Selective-area fusion of non-woven fabrics

• US 4,265,954 A
• Filed: 04/11/1978
• Issued: 05/05/1981
• Est. Priority Date: 04/11/1978
• Status: Expired due to Term

• Current Assignee: Amoco Corporation (BP PLC)
• Original Assignee: Phillips Petroleum Company (ConocoPhillips)
• Inventors: Romanek, Gerald A.
• Primary Examiner(s): Bell, James J.
• Application Number:
  US05/895,338
• Time in Patent Office: 1,120 Days
• Field of Search: 428/85, 428/90, 428/95, 428/131, 428/132, 428/137, 428/195, 428/211, 428/288, 428/296, 428/198, 428/195, 156/72, 156/181, 156/272, 156/273, 156/274, 156/296, 156/305, 156/308, 156/290, 264/22, 264/25, 264/129, 264/132, 264/327, 427/160, 427/288, 118/641
• US Class Current: 428/85
• CPC Class Codes: B29C 2035/0822 using IR radiation
• CPC Class Codes: B29C 2035/0855 using microwave
• CPC Class Codes: B29C 65/02 by heating, with or without pressure
• CPC Class Codes: B29C 65/10 using hot gases (e.g. combustion gases) or flames coming in contact with at least one of the parts to be joined
• CPC Class Codes: B29C 65/14 using wave energy , i.e. electromagnetic radiation, or particle radiation using mechanical waves B29C65/06; using ultrasonic waves B29C65/08; pressing means transparent to electromagnetic radiation B29C66/81267
• CPC Class Codes: B29C 65/1412 Infrared [IR] radiation
• CPC Class Codes: B29C 65/1425 Microwave radiation
• CPC Class Codes: B29C 65/1445 heating both sides of the joint
• CPC Class Codes: B29C 65/1464 making use of several radiators
• CPC Class Codes: B29C 65/1483 coated on the article
• CPC Class Codes: B29C 65/1496 making use of masks B29C65/1696 takes precedence
• CPC Class Codes: B29C 66/02 Preparation of the material, in the area to be joined, prior to joining or welding B29C66/32 takes precedence
• CPC Class Codes: B29C 66/1122 Single lap to lap joints, i.e. overlap joints B29C66/45, B29C66/472, B29C66/52272 take precedence
• CPC Class Codes: B29C 66/21 said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot welding
• CPC Class Codes: B29C 66/232 said joint lines being multiple and parallel, i.e. the joint being formed by several parallel joint lines
• CPC Class Codes: B29C 66/234 said joint lines being in the form of tessellations
• CPC Class Codes: B29C 66/45 Joining of substantially the whole surface of the articles methods or apparatus for laminating B32B37/00
• CPC Class Codes: B29C 66/71 characterised by the composition of the plastics material of the parts to be joined welding bar compositions B29C65/125
• CPC Class Codes: B29C 66/73711 oriented
• CPC Class Codes: B29C 66/73712 mono-axially
• CPC Class Codes: B29C 66/7392 : characterised by the material of at least one of the parts being a thermoplastic
• CPC Class Codes: B29C 66/73921 : characterised by the materials of both parts being thermoplastics
• CPC Class Codes: B29C 66/83413 : cooperating rollers, cylinders or drums
• CPC Class Codes: B29C 66/83415 : the contact angle between said rollers, cylinders or drums and said parts to be joined being a non-zero angle B29C66/83433 takes precedence
• CPC Class Codes: B29C 66/83417 : said rollers, cylinders or drums being hollow
• CPC Class Codes: B29C 66/83421 : band or belt types B29C66/83431 takes precedence
• CPC Class Codes: B29C 66/83431 : rollers, cylinders or drums cooperating with bands or belts
• CPC Class Codes: B29C 66/83511 : jaws mounted on rollers, cylinders or drums
• CPC Class Codes: B29C 66/83521 : jaws mounted on bands or belts
• CPC Class Codes: B29K 2067/00 : Use of polyesters or derivatives thereof, as moulding material
• CPC Class Codes: B29K 2075/00 : Use of PU, i.e. polyureas or polyurethanes or derivatives thereof, as moulding material
• CPC Class Codes: B29K 2077/00 : Use of PA, i.e. polyamides, e.g. polyesteramides or derivatives thereof, as moulding material
• CPC Class Codes: B29K 2105/0854 : in the form of a non-woven mat
• CPC Class Codes: D04H 1/54 : by welding together the fibres, e.g. by partially melting or dissolving in combination with needling D04H1/485
• CPC Class Codes: Y10T 156/1089 : of discrete laminae to single face of additional lamina
• CPC Class Codes: Y10T 428/23979 : Particular backing structure or composition
• CPC Class Codes: Y10T 428/24273 : including aperture
• CPC Class Codes: Y10T 428/24802 : Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]
• CPC Class Codes: Y10T 442/69 : Autogenously bonded nonwoven fabric

