EP1830976A2 - Method and apparatus for performing a magnetic pulse forming process - Google Patents
Method and apparatus for performing a magnetic pulse forming processInfo
- Publication number
- EP1830976A2 EP1830976A2 EP05855345A EP05855345A EP1830976A2 EP 1830976 A2 EP1830976 A2 EP 1830976A2 EP 05855345 A EP05855345 A EP 05855345A EP 05855345 A EP05855345 A EP 05855345A EP 1830976 A2 EP1830976 A2 EP 1830976A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- electrically conductive
- workpiece
- mandrel
- conductive member
- pulse forming
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 238000000034 method Methods 0.000 title claims abstract description 43
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 239000004020 conductor Substances 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 230000005672 electromagnetic field Effects 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 239000003990 capacitor Substances 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000002344 surface layer Substances 0.000 description 2
- 238000009827 uniform distribution Methods 0.000 description 2
- 206010039203 Road traffic accident Diseases 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000005520 electrodynamics Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/14—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces applying magnetic forces
Definitions
- This invention relates in general to magnetic pulse forming processes for deforming one or more metallic workpieces to a desired shape.
- this invention relates to an improved method and apparatus for performing such a magnetic pulse forming process wherein the plasticity of the workpiece to be deformed is preliminarily increased to facilitate deformation to the desired shape.
- Magnetic pulse forming is a well known process that can be used to deform one or more metallic workpieces to a desired shape.
- a magnetic pulse forming process is performed by initially disposing a portion of a workpiece either about or within a mandrel having the desired shape. Then, an electromagnetic field is generated either within or about the workpiece.
- Magnetic pulse forming can also be used to deform two metallic workpieces to a desired shape by initially disposing portions of first and second workpieces in an overlapping relationship and generating the electromagnetic field either within or about the overlapping portions of the first and second workpieces.
- Magnetic pulse forming can be used, for example, to form male and female members of a typical sliding spline type of slip joint.
- Such male and female members typically have respective pluralities of splines formed thereon.
- the male member is generally cylindrical in shape and has a plurality of outwardly extending splines formed on the outer surface thereof.
- the male member may be formed integrally with or secured to an end of a conventional driveshaft assembly, for example.
- the female member on the other hand, is generally hollow and cylindrical in shape and has a plurality of inwardly extending splines formed, on the inner surface thereof.
- the female member may be formed integrally with or secured to a yoke that forms a portion of a conventional universal joint, for example.
- the male member is inserted within the female member such that the outwardly extending splines of the male member cooperate with the inwardly extending splines of the female member.
- the male and female members are connected together for concurrent rotational movement.
- the outwardly extending splines of the male member can slide axially relative to the inwardly extending splines of the female member to allow a limited amount of relative axial movement to occur therebetween.
- the male and female members of such a sliding spline type of slip joint can be formed from hollow cylindrical workpieces that are deformed to have the male and females splines by means of magnetic pulse forming techniques.
- This invention relates to an improved method and apparatus for performing a magnetic pulse forming process wherein the plasticity of the workpiece to be deformed is preliminarily increased to facilitate deformation to the desired shape.
- a mandrel having a surface and an electrically conductive member are provided.
- the workpiece is oriented between the surface of the mandrel and the electrically conductive member, and a first electrical current is caused to flow through the workpiece and the electrically conductive member so as to increase the plasticity of the workpiece.
- a second electrical current is caused to flow through the electrically conductive member and the workpiece so as to cause to cause the workpiece to be deformed into engagement with the surface of the mandrel.
- FIG. 1 is a schematic side elevational view of a first embodiment of an apparatus for performing a magnetic pulse forming operation on a workpiece in accordance with this invention.
- Fig. 2 is an enlarged sectional elevational view of a portion of the apparatus illustrated in Fig. 1 shown during the deformation of the workpiece.
