US3964413A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Methods for necking-in sheet metal can bodies
Assignee: National Steel Corp
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Filing: 1974-07-22
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Granted: 1976-06-22
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Expires: 1994-07-22
Abstract
Abstract Die-forming method for forming necked-in flanging metal on a light gauge drawn and ironed can body with a longitudinally extended transition zone between the necked-in portion and the original can body diameter portion while avoiding wrinkling or puckering of the flanging metal. In an initial stage of the die-forming operation, sheet metal contiguous to the peripheral edge is strengthened by turning such edge inwardly about a small radius. The strengthening member formed exerts a lateral restraint during a second stage of the die-forming operation in which the flanging metal and longitudinally extended transition zone are formed. The die-forming operation is carried out from a single end of the can body using a loose fitting inner die which is readily removable from the working end after reducing the diameter of such end.
Inventors
- 👤 William T. Saunders
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 09:57
CPC Classifications
B; B21; B21D; B21D51/00; B21D51/16; B21D51/26; B21D51/2615; B21D51/2638; Y; Y10; Y10S; Y10S72/00; Y10S72/715; Y10T; Y10T70/00; Y10T70/70; Y10T70/7441; Y10T70/7486; Y10T70/7508; Y10T70/7537; Y10T70/7542; Y10T70/7559; Y10T70/7655
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
324 words
In the manufacture of a sheet metal container, a multi-stage die-forming method for necking-in the open end of a can body to provide flanging metal free of wrinkles, comprising the steps of providing an open-ended can body having a sidewall of substantially cylindrical configuration about a longitudinally extended central axis, the sidewall defining an open end having a peripheral edge, die-forming a strengthening member in the sheet metal contiguous to the open-end with a first set of dies including an outer strengthening-member die cooperating with an inner pilot die by turning such peripheral edge inwardly with such outer strengthening-member die toward the central axis of the can body about a radius of curvature of a dimension in the range of about ten to fifteen times the thickness of the sheet metal being die formed, the peripheral edge being turned inwardly about the full circumference of such peripheral edge and then turning such peripheral edge with the inner pilot die toward such open end to extend in a direction parallel to the central axis, such extension of sheet metal in the direction parallel to the central axis having a longitudinal dimension of less than .0625 inch, and then die-forming such open end with strengthening member to form a reduced diameter neck with a second set of dies including an outer necking-in die and an inner pilot-type die by contacting the can body sidewall at a location adjacent to but spaced longitudinally from the strengthening member with the outer necking-in die to form a curvilinear configuration transition zone between the original can body and the reduced diameter neck and to form wrinkle-free flanging metal, such transition zone being formed about a radius of curvature which is greater than fifteen times the thickness gage of the sheet metal being die formed, such necked-in flanging metal having a longitudinal dimension which is a plurality of times greater than the corresponding longitudinal dimension of the initially formed strengthening member.
Claim 2
Dependent Claim
324 words
In the manufacture of a sheet metal container, a multi-stage die-forming method for necking-in the open end of a can body to provide flanging metal free of wrinkles, comprising the steps of providing an open-ended can body having a sidewall of substantially cylindrical configuration about a longitudinally extended central axis, the sidewall defining an open end having a peripheral edge, die-forming a strengthening member in the sheet metal contiguous to the open-end with a first set of dies including an outer strengthening-member die cooperating with an inner pilot die by turning such peripheral edge inwardly with such outer strengthening-member die toward the central axis of the can body about a radius of curvature of a dimension in the range of about ten to fifteen times the thickness of the sheet metal being die formed, the peripheral edge being turned inwardly about the full circumference of such peripheral edge and then turning such peripheral edge with the inner pilot die toward such open end to extend in a direction parallel to the central axis, such extension of sheet metal in the direction parallel to the central axis having a longitudinal dimension of less than .0625 inch, and then die-forming such open end with strengthening member to form a reduced diameter neck with a second set of dies including an outer necking-in die and an inner pilot-type die by contacting the can body sidewall at a location adjacent to but spaced longitudinally from the strengthening member with the outer necking-in die to form a curvilinear configuration transition zone between the original can body and the reduced diameter neck and to form wrinkle-free flanging metal, such transition zone being formed about a radius of curvature which is greater than fifteen times the thickness gage of the sheet metal being die formed, such necked-in flanging metal having a longitudinal dimension which is a plurality of times greater than the corresponding longitudinal dimension of the initially formed strengthening member.
Claim 3
Dependent Claim
33 words
The method of claim 1 in which the sheet metal comprises flat rolled steel having a thickness gauge between about 0.003 inch and 0.0075 inch at a location contiguous to such peripheral edge.
Claim 4
Dependent Claim
30 words
The method of claim 1 in which the sheet metal comprises flat rolled aluminum having a thickness gauge contiguous to such peripheral edge between about 0.0065 inch and 0.0085 inch.
Claim 5
Dependent Claim
29 words
The method of claim 1 in which the longitudinal dimension parallel to the central axis of the necked-in flanging metal is between about 0.125 inch and about 0.75 inch.
Claim 6
Dependent Claim
75 words
The method of claim 1 in which the inner pilot die of the first set of dies and the inner pilot-type die of the second set of dies are cylindricallyshaped with clearance, in addition to the thickness of the sheet metal being worked, between portions of such respective die sets which are parallel to the central axis being between about 20 percent and about 100 percent of the thickness of the sheet metal being worked.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-06-22 | 1979-12-22 | 1980-06-22 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-06-22 | 1983-12-22 | 1984-06-22 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-06-22 | 1987-12-22 | 1988-06-22 | $7700.00 | Window Closed / Lapsed |