Systems and methods for electromagnetic forming of containers
US-10081045-B2 · Sep 25, 2018 · US
US2018339331A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2018339331-A1 |
| Application number | US-201715602583-A |
| Country | US |
| Kind code | A1 |
| Filing date | May 23, 2017 |
| Priority date | May 23, 2017 |
| Publication date | Nov 29, 2018 |
| Grant date | — |
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A method, system, and apparatus for a part forming system. The part forming system comprises a field shaper having a cavity configured to receive a workpiece and a die. The field shaper has a number of dimensions based on being inserted into a main coil. The workpiece is bent to form a part with a desired shape when an electromagnetic field from the main coil is applied to the field shaper while the filed shaper is located within the main coil.
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What is claimed is: 1 . A part forming system comprising: a field shaper having a cavity configured to receive a workpiece and a die, wherein the field shaper has a number of dimensions based on being inserted into a main coil, and wherein the workpiece is bent to form a part with a desired shape when an electromagnetic field from the main coil is applied to the field shaper while the field shaper is located within the main coil. 2 . The part forming system of claim 1 further comprising: an electromagnetic system having the main coil, wherein the main coil causes a compressive force on the workpiece on the die to form the part. 3 . The part forming system of claim 1 , wherein the field shaper has a first half and a second half, wherein the first half has a slot that receives the die and the second half has a shape that receives the workpiece placed on the die when the first half and the second half are joined to define the cavity. 4 . The part forming system of claim 1 , wherein the number of dimensions is selected based on a size of the main coil. 5 . The part forming system of claim 4 , wherein the number of dimensions is selected from at least one of a height of the field shaper, a length of the field shaper, a length of a forming area, and a height of the forming area. 6 . The part forming system of claim 1 , wherein the die is selected from a group of dies consisting of a joggle die, an offset joggle die, and a crush joggle die. 7 . The part forming system of claim 1 , wherein the electromagnetic field causes a magnetic pressure that forms joggle bends in the workpiece for the desired shape of the part. 8 . The part forming system of claim 1 , wherein the field shaper has a cylindrical shape. 9 . The part forming system of claim 1 , wherein the die is a joggle die and the part is a stringer for an aircraft. 10 . The part forming system of claim 1 , wherein the part is selected from one of a stringer, a fuselage stringer, an aircraft stringer, an intercostal, a hydraulic reservoir, a cleat, a duct, a shaped frame, and a shear tie. 11 . The part forming system of claim 1 , wherein the workpiece comprises at least one of a conductive material, a metal alloy, a nickel alloy, aluminum, steel, carbon steel, copper, brass, silver, iron, or titanium. 12 . A part forming system for forming joggle bends in a workpiece, the part forming system comprising: a main coil; a joggle die; and a field shaper having a cavity configured to receive the workpiece and the joggle die, wherein the field shaper has a number of dimensions based on a number of dimensions of the main coil, and wherein the joggle bends are formed in the workpiece to form a part with a desired shape when an electromagnetic field from the main coil is applied to the field shaper while the field shaper is located within the main coil. 13 . The part forming system of claim 12 , wherein the field shaper has a first half and a second half, the first half has a slot that receives the joggle die, and the second half has a shape that receives the workpiece placed on the joggle die when the first half and the second half are joined to define the cavity. 14 . The part forming system of claim 12 , wherein the number of dimensions is selected based on a size of the main coil. 15 . The part forming system of claim 12 , wherein the joggle die is selected from a group of dies consisting of an offset joggle die and a crush joggle die. 16 . A method for forming a part, the method comprising: placing a workpiece into a cavity of a field shaper; and applying an electromagnetic field to the field shaper from a main coil located around the field shaper, wherein the electromagnetic field causes a magnetic pressure that bends the workpiece on a die into a desired shape for the part. 17 . The method of claim 16 further comprising: inserting the field shaper with the workpiece in the cavity into the main coil. 18 . The method of claim 16 , wherein the magnetic pressure is a compressive force on the workpiece that bends the workpiece into the desired shape for the part. 19 . The method of claim 16 , wherein the magnetic pressure forms joggle bends in the workpiece to form the part. 20 . The method of claim 16 , wherein the part is selected from one of a stringer, a fuselage stringer, an aircraft stringer, an intercostal, a hydraulic reservoir, a cleat, a duct, a shaped frame, and a shear tie.
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