- Fig. 3 is a further enlarged sectional elevational view of a portion of the apparatus illustrated in Figs. 1 and 2 shown after the deformation of the workpiece.
- Fig. 4 is a schematic side elevational view of a second embodiment of an apparatus for performing a magnetic pulse forming operation in accordance with this invention.
- Fig. 5 is an enlarged sectional elevational view of a portion of the apparatus illustrated in Fig. 4 shown prior to the deformation of the workpiece.
- Fig. 6 is a schematic side elevational view of a third embodiment of an apparatus for performing a magnetic pulse forming operation on a workpiece in accordance with this invention.
- Fig. 7 is an enlarged sectional elevational view showing four different versions of the apparatus illustrated in Fig. 6 shown prior to the deformation of the workpiece.
- Fig. 8 is a schematic side elevational view of a fourth embodiment of an apparatus for performing a magnetic pulse forming operation on a workpiece in accordance with this invention.
- Fig. 9 is an enlarged sectional elevational view of a portion of the apparatus illustrated in Fig. 8 shown after to the deformation of the workpiece.
- Fig. 10 is an enlarged sectional elevational view of a portion of the apparatus illustrated in Figs. 8 and 9 shown after the deformation of the workpiece.
- Fig. 11 is a schematic side elevational view of a fifth embodiment of an apparatus for performing a magnetic pulse forming operation on a workpiece in accordance with this invention.
- Fig. 12 is an enlarged sectional elevational view of a portion of the apparatus illustrated in Fig. 11 shown after the deformation of the workpiece.
- FIG. 1 a first embodiment of a system, indicated generally at 10, for performing a magnetic pulse forming process in accordance with this invention.
- a tubular workpiece 12 is located co-axially relative to an axis L defined by an outer electrically conductive member 14 and an internal mandrel 16.
- the mandrel 16 includes a first end 18, a second end 20, and an elongated intermediate portion, indicated generally at 22.
- An outer surface of the intermediate portion 22 has a shape the corresponds to a desired final shape of the outer tubular member 12 after the magnetic pulse forming process has been performed.
- the outer surface of the intermediate portion 22 of the mandrel 16 has a plurality of longitudinally extending splines 24 formed thereon.
- the outer surface of the intermediate portion 22 of the mandrel 16 may have any desired shape.
- the first end 18 of the mandrel 16 is surrounded by the tubular workpiece 12 and is supported by a first electrically conductive insert 26 and an electrically conductive end member 28.
- the electrically conductive end member 28 is spaced from and electrically isolated from the outer member 14.
- the first insert 26 is preferably formed from a material that is a good electrical conductor, such as copper, for example.
- the second end 20 of the mandrel 16 is surrounded by a dielectric bushing 30.
- a bushing 32 surrounds the dielectric bushing 30 and abuts an inner wall of the tubular workpiece 12.
- the dielectric bushing 30 electrically insulates the bushing 32 from the mandrel 16 and prevents a short circuit from occurring with the tubular workpiece 12 during preheating, as will be explained in detail below.
- the dielectric bushing 32 also co-axially centers the mandrel 16 within the tubular workpiece 12.
- a second electrically conductive insert 34 is disposed between an outer wall of the tubular workpiece 12 and the outer electrically conductive member 14 to provide reliable and substantially uniform annular electrical contact between the outer electrically conductive member 14 and the tubular workpiece 12.
- the second insert 34 is also preferably formed from a material that is a good electrical conductor, such as copper, for example.
- a preheating current source 36 is electrically connected to the outer electrically conductive member 14 and to the electrically conductive end member 28.
- a switch 38 is provided to selectively interrupt the flow of electrical current from the preheating current source 36 to the outer electrically conductive member 14 and to the electrically conductive end member 28.
- the amplitude of the preheating current generated by the preheating current source 36 can be set as desired, but is preferably less than one hundred kiloamps.
