US4919738A
Expired / Lapsed
US
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Dynamic mechanical bonding method and apparatus
Assignee: Procter and Gamble Co
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Filing: 1989-05-25
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Granted: 1990-04-24
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Expires: 2009-05-25
Abstract
Abstract A method of and apparatus for dynamically mechanically bonding together a plurality of laminae, at least one of which comprises thermoplastic material: for example, polyethylene. In one aspect of the invention the laminae are forwarded in face to face relation through a pressure biased nip between a patterned nip defining member and an opposing nip defining member (e.g., a relief patterned cylinder and an anvil cylinder) which members are independently driven to maintain a predetermined surface velocity differential between them. In another aspect of the invention which is particularly useful at intermediate and higher line velocities-preferably for line velocities of about 300 feet or more per minute and, more preferably, for line speeds of about 450 feet or more per minute-the nip defining members may be operated with equal surface velocities. In each of these aspects of the invention, the members may be biased towards each other to provide a predetermined pattern-element-psi loading; and, additionally, they may be independently heated to provide each with an elevated surface temperature which is, preferably, in a predetermined range below the melt temperature of the thermoplastic lamina disposed closet to or in contact with each respective nip defining member as the laminae are forwarded through the nip.
Inventors
- 👤 W. Kenneth Ball
- 👤 David J. K. Goulait
- 👤 James E. Zorb
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 11:16
CPC Classifications
B; B29; B29C; B29C66/00; B29C66/01; B29C66/05; B29C66/20; B29C66/21; A; A61; A61F; A61F13/00; A61F13/15; A61F13/56; A61F13/62; B29C65/00; B29C65/02; B29C65/18; B29C66/10; B29C66/11; B29C66/112; B29C66/1122; B29C66/40; B29C66/41; B29C66/43; B29C66/70; B29C66/73; B29C66/739; B29C66/7392; B29C66/80; B29C66/81; B29C66/814; B29C66/8141; B29C66/81433; B29C66/82; B29C66/824; B29C66/8242; B29C66/83; B29C66/834; B29C66/8341; B29C66/83411; B29C66/8351; B29C66/83511; B29C66/90; B29C66/91; B29C66/914; B29C66/9141; B29C66/91421; B29C66/919; B29C66/9192; B29C66/91921; B29C66/91931; B29C66/91935; B29C66/92; B29C66/924; B29C66/9241; B29C66/929; B29C66/93; B29C66/934; B29C66/93411; B29C66/93431; B29C66/93451; B29C66/939; B29C65/82; B29C65/8207; B29C65/8223; B29C66/344; B29C66/71; B29C66/72; B29C66/729; B29C66/7294; B29C66/812; B29C66/8122; B29C66/91423; B29K; B29K2023/00; B29K2023/04; B29K2023/06; B29K2905/00; B29K2905/08; B29K2905/12; B29L; B29L2024/00; B29L2031/00; B29L2031/48; B29L2031/4871; B29L2031/4878; Y; Y10; Y10T; Y10T156/00; Y10T156/17; Y10T156/1702; Y10T156/1712; Y10T156/1737; Y10T156/1741
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
106 words
A method of dynamically bonding plural lamina together, at least one of which laminae comprises thermoplastic material, said method comprising the steps of: forwarding said laminae at a velocity of about 300 to about 600 per feet minute, with portions thereof in face to face relation, through a pressure biased nip between a relief patterned nip defining member having pattern element segments, and a nip defining anvil member; biasing said nip defining members towards each other with a predetermined pattern-element loading that is between about 68,000 psi and about 113,000 psi; and sufficiently heating each said nip defining member to enable dynamically thermobonding said laminae together.
Claim 2
Independent Claim
106 words
A method of dynamically bonding plural lamina together, at least one of which laminae comprises thermoplastic material, said method comprising the steps of: forwarding said laminae at a velocity of about 300 to about 600 per feet minute, with portions thereof in face to face relation, through a pressure biased nip between a relief patterned nip defining member having pattern element segments, and a nip defining anvil member; biasing said nip defining members towards each other with a predetermined pattern-element loading that is between about 68,000 psi and about 113,000 psi; and sufficiently heating each said nip defining member to enable dynamically thermobonding said laminae together.
Claim 3
Dependent Claim
21 words
The method of claim 1 wherein said laminae are forwarded at a velocity of about 450 feet per minute or greater.
Claim 4
Dependent Claim
52 words
The method of claim 1 wherein the step of heating comprises heating each said nip defining member to provide a surface temperature that will precipitate relatively high strength bonds, said temperature being inversely related to line velocity and directly related to the melt temperature of the thermoplastic lamina disposed most adjacent thereto.
Claim 5
Dependent Claim
71 words
The method of claim 1 wherein said step of heating of each said nip defining member having a direct contacting relation with a thermoplastic lamina being limited to effecting a surface temperature that is sufficiently below the melt temperature of the thermoplastic lamina in direct contacting relation therewith to substantially preclude the thermoplastic from melting or sticking to the nip defining members in the event the nip defining members are stopped.
Claim 6
Dependent Claim
23 words
The method of claim 1 wherein said pattern element segments are discrete projections having tip surface areas greater than about 0.002 square inches.
Claim 7
Dependent Claim
24 words
The method of claim 1 wherein said pattern element segments are discrete projections having tip surface areas of about 0.004 square inches or greater.
Claim 8
Dependent Claim
19 words
The method of claim 1 or 2 wherein said nip defining members are driven at substantially equal surface velocities.
Claim 9
Dependent Claim
22 words
The method of claim 1 or 2 wherein said nip defining members are driven at differential surface velocities within a predetermined range.
Claim 10
Dependent Claim
74 words
The method of claim 1 wherein: said nip defining members are biased towards each other with a predetermined pattern-element loading that is approximated by the formula: PEL=-0.15LV+158, where PEL is the pattern element loading in kpsi, LV is the line velocity in feet per minute and 300≦LV≦600; and each said nip defining member is sufficiently heated to a temperature less than the melting temperature of the laminae to enable dynamically thermobonding said laminae together.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1993-04-23 | 1993-10-23 | 1994-04-24 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-04-23 | 1997-10-23 | 1998-04-24 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-04-23 | 2001-10-23 | 2002-04-24 | $7700.00 | Window Closed / Lapsed |