US4224092A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for making all-plastic heat-sealable container
Assignee: Champion International Corp
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Filing: 1978-08-10
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Granted: 1980-09-23
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Expires: 1998-08-10
Abstract
Abstract The invention provides a dynamic system for heat-sealing an all-plastic material in a continuous process at high speed. The invention includes an all-plastic heat-sealable container material comprising a multiple-layer composite, in sheet form, including a core layer and at least one outer layer on one side thereof. The layers preferably comprise thermoplastic material, the core layer material having a higher softening point than the outer layer material. The composite sheet is conveyed through a converting, side-seaming or other apparatus at high speed, the system being tuned to dynamically heat the outer layers to a molten state for heat sealing, while the core does not soften but remains undistorted. The core is thus thermally insensitive to heat at speeds used in side-seaming the composite, and as such it supports and maintains the structure of the sealing outer layers on its exterior while they are in a molten condition.
Inventors
- 👤 Kenneth P. Thompson
- 👤 Richard C. Ihde
- 👤 Clarence E. Roth
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 17:04
CPC Classifications
B; B32; B32B; B32B27/00; B32B27/06; B32B27/08; B29; B29C; B29C65/00; B29C65/02; B29C65/10; B29C65/106; B29C66/00; B29C66/01; B29C66/05; B29C66/10; B29C66/11; B29C66/112; B29C66/1122; B29C66/40; B29C66/41; B29C66/43; B29C66/431; B29C66/4312; B29C66/43121; B29C66/43122; B29C66/432; B29C66/4322; B29C66/4326; B29C66/70; B29C66/72; B29C66/723; B29C66/73; B29C66/731; B29C66/7311; B29C66/7313; B29C66/739; B29C66/7392; B29C66/73921; B29C66/80; B29C66/83; B29C66/836; B31; B31B; B31B50/00; B31B50/60; B31B50/64; B32B1/00; B32B1/08; B32B27/32; B32B38/00; B32B38/0036; B65; B65D; B65D5/00; B65D5/42; B65D5/56; B65D5/563; B29C66/71; B29C66/7232; B29C66/72327; B29C66/72328; B29C66/73132; B29L; B29L2031/00; B29L2031/712; B29L2031/7162; B29L2031/7166; B32B2272/00; B32B2307/00; B32B2307/30; B32B2307/31; B32B2309/00; B32B2309/08; B32B2309/10; B32B2309/105; B32B2398/00; B32B2398/20; B32B2439/00; B32B2439/40; B32B2439/62; Y; Y10; Y10T; Y10T156/00; Y10T156/10; Y10T156/1052; Y10T156/1062; Y10T156/1064; Y10T156/1082; Y10T428/00; Y10T428/24; Y10T428/24942; Y10T428/2495; Y10T428/24967; Y10T428/31504; Y10T428/31855; Y10T428/31909; Y10T428/31913
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
260 words
A method of making a multiple-layer composite blank product in flattened tube form from which containers can be made, said blank comprising a composite sheet having a core layer of high density thermoplastic polymeric material having a specific gravity of about 0.950 to about 0.965, a thickness of 15 mils to about 17.5 mils, and a first pre-determined softening point, and at least one outer layer of lower density thermoplastic polymeric material on a side of said core layer, said outer layer having a specific gravity of about 0.918 to about 0.930, a thickness of about 0.75 mils to about 2.0 mils, and a second pre-determined softening point lower than said first pre-determined softening point such that said outer layer, at unconfined edge portions of said blank can be dynamically heated to sufficient molten condition for heat sealing while said core layer is not significantly thermally affected, and provides structural support for said outer layer without distortion or shrivelling, said method comprising the steps of co-extruding said layers to form a composite sheet having a core layer and an outer layer; cutting and scoring said sheet to form said composite container blank; passing unconfined portions of said composite container blank through an open flame, said flame impinging on said unconfined portions; thereby heating said outer layer by said flame to a molten condition for heat-sealing, while said core layer remains thermally insensitive to said heat and structurally supports said tacky outer layer in an undistorted condition; and, joining tacky portions of said composite container blank to form a side-seamed tube.
