Forming device and forming method
US-2018361458-A1 · Dec 20, 2018 · US
US9962753B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9962753-B2 |
| Application number | US-201514877381-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 7, 2015 |
| Priority date | Jun 28, 2013 |
| Publication date | May 8, 2018 |
| Grant date | May 8, 2018 |
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Official abstract text for this publication.
A tool is provided for preforming a metallic starter tube section for subsequent internal high pressure forming in order to produce a tubular IHF-component. The tool includes a plurality of tool sections that can move relative to one another and that delimit, between them, a shaping cavity for receiving and forming the starter tube section. The cavity has a contour which is both derived from the shape of the IHF component to be produced and adapted to the circumference of the starter tube section to be formed, such that each cavity cross section perpendicular to a cavity longitudinal axis predefined by the starter tube section corresponds to the cross-sectional shape of the IHF component cross-section in the same position, reduced in its cross-sectional circumference to exactly the circumference of the starter tube section. A method is provided for producing such a tool, and a method is provided for producing a tube-like IHF component using such a tool.
Opening claim text (preview).
What is claimed is: 1. A tool for preforming a metallic starter tube section for subsequent internal high pressure forming in order to produce a tubular IHF component, the tool comprising: a plurality of tool parts configured to move relative to one another, said plurality of tool parts between them delimiting a shaping cavity that receives and forms the starter tube section, wherein the shaping cavity has a contour both derived from a shape of the tubular IHF component to be produced and adapted to a circumference of the starter tube section to be preformed, the shaping cavity is structurally configured such that each cavity cross-section of the shaping cavity perpendicular to a cavity longitudinal axis conforms to a cross-sectional shape of the tubular IHF component cross-section, and the shaping cavity has a cross-sectional circumference that corresponds exactly to the circumference of the starter tube section. 2. The tool according to claim 1 , wherein the tool is a press-based tool, and the plurality of tool parts comprise a tool underpart and a tool upper part relatively movable with respect to one another. 3. A method for producing a tool for preforming a metallic starter tube section for subsequent internal high pressure forming in order to produce a tubular IHF component, the tool comprising a plurality of tool parts configured to move relative to one another, said plurality of tool parts between them delimiting a shaping cavity that receives and forms the starter tube section, wherein the shaping cavity has a contour both derived from a shape of the tubular IHF component to be produced and adapted to a circumference of the starter tube section to be preformed, and each cavity cross-section of the shaping cavity perpendicular to a cavity longitudinal axis predefined by the starter tube section conforms to a cross-sectional shape of the tubular IHF component cross-section in a same position, but reduced in its cross-sectional circumference to exactly the circumference of the starter tube section; the method comprising the acts of: providing geometrical data determining a shape of the tubular IHF component to be produced; determining the circumference of the starter tube section to be preformed; calculating the contour of the shaping cavity required to preform the starter tube section by use of guide sections, for which purpose transverse sections are produced initially along the longitudinal axis of the tubular IHF component, and said transverse sections are then reduced in circumference to the determined circumference of the starter tube section to be preformed; and manufacturing the tool with the shaping cavity having the calculated contour. 4. The method according to claim 3 , wherein the acts of providing, determining, and calculating are carried out automatically via a CAD program. 5. A tool for preforming a metallic starter tube section made in accordance with the method of claim 3 . 6. A method for producing a tubular IHF component via internal high pressure forming, the method comprising the acts of: providing a starter tube section; preforming the starter tube section in a tool having a plurality of tool parts movable relative to one another and between which delimit a shaping cavity for receiving and preforming the starter tube section, wherein the shaping cavity has a contour both derived from a shape of the tubular IHF component to be produced and adapted to a circumference of the starter tube section to be preformed, and each cavity cross-section of the shaping cavity perpendicular to a cavity longitudinal axis predefined by the starter tube section conforms to a cross-sectional shape of the tubular IHF component cross-section in a same position, but reduced in its cross-sectional circumference to exactly the circumference of the starter tube section; performing internal high pressure forming of the preformed starter tube section in an IHF tool in order to produce the tubular IHF component. 7. The method according to claim 6 , further comprising the act of: first bending the starter tube section prior to preforming the starter tube section. 8. The method according to claim 7 , wherein the starter tube section is formed of an aluminum or steel material and has a circular or oval cross-section. 9. The method according to claim 6 , wherein the starter tube section is formed of an aluminum or steel material and has a circular or oval cross-section. 10. The method according to claim 6 , wherein different circumferential stretching lying within a range of between 3% and 2% is achieved over the longitudinal axis of the preformed starter tube section during the performance of the internal high pressure forming. 11. The method according to claim 7 , wherein different circumferential stretching lying within a range of between 3% and 2% is achieved over the longitudinal axis of the preformed starter tube section during the performance of the internal high pressure forming. 12. The method according to claim 8 , wherein different circumferential stretching lying within a range of between 3% and 2% is achieved over the longitudinal axis of the preformed starter tube section during the performance of the internal high pressure forming. 13. The method according to claim 6 , wherein the preformed starter tube section is inserted into a cavity of the IHF tool such that a same distance to a cavity wall exists at every point on the longitudinal axis over a respective cross-sectional circumference. 14. The method according to claim 12 , wherein the preformed starter tube section is inserted into a cavity of the IHF tool such that a same distance to a cavity wall exists at every point on the longitudinal axis over a respective cross-sectional circumference. 15. The method according to claim 6 , wherein the tubular IHF component produced is a motor vehicle component. 16. The method according to claim 14 , wherein the tubular IHF component produced is a motor vehicle component. 17. A tool for preforming a metallic starter tube section made in accordance with the method of claim 6 .
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