122542A true GB2122542A (en) | 1984-01-18 |
GB2122542B GB2122542B (en) | 1985-12-18 |
Family
ID=23539420
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08316443A Expired GB2122542B (en) | 1982-06-18 | 1983-06-16 | Method of reinforcing textile top fabrics and products thereby |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP0097496B1 (en) |
JP (1) | JPS5931114A (en) |
AU (1) | AU1563783A (en) |
DE (1) | DE3371311D1 (en) |
GB (1) | GB2122542B (en) |
ZA (1) | ZA834228B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101120136B (en) * | 2005-02-12 | 2012-06-13 | 卡尔弗罗伊登柏格两合公司 | Textile fabric with improved finish, production and use thereof |
CN103889695A (en) * | 2011-10-05 | 2014-06-25 | 3M创新有限公司 | Three-dimensional polymeric strand netting, dies, and methods of making the same |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3330866A1 (en) * | 1983-08-26 | 1985-03-14 | Kufner Textilwerke GmbH, 8000 München | UPPER FABRIC FOR CLOTHING AND PRODUCTION PROCESS AND TRANSFER UNIT THEREFOR |
DE3407005A1 (en) * | 1983-09-26 | 1985-04-04 | Bayer Ag, 5090 Leverkusen | HYDROXYETHYLAZOLYL OXIME DERIVATES |
TW252163B (en) * | 1994-05-10 | 1995-07-21 | At & T Corp | Woven plastic fiber cloth having fused stiffening areas |
US5885686A (en) * | 1994-08-26 | 1999-03-23 | Leucadia, Inc. | Bicomponent elastomeric netting |
FR2738770B1 (en) * | 1995-09-15 | 1997-10-24 | Nortene Technologies | PLASTIC TABLECLOTH MATERIAL PARTICULARLY FOR THE PRODUCTION OF OCCULTATION SCREENS FOR GARDENS, TERRACES AND BALCONIES |
US6204207B1 (en) * | 1996-08-01 | 2001-03-20 | Leucadia, Inc. | Extruded netting exhibiting stretch and bonding |
DE102004012269A1 (en) * | 2004-03-13 | 2005-09-29 | Carl Freudenberg Kg | Textile fabrics with a grid-shaped coating, their manufacture and use |
CN103842164A (en) * | 2011-08-22 | 2014-06-04 | 3M创新有限公司 | Netting, arrays, and dies, and methods of making the same |
US20150079337A1 (en) * | 2012-03-26 | 2015-03-19 | 3M Innovative Properties Company | Films comprising an array of openings and methods of making the same |
KR20150127227A (en) | 2013-03-13 | 2015-11-16 | 쓰리엠 이노베이티브 프로퍼티즈 캄파니 | Nettings, dies, and methods of making the same |
KR20160127058A (en) | 2014-02-28 | 2016-11-02 | 쓰리엠 이노베이티브 프로퍼티즈 컴파니 | Filtration medium including polymeric netting of ribbons and strands |
WO2015130942A1 (en) | 2014-02-28 | 2015-09-03 | 3M Innovative Properties Company | Polymeric netting of strands and first and second ribbons and methods of making the same |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1427282A (en) * | 1973-08-13 | 1976-03-10 | Hercules Inc | Elastically extensible network structures |
GB1427281A (en) * | 1973-01-16 | 1976-03-10 | Hercules Inc | Network structures |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1088555A (en) * | 1964-08-17 | 1967-10-25 | Smith & Nephew Plastics | Improvements in and relating to laminates and methods for their manufacture |
DE2214236C3 (en) * | 1972-03-23 | 1983-11-10 | Kufner Textilwerke KG, 8000 München | Grid-shaped coating of heat-seal adhesives on flat structures |
JPS49116373A (en) * | 1973-03-08 | 1974-11-07 | ||
DE2351405C3 (en) * | 1973-10-12 | 1979-05-17 | Kufner Textilwerke Kg, 8000 Muenchen | Process for the production of a one-sided heat-sealable fleece |
GB1528383A (en) * | 1974-12-02 | 1978-10-11 | Codama Holding Sa | Method and apparatus for locally reinforcing a top cloth piece for a garment |
DE2741793A1 (en) * | 1977-09-16 | 1979-03-29 | Nino Ag | HEAT SEALABLE TEXTILE INNER FABRIC AND METHOD FOR MANUFACTURING THESE |
-
1983
- 1983-06-09 AU AU15637/83A patent/AU1563783A/en not_active Abandoned
- 1983-06-09 ZA ZA834228A patent/ZA834228B/en unknown
- 1983-06-16 EP EP83303499A patent/EP0097496B1/en not_active Expired
- 1983-06-16 DE DE8383303499T patent/DE3371311D1/en not_active Expired
- 1983-06-16 GB GB08316443A patent/GB2122542B/en not_active Expired
- 1983-06-17 JP JP58110041A patent/JPS5931114A/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1427281A (en) * | 1973-01-16 | 1976-03-10 | Hercules Inc | Network structures |
GB1427282A (en) * | 1973-08-13 | 1976-03-10 | Hercules Inc | Elastically extensible network structures |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101120136B (en) * | 2005-02-12 | 2012-06-13 | 卡尔弗罗伊登柏格两合公司 | Textile fabric with improved finish, production and use thereof |
CN103889695A (en) * | 2011-10-05 | 2014-06-25 | 3M创新有限公司 | Three-dimensional polymeric strand netting, dies, and methods of making the same |
Also Published As
Publication number | Publication date |
---|---|
GB8316443D0 (en) | 1983-07-20 |
EP0097496A3 (en) | 1984-12-27 |
AU1563783A (en) | 1983-12-22 |
GB2122542B (en) | 1985-12-18 |
JPS5931114A (en) | 1984-02-20 |
ZA834228B (en) | 1984-06-27 |
DE3371311D1 (en) | 1987-06-11 |
EP0097496B1 (en) | 1987-05-06 |
EP0097496A2 (en) | 1984-01-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19950616 |