- a pulse forming current source 40 is also electrically connected to the outer electrically conductive member 14 and to the electrically conductive end member 28. The amplitude of the pulse forming current generated by the pulse forming current source 40 can be set as desired, but is preferably at least five hundred kiloamps.
- a switch 42 is provided to selectively interrupt the flow of electrical current from the pulse forming current source 40 to the outer electrically conductive member 14 and to the electrically conductive end member 28.
- the energy needed for producing a pulse forming current in the pulse forming current source 40 can be stored in one or more energy storing devices or capacitors 44, which can be charged by a high-voltage charging supply (not shown).
- Other energy storing devices such as a motor/ generator set or some other suitable pulse source, for example, can be used without departing from the scope and spirit of the invention.
- the tubular workpiece 12 has a shape and position shown by dashed lines and depicted as A in Fig. 1.
- a gap G thus initially exists between the tubular workpiece 12 and the mandrel 16.
- the capacitors 44 of the pulse forming current source 40 are charged to the operating voltage. Air trapped in the gap G is preferably evacuated through special passages (not shown) formed in the mandrel 16 or the bushing 32.
- the air is evacuated to militate against the captured air acting as a damper and reducing the effectiveness of the deformation process.
- the switch 38 of the preheating current source 36 is then moved to the closed position to supply current to preheat the tubular workpiece 12. This preheating is accomplished by causing an electrical current to be passed through the electrically conductive end member 28, the first insert 26, the tubular workpiece 12, the second insert 34, and the outer electrically conductive member 14. It is desirable to maintain the power and the current of the preheating current source 36 as high as possible to provide the fastest preheating time to a desired plasticity of the tubular workpiece 12 without causing deformation.
- the switch 38 of the preheating current source 36 is moved to the open position, and the switch 42 of the pulse forming current source 36 is moved to the closed position.
- the capacitors 44 are thus caused to discharge the stored energy through the electrically conductive end member 28, the first insert 26, the preheated tubular workpiece 12, the second insert 34, and the outer electrically conductive member 14.
- the arrows in Fig. 1 show the direction of the electric current along the tubular workpiece 12 and through the outer electrically conductive member 14.
- the electrodynamic pressure of the magnetic field accompanying the current compresses a desired portion of the tubular workpiece 12 until an internal surface thereof contacts an outer surface of the mandrel 16.
- Fig. 2 shows the tubular workpiece 12 of Fig. 1 during the magnetic pulse forming operation, illustrating a magnetic field M that is induced between the tubular workpiece 12 and the outer electrically conductive member 14.
- the splines or teeth of the outer electrically conductive member 14 are located opposite the splines or teeth 24 formed on the mandrel 16.
- the configuration of the magnetic field M in the gap between the tubular workpiece 12 and the outer electrically conductive member 14 is shown for the last stage of the forming process, i.e., when the pulse current is being caused to flow.
- the frequency of the pulse current has been found to be desirable when between ten and twenty kilohertz, although it is understood that different current frequencies may be used as desired. Due to a proximity effect, the current is concentrated very close to the surface of the tubular workpiece 12. As a result, the discharge current is concentrated in thin surface layers of the outer electrically conductive member 14 and the tubular workpiece 12 that are faced one to the other, and magnetic field M has a wave form.
- the inner wall of the outer electrically conductive member 14 includes splines formed therein. It is understood that the inner wall could have a different cross-sectional shape such as circular, for example, without departing from the scope and spirit of the invention.
- FIG. 3 illustrates the tubular workpiece 12 of Fig. 1 as being attached to the mandrel 16 after the magnetic pulse forming operation has been performed. After the forming operation, the first insert 26 and the second insert 34 are removed, and the tubular workpiece 12, the dielectric bushings 30, the bushings 32, and the mandrel 16 are then disassembled.
- the method as described in Figs. 1, 2, and 3 relate to the use of an external inductor for deforming the tubular workpiece 12 inwardly onto the mandrel 16 disposed therein.
