Process of manufacturing a refastenable mechanical fastening system

• US 5,180,534 A
• Filed: 12/21/1990
• Issued: 01/19/1993
• Est. Priority Date: 12/21/1990
• Status: Expired due to Term

• Current Assignee: The Procter & Gamble Company
• Original Assignee: The Procter & Gamble Company
• Inventors: Goulait, David J. K., Thomas, Dennis A., Cox, Robert G. Jr.
• Primary Examiner(s): Woo, Jay H.
• Assistant Examiner(s): Davis, Robert B.
• Application Number:
  US07/632,283
• Time in Patent Office: 760 Days
• Field of Search: 264/164, 264/145, 264/175, 425/378.1, 425/DIG. 34
• US Class Current: 264/145
• CPC Class Codes: A44B 18/0049 obtained by moulding processes compression moulding or articles of indefinite length characterised by the shape of the surface B29C43/222; screen moulding B29C67/08
• CPC Class Codes: A61F 13/625 characterised by the hook
• CPC Class Codes: B29C 43/222 characterised by the shape of the surface
• CPC Class Codes: B29L 2031/729 Hook and loop-type fasteners

Abstract

The invention is a refastenable mechanical fastening system, made of free formed prongs joined to a substrate. The prongs taper and are nonperpendicularly oriented relative to the plane of the substrate. The prongs also have an azimuthal angle relative to the machine direction of the substrate. Each prong has an engaging means projecting laterally from the periphery of the prong. The free formed prongs are manufactured by the process of depositing liquid material onto a moving substrate, stretching the liquid material in a direction parallel to the plane of the substrate, severing the stretched material to form the distal end and engaging means of the prong, and imparting an azimuthal angle to the prong. The advantageous usage of the fastening system in an article of manufacture, such as a disposable absorbant garment, specifically a diaper.

Claims

1. A method for manufacturing a fastening material having prongs, the method comprising the steps of:

providing a thermally sensitive material;

heating said thermally sensitive material to at least the melting point;

providing a substrate transported in a first direction;

depositing discrete amounts of said thermally sensitive material on said transported substrate;

stretching said discrete amounts of thermally sensitive material in a direction having a vector component parallel to the plane of said substrate;

severing said stretched thermally sensitive material to form prongs having shanks, each of said shanks having a distal end and engaging means thereon; and

imparting an azimuthal angle of between about 20 degrees to about 160 degrees to said shanks of said prongs.

2. The method according to claim 1 wherein said step of imparting an azimuthal angle to said shanks comprises biasing said prongs.

3. The method of claim 2 wherein said step of imparting an azimuthal angle comprises biasing said prongs while they are newly formed and not yet solidifed.

4. The method of claim 2 wherein said step of biasing said prongs comprises applying a fluid pressure differential in a direction having a vector component perpendicular to said first direction to at least a portion of said prongs.

5. The method of claim 4 wherein said step of applying a fluid pressure differential comprises flowing a gas from a high-pressure area to a low-pressure area across the substrate.

6. The method of claim 5 wherein said step of flowing a gas across the substrate comprises providing a substantially laminar flow of gas across the substrate.

7. The method of claim 6 wherein said step of providing a substantially laminar flow of gas across the substrate comprises flowing a gas through at least one flow amplifier.

8. The method of claim 6 wherein said step of providing a substantially laminar flow of gas across the substrate comprises using a first and a second flow amplifier such that the discharge of said first flow amplifier is drawn into the suction of said second flow amplifier.

9. The method of claim 7 or 8 wherein said pressure differential is about 1 psi to about 10 psi.

10. The method according to claim 2 wherein said step of biasing said prongs comprises subjecting said prongs to gravitational forces in a direction having a vector component perpendicular to said first direction, such that an azimuthal angle of between about 20 degrees to about 160 degrees is imparted to said shanks of said prongs.

11. The method of claim 10 wherein said step of subjecting said prongs to gravitational forces in a direction having a vector component perpendicular to said first direction, comprises vertically inclining said substrate relative to the horizontal.

12. The method of claim 11 wherein said step of subjecting said prongs to gravitational forces in a direction having a vector component perpendicular to said first direction, comprises vertically inclining said substrate at least about 15°

relative to the horizontal.

13. The method of claim 11 wherein said step of subjecting said prongs to gravitational forces in a direction having a vector component perpendicular to said first direction, comprises vertically including said substrate to least about 30°

relative to the horizontal.

14. The method of claim 2 wherein said step of biasing said prongs comprises both applying a fluid pressure differential to said prongs and subjecting said prongs to gravitational forces in a direction having a vector component perpendicular to said first direction.

15. The method of claim 1 wherein said step of imparting an azimuthal angle comprises imparting an azimuthal angle of between about 45°

to about 135°

to said shanks of said prongs.

16. The method of claim 1 wherein said step of imparting an azimuthal angle comprises imparting an azimuthal angle of between about 60°

to about 120°

to said shanks of said prongs.