Abstract

A non-woven sheet or web of fibers, containing at least some thermoplastic fibers, is fused to consolidate the fibers, bond another sheet of material thereto, perforate the sheet or bind tufting fibers therein by heating the sheet to a temperature and for a time sufficient to fuse at least some of the fibers in preselected areas of the sheet while simultaneously blocking heat transmission to the non-selected areas, or by pretreating patterned areas of the sheet to increase or decrease the heat-absorptivity of the patterned areas relative to the remainder of the sheet and thereafter heating the sheet. Improved non-woven fabrics, consolidated in preselected areas, non-woven fabrics bonded to another sheet material in preselected areas, non-woven fabrics perforated in predetermined areas and non-woven fabric substrates firmly holding tufting materials in preselected areas, are also produced.

Claims

1. A method for physically fusing preselected areas by the application of heat while leaving unfused adjacent, nonselected areas of an extended, flat body of nonwoven, fibrous material, containing at least some thermoplastic fibers;

comprising, exposing said fibrous material to heat, from a source of radiant energy adapted to produce heat in said body of fibrous material, spaced from said body of fibrous material and radiating over an area of said body of fibrous material including both said preselected and said nonselected areas, at a temperature and for a time at least sufficient to fuse at least some of said thermoplastic fibers and concentrating the heat from said source of energy in said preselected areas by (a) modifying the heat absorptivity of said preselected areas of said body of fibrous material, (b) modifying the heat absorptivity of said nonselected areas of said body of fibrous material, (c) interposing between said body of fibrous material and said source of energy a mask having areas of increased radiant energy transmission corresponding to said preselected areas of said body of fibrous material, (d) interposing between said body of fibrous material and said source of energy a mask having areas of decreased radiant energy transmission corresponding to said nonselected areas of said body of fibrous material or (e) any combination of at least two of (a), (b), (c) and (d).

2. A method in accordance with claim 1 wherein the source of energy is an infrared source.

3. A method in accordance with claim 1 wherein the source of energy is a dielectric source.

4. A method in accordance with claim 1 wherein the source of energy is a microwave source.

5. A method in accordance with claim 1 wherein the heat is concentrated in the preselected areas by modifying the body of fibrous materials to render said body of fibrous materials more heat absorptive in said preselected areas than in the nonselected areas of said body of fibrous materials.

6. A method in accordance with claim 5 wherein the heat absorptivity of the preselected areas is increased by applying a heat absorbing coating in said preselected areas.

7. A method in accordance with claim 6 wherein the heat absorbing coating is an oleaginous material.

8. A method in accordance with claim 5 wherein the heat absorptivity of the preselected areas is increased by densifying the fibrous material in said preselected areas.

9. A method in accordance with claim 5 wherein the fibrous material is densified in the preselected areas by subjecting said preselected areas to pressure prior to exposing said fibrous material to the source of energy.

10. A method in accordance with claim 1 wherein the heat is concentrated in the preselected areas by modifying the body of fibrous material to render said body of fibrous materials less heat absorptive in the nonselected areas than in the preselected areas of said body of fibrous materials.

11. A method in accordance with claim 10 wherein the heat absorptivity of the nonselected areas is decreased by applying a coating of reduced heat absorptivity in said nonselected areas.