- the method of this invention can also be used in conjunction with an external inductor (not shown) for deforming the tubular workpiece 12 outwardly within a mandrel (not shown) disposed thereabout.
- the inner surface of the mandrel would be provided with the desired splined cross sectional shape for the tubular workpiece 12, which is expanded outwardly into engagement therewith.
- FIGs. 4 and 5 illustrate a second embodiment of a system, indicated generally at 50, for performing a magnetic pulse forming process in accordance with this invention.
- the magnetic pulse forming operation causes a radial expansion of an inner tubular member 52 into an external die or mandrel 54.
- the external mandrel 54 includes an annular array of axially extending teeth or splines 56 formed thereon.
- a cylindrical inner electrically conductive member 58 includes a first end 60 that is supported by a first electrically conductive end member 62 by means of a first insert 64.
- a second end 66 of the inner electrically conductive member 58 is supported by a second insert 68.
- a dielectric bushing 70 can be disposed adjacent the supported portion of the inner tubular member 52 and be embedded into the external mandrel 54.
- a supported portion of the inner tubular member 52 adjacent the first end 60 of the inner electrically conductive member 58 is seated on a second dielectric bushing 72.
- the supported portion of the inner tubular member 52 adjacent the first end 60 of the inner electrically conductive member 58 is supported by a second electrically conductive end member 74 and a third insert 76, which contacts the external mandrel 54.
- the first electrically conductive end member 62, the second electrically conductive end member 74, the inner tubular member 52, and the external mandrel 54 are concentrically disposed about longitudinal axis L.
- the second dielectric bushing 72 militates against radial deformation of the supported portion of the inner tubular member 52 adjacent the first end 60 of the inner electrically conductive member 58.
- Fig. 5 shows a sectional elevational view of the inner tubular member 52 of Fig. 4 during the magnetic pulse forming operation illustrating the magnetic field M induced between the inner tubular member 52 and the inner electrically conductive member 58.
- the splines or teeth of the inner electrically conductive member 58 are located opposite the splines or teeth 56 formed on the mandrel 54.
- the configuration of the magnetic field M in the gap between the inner tubular member 52 and the inner electrically conductive member 58 is shown for the last stage of the forming process, i.e., when the pulse current is being caused to flow.
- the frequency of the pulse current has been found to be desirable when between ten and twenty kilohertz, although it is understood that different current frequencies may be used as desired. Due to a proximity effect, the current is concentrated very close to the surface of the inner tubular member 52. As a result, the discharge current is concentrated in thin surface layers of the inner electrically conductive member 58 and the inner tubular member 52 which are faced one to the other, and magnetic field M has a wave form.
- Fig. 6 illustrates a third embodiment of a pulse forming system 80 including a magnetic field concentrator or electrically conductive bushing 82.
- the field concentrator 82 is inserted between an outer electrically conductive member 84 and an outer tubular member 86 and is electrically insulated from both the outer electrically conductive member 84 and the outer tubular member 86.
- the arrows in Fig. 6 show the current path when proximity effects are taken into account.
- the field concentrator 82 facilitates a method of concentrating and shaping the magnetic field and is useful when it becomes necessary to frequently readjust the pulse forming system 80 to form a tubular member having different diameters and shapes.
- the field concentrator 82 works by an induction principle, i.e., electric contact is not required with any elements of a discharge circuit, and it is much easier to change than any element of the circuit.
- the field concentrator 82 permits the number of splines to be formed to be easily changed. During the forming of tubular members, to create different diameters and numbers of splines, only the field concentrator 82 and first and second inserts 88, 90 need to be changed.
- FIG. 7 is a sectional elevational drawing of the magnetic field concentrator 82 of Fig. 6 illustrating the effect on the magnetic field with the magnetic field; concentrator 82 having different cross sectional shapes. Sectors a) and b) are shown such that the smooth, cylindrical surfaces of the outer electrically conductive member 84 and the field concentrator 82 provide the shortest magnetic line O in the gap between those surfaces.
