Patent US3933020A successfully refreshed from Google Patents.
US3933020A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for stretch wrapping of panels
Assignee: Astech MCI Manufacturing Inc
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Filing: 1974-07-18
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Granted: 1976-01-20
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Expires: 1994-07-18
Abstract
Abstract A method of stretch wrapping metallic panels, particularly honeycomb structure sandwich panels, in which the panel is heated by passing an electrical current through it during the forming step. A pair of electrode tabs are joined to opposing edges of the panel and are gripped in gripper jaws which are slidable between tapered blocks so that as more tension is created in the panel, the jaws tighten. The electrical connections are made to the tapered blocks and current flows to the panel across the sliding joint and through the jaws.
Inventors
- 👤 Lavern G. Orr
- 👤 Etric Lee Stone
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 16:25
CPC Classifications
B; B21; B21D; B21D11/00; B21D11/02; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49826; Y10T29/49861
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
162 words
A method of stretch forming a honeycomb structure sandwich panel which comprises: a. joining a pair of electrode tabs to opposing edges of said panel; b. sealing the periphery of said panel; c. gripping each of said electrode tabs between two groups of pairs of jaws, each of said pair of jaws being slideable between a pair of tapered blocks, whereby the clamping force between each pair of jaws will increase as tension is applied to said panel; d. applying force to separate said groups of pairs of jaws, whereby tension will be created in said panel; e. coupling a source of electrical current to said tapered blocks, all of said tapered blocks gripping one of said electrode tabs being coupled in parallel; f. circulating an inert gas through the interior of said panel while said panel heated by said electrical current; and g. wrapping said panel about a form block wherey said panel will assume the contours of said form block.
Claim 2
Independent Claim
162 words
A method of stretch forming a honeycomb structure sandwich panel which comprises: a. joining a pair of electrode tabs to opposing edges of said panel; b. sealing the periphery of said panel; c. gripping each of said electrode tabs between two groups of pairs of jaws, each of said pair of jaws being slideable between a pair of tapered blocks, whereby the clamping force between each pair of jaws will increase as tension is applied to said panel; d. applying force to separate said groups of pairs of jaws, whereby tension will be created in said panel; e. coupling a source of electrical current to said tapered blocks, all of said tapered blocks gripping one of said electrode tabs being coupled in parallel; f. circulating an inert gas through the interior of said panel while said panel heated by said electrical current; and g. wrapping said panel about a form block wherey said panel will assume the contours of said form block.
Claim 3
Dependent Claim
16 words
The method of claim 1, wherein said electrode tabs are joined to said panel by welding.
Claim 4
Independent Claim
165 words
A method of forming a honeycomb sandwich panel in a stretch forming apparatus which comprises the steps of: a. attaching a pair of metallic sheets to two spaced edges of said panel; b. sealing the periphery of said panel and filling the interior of said panel with an inert gas; c. gripping substantially parallel edges of said metallic sheets between two groups of pairs of jaws, each of said groups of jaws being electrically insulated from the frame of said apparatus of said jaws being arranged to grip said panel with increasing force as tension is applied to said panel; d. applying force to separate said groups of pairs of jaws whereby tension will be created in said panel; e. applying an electrical potential to said metallic sheets and panel between said groups of pairs of jaws, each pair of jaws within each group being coupled; f. wrapping said panel about a form block, whereby said panel will assume the contours of said form block.
Claim 5
Independent Claim
165 words
A method of forming a honeycomb sandwich panel in a stretch forming apparatus which comprises the steps of: a. attaching a pair of metallic sheets to two spaced edges of said panel; b. sealing the periphery of said panel and filling the interior of said panel with an inert gas; c. gripping substantially parallel edges of said metallic sheets between two groups of pairs of jaws, each of said groups of jaws being electrically insulated from the frame of said apparatus of said jaws being arranged to grip said panel with increasing force as tension is applied to said panel; d. applying force to separate said groups of pairs of jaws whereby tension will be created in said panel; e. applying an electrical potential to said metallic sheets and panel between said groups of pairs of jaws, each pair of jaws within each group being coupled; f. wrapping said panel about a form block, whereby said panel will assume the contours of said form block.
References Cited (Backward Citations)
US2279964A
Cited
US2442268A
Cited
US2325481A
Cited
US2443336A
Cited
US2632493A
Cited
US3021887A
Cited
US2824594A
Cited
US3073373A
Cited
US3077031A
Cited
US3788117A
Cited
US3785788A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-01-19 | 1979-07-21 | 1980-01-20 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-01-19 | 1983-07-21 | 1984-01-20 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-01-19 | 1987-07-21 | 1988-01-20 | $7700.00 | Window Closed / Lapsed |