12. A method in accordance with claim 11 wherein the coating of reduced heat absorptivity is an aqueous solution.

13. A method in accordance with claim 1 wherein the heat is concentrated in the preselected areas by interposing between the body of fibrous material and the source of energy a mask having areas, corresponding to said preselected areas of said body of fibrous material modified to render said mask more transparent to radiant energy than the remaining areas thereof.

14. A method in accordance with claim 1 wherein the heat is concentrated in the preselected areas by interposing between the body of fibrous material and the source of energy a mask having areas, corresponding to the nonselected areas of said body of fibrous material, modified to render said mask less transparent to radiant energy than the remaining areas thereof.

15. A method in accordance with claim 1 wherein the heat is concentrated in the preselected areas by interposing between the body of fibrous material and the source of energy a mask relatively impervious to the transmission of radiant energy in the areas of said body of fibrous material corresponding to the nonselected areas and cut out in a configuration corresponding to said preselected areas of said body of fibrous material.

16. A method in accordance with claim 15 wherein the mask is in the form of the outer surface of at least rotatable roller and the body of fibrous material is continuously drawn over the surface of said roller.

17. A method in accordance with claim 16 wherein the source of energy is a stationary source mounted within the roller.

18. A method in accordance with claim 16 wherein the mask is in the form of two spaced, rotatable rollers, the source of energy is a source of energy within each of said rollers and the body of fibrous material is continuously drawn over the surfaces of said rollers in an S-type configuration to thereby expose both sides of said body of fibrous material to said source of energy.

19. A method in accordance with claim 15 wherein the mask is a moving belt and the body of fibrous material is maintained in contact with and carried along with said belt.

20. A method in accordance with claim 1 wherein the temperature and time of exposure of the body of fibrous material to the source of energy is sufficient to form a plurality of perforations in at least part of the preselected areas of said body of fibrous material.

21. A method in accordance with claim 1 wherein the temperature and time of exposure of the body of fibrous material to the source of energy is sufficient to form perforations in the entire preselected areas of said body of fibrous material.

22. A method in accordance with claim 1 wherein at least one second, extended, flat body of material is placed in contact with the body of fibrous material and the temperature and time of exposure to the source of energy is sufficient to bond said body of fibrous material to said second body of material in the preselected areas.

23. A method in accordance with claim 22 wherein the second body of material is paper.

24. A method in accordance with claim 22 wherein the second body of material is aluminum foil.

25. A method in accordance with claim 22 wherein the second body of material is a second body of nonwoven fibrous material.

26. A method in accordance with claim 1 wherein the body of fibrous material is prevented from shrinking during exposure to the source of energy, fibrous tufting materials are associated with said body of fibrous material and the preselected areas are selected to generally correspond to the points of contact of said tufting materials with said body of fibrous material.

27. A method in accordance with claim 1 wherein the body of fibrous material is permitted to shrink during exposure to the source of energy, fibrous tufting materials are associated with said body of fibrous material and the preselected areas are selected to generally correspond to the points of contact of said tufting materials with said body of fibrous material.

28. A method in accordance with claim 27 wherein the body of fibrous material is permitted to shrink in direction parallel to the major axis of the fibers of said body of fibrous material.

29. An extended, flat body of nonwoven, fibrous material, containing at least some thermoplastic fibers and having tufting materials combined in at least some preselected areas of said body of fibrous material, by exposing said fibrous material to heat, from a source of radiant energy adapted to produce heat in said body of fibrous material, spaced from said body of fibrous material and radiating over an area of said body of fibrous material including both said preselected areas and adjacent, nonselected areas of said body of fibrous material, at a temperature and for a time sufficient to fuse at least some of said thermoplastic fibers and concentrating the heat from said source of energy in said preselected areas of said body of fibrous material, to fuse at least some of said thermoplastic fibers in said preselected areas where said tufting materials contact said body of fibrous material.

30. A nonwoven, fibrous material in accordance with claim 29 wherein the body of fibrous material is prevented from shrinking during exposure to the source of energy.

31. A nonwoven, fibrous material in accordance with claim 29 wherein the body of fibrous material is permitted to shrink during exposure to the source of energy.

32. A nonwoven, fibrous material in accordance with claim 31 wherein the body of fibrous material is permitted to shrink in a direction parallel to the major axis of the fibers of said body of fibrous material.