- a method of providing a desirable distribution of a current by means of using axially extending splines or teeth 94 on the external surface of the field concentrator 82 and axially extending splines or teeth 96 on the internal surface of outer electrically conductive member 84.
- the splines 94 are disposed between the splines 96 and are insulated from one another (the insulation is not shown to make clear the changing configuration of magnetic field). The deeper and the larger the quantity the splines 94 and the splines 96, the lower the magnetic loss.
- FIG. 8 illustrates a fourth embodiment of a magnetic pulse forming system 100, wherein the magnetic pulse forming system 100 causes a radial compression of an inner tubular member 102 and an outer tubular member 104.
- the inner tubular member 102 and the outer tubular member 104 can be press fit together such that a desired amount of overlap exists.
- a mandrel 106 is co- axially disposed along axis L within the inner tubular member 102 and the outer tubular member 104.
- the mandrel 106 includes a first end 108, a second end 110, and an elongated intermediate portion, indicated generally at 112.
- An outer surface of the intermediate portion 112 has a shape in accordance with a desired final shape of the inner tubular member 102 and the outer tubular member 104 after the pulse forming operation has been conducted.
- a plurality of teeth or splines 114 is formed on the outer surface of the intermediate portion 112, as illustrated in Fig. 9.
- the first end 108 of the mandrel 106 is surrounded by the inner tubular member 102, and the outer tubular member 104 and is supported by a first electrically conductive insert 116 and an electrically conductive end member 118.
- the electrically conductive end member 118 is spaced from and electrically isolated from an outer electrically conductive member 120.
- the first insert 116 is preferably formed from a material that is a good electrical conductor, such as copper, for example.
- the second end 110 of the mandrel 106 is surrounded by a dielectric bushing 122.
- a bushing 124 surrounds the dielectric bushing 122 and abuts an inner wall of the outer tubular member 104.
- the dielectric bushing 122 electrically insulates the bushing 124 from the mandrel 106 and prevents a short circuit from occurring with the outer tubular member 104 during preheating, as discussed above.
- the bushing 124 also axially centers the mandrel 106 within the outer tubular member 104.
- a second electrically conductive insert 126 is disposed between an outer wall of the outer tubular member 104 and the outer electrically conductive member 120 to provide reliable and substantially uniform annular electric contact between the outer electrically conductive member 120 and the outer tubular member 104.
- the second insert 126 is also preferably formed from a material that is a good electrical conductor, such as copper, for example.
- the remainder of the structure and the forming process is the same as described above for Fig. 1.
- the direction of flow of the current is indicated by the arrows.
- inner tubular member 102 and the outer tubular member 104 could be disposed within the mandrel 106 and the outer electrically conductive member 120 disposed within the inner tubular member 102 and the outer tubular member 104 to deform the inner tubular member 102 and the outer tubular member 104 outwardly into engagement with the mandrel 106 without departing from the scope and spirit of the invention.
- FIG. 9 illustrates the fourth embodiment of the invention of Fig. 8 showing the inner tubular member 102 and the outer tubular member 104 on the mandrel 106.
- Fig. 10 illustrates of the inner tubular member 102 and the outer tubular member 104 of Fig. 8 removed from the mandrel 106 after the magnetic pulse forming operation.
- the fourth embodiment illustrated in Figs. 8, 9, and 10 is particularly useful in forming a collapsible telescopic driveshaft. The forming according to the method militates against any relative axial or rotational movement between the inner tubular member 102 and the outer tubular member 104 under normal operating conditions of the driveshaft.
- the inner tubular member 102 and the outer tubular member 104 will move telescopically relative to one another.
- the amount of force required to cause such telescopic movement can be adjusted by varying the length of the overlapping section of the inner tubular member 102 and the outer tubular member 104.
