US2001016459A1PendingUtilityA1
Electromagmetic joining or welding of metal objects
Priority: Dec 20, 1995Filed: May 5, 1998Published: Aug 23, 2001
Est. expiryDec 20, 2015(expired)· nominal 20-yr term from priority
B21D 26/14B23K 20/00B23K 20/06
28
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Claims
Abstract
A method of joining or welding of at least a portion of a first metal workpiece to at least a portion of one or more second metal workpieces, comprising inducing movement in said portion of the first workpiece by means of a pulsed magnetic force so as to impact said portion of the second workpiece, the movement imparting a kinetic energy on the at least portion of the first workpiece to cause the two at least portions to join or weld to one another.
Claims
exact text as granted — not AI-modified1 . A method of joining or welding of at least a portion of a first metal workpiece to at least a portion of one or more second metal workpieces, comprising inducing movement in said portion of the first workpiece by means of a pulsed magnetic force so as to impact said portion of the second workpiece, the movement imparting a kinetic energy on the at least portion of the first workpiece to cause the two at least portions to join or weld to one another
2 . A method according to claim 1 , comprising:
(a) bringing the two metal workpieces into proximity to one another such that a first surface or a portion thereof in a first of the two workpiece which is to be joined or welded to a second surface or portion thereof in a second of the two workpieces, is opposite said second surface or portion; (b) forcing at least a portion of the first workpiece which comprises said first surface or said portion, towards the second workpiece by means of a pulsed magnetic force, the force being such so as to cause a portion of the first workpiece to impact onto said second workpiece with an initial kinetic energy of the first workpiece prior to impact is equal to or larger than the combined plastic deformation energy of the first workpiece, and elastic deformation energy of the second workpiece after the impact; whereby the two workpieces become joined or welded to one another.
3 . A method according to claim 1 , wherein each of the two metal workpieces is, independently, either an elongated object or has at least an elongated portion, the two workpieces being joined or welded to one another at the at least elongated portion; the dimensions of the two workpieces or portions being initially such that they can fit one into the other; the method comprising:
(a) inserting the at least elongated portions of one of the two workpieces, into a hollow interior of the other; (b) causing surfaces of the at least elongated portion of the first workpiece to move towards opposite surfaces of the at least elongated portion of the second workpiece by means of a pulsed magnetic force, so as to cause the surfaces of the at least elongated portion of the first workpiece to impact the opposite surfaces of the at least elongated portion of the second workpiece at a velocity such that the kinetic energy of the moving surfaces of the at least elongated portion of the first workpiece prior to the impact will be larger than a combination of the plastic deformation energy of the moving at least elongated portion of the first workpiece and the elastic deformation energy of the at least elongated portion of the second workpiece, after the impact; whereby the at least elongated portions of the two workpieces will become joined or welded to one another.
4 . A method according to claim 3 , wherein said first workpiece is a cable lug and said second workpiece is a cable.
5 . A method according to claim 3 , wherein said first workpiece is an envelope or matrix of a super-conductor cable made of one alloy and the second workpiece is one or more filaments made of a second alloy inserted in a lumen or longitudinal bores of the super-conductor cable; the method comprising inserting said filaments in said lumen or bores and then constricting said matrix or envelope by means of said pulsed magnetic force.
6 . A method according to claim 3 , for the production of a ground lead.
7 . A method according to claim 3 , wherein the velocity U of the surface of the first workpiece prior to impact with the opposite surface of the second workpiece is approximately represented by the following Equation (1):
U >{square root}{square root over (( A 1 +A 2 )/ m 1 )} (8)
wherein
U is the velocity of the moving surface of the first, moving workpiece, prior to the impact,
m 1 is the mass of the moving workpiece or if not the entire workpiece is being deformed then the mass of the worked portion, and
A 1 and A 2 are the plastic deformation energy of the first, moving workpiece, and the elastic deformation energy of the second, still workpiece, respectively, which may be calculated according to the following approximate Equations (2) and (3):
A 1 =σ 1 V 1 e In(1/(1+δ 1 )) /( r 02 /r 2 −1) (10)
wherein
r 01 and r 02 , are, respectively, the radii of the first and second workpieces of said portion prior to the deformation,
r 1 and r 2 are, respectively, the radii of the first and second workpieces of said portion after deformation,
δ 1 and δ 2 are the tensile strength of the material,
V 1 and V 2 are, respectively, the volumes enclosed within the first and within the second workpiece or within said portions after the deformation, and
δ 1 and δ 2 are the relative extension of the first and the second workpiece, respectively, calculated according to the following Equations (4) and (5):
δ 1 = r 01 - r 1 r 01 ( 11 ) δ 2 = r 02 - r 2 r 02 ( 12 )
8 . A method according to claim 7 , wherein the working voltage V is calculated by the following approximate Equations (6) and (7):
W = km 1 U 2 4 π μ 0 r 01 l 1 h ( 13 ) V = 2 W C ( 14 )
where
W is the energy stored in the capacitor battery,
k is a coefficient which depends on the parameters of the PMF device (including capacitance and own inductance) and parameters of working coil, and
m 1 and r 01 are as above,
l is the length of the working coil (and also the length of the deforming section of the workpiece.
h is the thickness of the space between the working coil and the workpiece.
9 . A method according to claim 1 , wherein the two workpieces are essentially planar or have at least a planar portion, with the two at least planar portions being welded to one another.
10 . A joint between a cable and a cable lug having a void space within the lug which is essentially zero.
11 . A super-conductor cable comprising a matrix or envelope made of one alloy and filaments made of another alloy and being contained within a lumen or longitudinal bore within said matrix or envelope, said cable being characterized in that it has void space which is essentially zero.
12 . A device for a pulsed magnetic forming of a metal alloy, comprising a plurality of current discharge circuits each comprising an independent primary coil and comprising a field shaper which is in a current inductive association with the primary coils of each of the plurality of circuits.
13 . A device for a magnetic forming of metal alloys, comprising a plurality of current discharge circuits, each comprising an independent primary coil of a plurality of windings and a secondary coil with a single winding, all secondary coils being connected in parallel to a forming coil of a single wind.
14 . A device according to claim 12 or 13 , wherein each of the circuits comprising a discharge switch, the device further comprising a triggering generator, the discharge switches of all circuities being controlled by the triggering generator.Join the waitlist — get patent alerts
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