Claim 2
Independent Claim
260 words
A method of making a multiple-layer composite blank product in flattened tube form from which containers can be made, said blank comprising a composite sheet having a core layer of high density thermoplastic polymeric material having a specific gravity of about 0.950 to about 0.965, a thickness of 15 mils to about 17.5 mils, and a first pre-determined softening point, and at least one outer layer of lower density thermoplastic polymeric material on a side of said core layer, said outer layer having a specific gravity of about 0.918 to about 0.930, a thickness of about 0.75 mils to about 2.0 mils, and a second pre-determined softening point lower than said first pre-determined softening point such that said outer layer, at unconfined edge portions of said blank can be dynamically heated to sufficient molten condition for heat sealing while said core layer is not significantly thermally affected, and provides structural support for said outer layer without distortion or shrivelling, said method comprising the steps of co-extruding said layers to form a composite sheet having a core layer and an outer layer; cutting and scoring said sheet to form said composite container blank; passing unconfined portions of said composite container blank through an open flame, said flame impinging on said unconfined portions; thereby heating said outer layer by said flame to a molten condition for heat-sealing, while said core layer remains thermally insensitive to said heat and structurally supports said tacky outer layer in an undistorted condition; and, joining tacky portions of said composite container blank to form a side-seamed tube.
Claim 3
Dependent Claim
21 words
A method, as in claim 1 wherein, said core layer provides the sole structural support for said unconfined molten outer layers.
Claim 4
Independent Claim
257 words
A method of making a multiple-layer composite blank product in flattened tube form from which containers can be made, said blank comprising a core layer of high density thermoplastic polymeric material having a specific gravity of about 0.950 to about 0.965, a thickness of 15 mils to about 17.5 mils, and a first pre-determined softening point, and an outer layer of lower density thermoplastic polymeric material on each side of said core layer, said outer layers having a specific gravity of about 0.918 to about 0.930, a thickness of about 0.75 mils to about 2.0 mils, and a second pre-determined softening point lower than said first pre-determined softening point such that said outer layers at unconfined edge portions of said blank, can be dynamically heated to sufficient molten condition for heat-sealing, while said core layer is not significantly thermally affected, and provides structural support for said outer layer without distortion or shrivelling, said method comprising the steps of: co-extruding said layers to form a composite sheet having a core layer and an outer layer on each side thereof; cutting and scoring said sheet to form a composite container blank; passing unconfined portions of said composite container blank through an open flame, said flame impinging on said unconfined portions; thereby heating said outer layers by said flame to a molten condition for heat-sealing, while said core layer remains thermally insensitive to said heat and structurally supports said tacky outer layers in an undistorted condition; and, joining tacky portions of said composite container blank to form a side-seamed tube.
Claim 5
Independent Claim
257 words
A method of making a multiple-layer composite blank product in flattened tube form from which containers can be made, said blank comprising a core layer of high density thermoplastic polymeric material having a specific gravity of about 0.950 to about 0.965, a thickness of 15 mils to about 17.5 mils, and a first pre-determined softening point, and an outer layer of lower density thermoplastic polymeric material on each side of said core layer, said outer layers having a specific gravity of about 0.918 to about 0.930, a thickness of about 0.75 mils to about 2.0 mils, and a second pre-determined softening point lower than said first pre-determined softening point such that said outer layers at unconfined edge portions of said blank, can be dynamically heated to sufficient molten condition for heat-sealing, while said core layer is not significantly thermally affected, and provides structural support for said outer layer without distortion or shrivelling, said method comprising the steps of: co-extruding said layers to form a composite sheet having a core layer and an outer layer on each side thereof; cutting and scoring said sheet to form a composite container blank; passing unconfined portions of said composite container blank through an open flame, said flame impinging on said unconfined portions; thereby heating said outer layers by said flame to a molten condition for heat-sealing, while said core layer remains thermally insensitive to said heat and structurally supports said tacky outer layers in an undistorted condition; and, joining tacky portions of said composite container blank to form a side-seamed tube.
Claim 6
Dependent Claim
21 words
A method, as in claim 3 wherein, said core layer provides the sole structural support for said unconfined molten outer layers.
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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) | 1983-09-23 | 1984-03-24 | 1984-09-23 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-09-23 | 1988-03-24 | 1988-09-23 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-09-23 | 1992-03-24 | 1992-09-23 | $7700.00 | Window Closed / Lapsed |