- Fig. 11 illustrates a fifth embodiment of a magnetic pulse forming system 130, wherein the magnetic pulse forming system 130 causes a radial compression of an inner tubular member 132 with an annular recess 134 formed therein by an annular recess 136 formed in a mandrel, indicated generally at 138.
- the recess 134 facilitates cutting, chamfering, and other machining operations that may be necessary for joining the inner tubular member 132 with an outer tubular member (not shown).
- an axial current is applied as illustrated in Fig. 11, to provide the relatively deeper deformation in the area of the annular recess 134 of the inner tubular member 132 a greater amplitude of current may be required.
- Fig. 12 is an involuted partial sectional view of the inner tubular member 132 of Fig. 11 with the inner tubular member 132 attached to the mandrel 138 after the magnetic pulse forming operation.
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Manufacturing Cores, Coils, And Magnets (AREA)
Abstract
Description
Claims
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US63924704P | 2004-12-27 | 2004-12-27 | |
| US11/312,248 US20060156776A1 (en) | 2004-12-27 | 2005-12-19 | Method and apparatus for performing a magnetic pulse forming process |
| PCT/US2005/046764 WO2006071766A2 (en) | 2004-12-27 | 2005-12-27 | Method and apparatus for magnetic pulse forming |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1830976A2 true EP1830976A2 (en) | 2007-09-12 |
| EP1830976A4 EP1830976A4 (en) | 2008-11-26 |
Family
ID=36615441
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP05855345A Withdrawn EP1830976A4 (en) | 2004-12-27 | 2005-12-27 | Method and apparatus for performing a magnetic pulse forming process |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20060156776A1 (en) |
| EP (1) | EP1830976A4 (en) |
| JP (1) | JP2008525198A (en) |
| BR (1) | BRPI0519358A2 (en) |
| WO (1) | WO2006071766A2 (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI351325B (en) * | 2008-12-09 | 2011-11-01 | Metal Ind Res & Dev Ct | Device for producing patterns and a method thereof |
| US8408317B2 (en) * | 2010-01-11 | 2013-04-02 | Tiw Corporation | Tubular expansion tool and method |
| CN102486509A (en) * | 2010-12-01 | 2012-06-06 | 首都航天机械公司 | Life test method of magnetic-pulse forming inductor |
| US8899084B2 (en) | 2011-10-10 | 2014-12-02 | Dana Automotive Systems Group, Llc | Magnetic pulse welding and forming for plates |
| US9028164B2 (en) | 2012-03-08 | 2015-05-12 | Dana Automotive Systems Group, Llc | Magnetic pulse formed vehicle driveshaft and method of making same |
| EP3512664A1 (en) * | 2016-06-13 | 2019-07-24 | Mores, Stylianos | Electromagnetic hammer device for the mechanical treatment of materials and method of use thereof |
| JP6539366B1 (en) * | 2018-03-02 | 2019-07-03 | 株式会社神戸製鋼所 | Electromagnetic molding method |
| US20230241705A1 (en) * | 2022-01-28 | 2023-08-03 | GM Global Technology Operations LLC | Method and device for impact welding of battery terminals |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2199926A (en) * | 1937-07-19 | 1940-05-07 | Borg Warner | Resilient slip joint |
| US3293884A (en) * | 1961-08-03 | 1966-12-27 | Grob Inc | Power transmitting element |
| US3794805A (en) * | 1971-07-02 | 1974-02-26 | W Rudd | Magnetic pulse welding using spaced proximity conductor |
| US3998081A (en) * | 1974-07-17 | 1976-12-21 | The Boeing Company | Electromagnetic dent puller |
| FR2374106A1 (en) * | 1976-12-20 | 1978-07-13 | Ardef Asbl | Magnetic pulse metal tube shaping system - also uses induction member to heat workpiece for improved results |
| US4702543A (en) * | 1986-04-30 | 1987-10-27 | G & H Technology, Inc. | Environmental seal and alignment means for an electromagnetically formed backshell |
| US4986102A (en) * | 1989-05-23 | 1991-01-22 | The Boeing Company | Electromagnetic dent remover with tapped work coil |
| US5331832A (en) * | 1993-08-23 | 1994-07-26 | Xerox Corporation | Sleeve sizing processes |
| US5836070A (en) * | 1994-04-12 | 1998-11-17 | Northrop Grumman Corporation | Method and forming die for fabricating torque joints |
| ES2202339T3 (en) * | 1994-10-13 | 2004-04-01 | Matsui Universal Joint Manufacturing Company | MANUFACTURING PROCEDURE OF A CONTROL AXIS. |
| US5824998A (en) * | 1995-12-20 | 1998-10-20 | Pulsar Welding Ltd. | Joining or welding of metal objects by a pulsed magnetic force |
| DE19602951C2 (en) * | 1996-01-27 | 2000-12-07 | Steingroever Magnet Physik | Method and device for expanding pipes or tubular parts by the magnetic field of a current pulse |
| US5730016A (en) * | 1996-03-22 | 1998-03-24 | Elmag, Inc. | Method and apparatus for electromagnetic forming of thin walled metal |
| US5983478A (en) * | 1996-09-18 | 1999-11-16 | The Boeing Company | Tube forming on an end fitting |
| US6065317A (en) * | 1997-04-12 | 2000-05-23 | Magnet-Physik Dr. Steingroever Gmbh | Apparatus and procedure for manufacturing metallic hollow bodies with structural bulges |
| US6379254B1 (en) * | 1997-06-20 | 2002-04-30 | Spicer Driveshaft, Inc. | End fitting adapted to be secured to driveshaft tube by electromagnetic pulse welding |
| US5981921A (en) * | 1997-06-20 | 1999-11-09 | Dana Corporation | Method of magnetic pulse welding an end fitting to a driveshaft tube of a vehicular driveshaft |
| US6015350A (en) * | 1997-12-03 | 2000-01-18 | Dana Corporation | Collapsible vehicle driveshaft |
| US6484384B1 (en) * | 1998-12-31 | 2002-11-26 | Spicer Driveshaft, Inc. | Method of manufacturing an axially collapsible driveshaft assembly |
| US6368225B1 (en) * | 1999-12-30 | 2002-04-09 | Spicer Driveshaft, Inc. | Axially collapsible driveshaft assembly and method of manufacturing same |
| US6371859B1 (en) * | 2000-02-03 | 2002-04-16 | Dana Corporation | Axially collapsible driveshaft assembly |
| US7007362B2 (en) * | 2003-04-29 | 2006-03-07 | Torque-Tractiontechnologies, Inc. | Method of forming a slip joint |
| US7395597B2 (en) * | 2005-02-18 | 2008-07-08 | Edison Welding Institute Inc | Opposed current flow magnetic pulse forming and joining system |
-
2005
- 2005-12-19 US US11/312,248 patent/US20060156776A1/en not_active Abandoned
- 2005-12-27 WO PCT/US2005/046764 patent/WO2006071766A2/en not_active Ceased
- 2005-12-27 EP EP05855345A patent/EP1830976A4/en not_active Withdrawn
- 2005-12-27 JP JP2007548515A patent/JP2008525198A/en active Pending
- 2005-12-27 BR BRPI0519358-3A patent/BRPI0519358A2/en not_active Application Discontinuation
Also Published As
| Publication number | Publication date |
|---|---|
| BRPI0519358A2 (en) | 2009-01-20 |
| JP2008525198A (en) | 2008-07-17 |
| US20060156776A1 (en) | 2006-07-20 |
| WO2006071766A2 (en) | 2006-07-06 |
| WO2006071766A3 (en) | 2006-10-26 |
| EP1830976A4 (en) | 2008-11-26 |
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