Wire threading method and apparatus (original) (raw)
April 18, 1967 JUDGE WIRE THREADING METHOD AND APPARATUS 4 Sheets-Sheet 1' Filed April 29, 1964 INVENTOR ROBERT L. JUDGE Fifi III III ATTORNEY April 18, 196? R. L. JUDGE WIRE THREADING METHOD AND APPARATUS 4 Sheets-Sheet z Filed April 29, 1964 O O O O O O O O O o O O ODOOQOOOOOO OOOOOOOOOOO oooooooooo' April 18, 1967 ,1 L, JUDGE 3,314,131
WIRE THREADING METHOD AND APPARATUS Filed April 29, 1964 4 Sheets-Sheet 5 2 5 5g as F N ca\ i i. 0 1 m I FIG. 5
April 18, 1967 R. L. JUDGE 3,314,131
WIRE THREADING METHOD AND APPARATUS United States Patent Ofiice 3,314,131 Patented Apr. 18, 1967 3,314,131 WIRE THREADING METHOD AND APPARATUS Robert L. Judge, Poughkeepsie, N.Y., assignor to International Business Machines Corporation, New York, N.Y., a corporation of New York I Filed Apr. 29, 1964, Ser. No. 363,481
30 Claims. (Cl. 29-1555) This invention relates in general to wire inserting techniques and more particularly to techniques for threading thin, flexible wires through groups of small, apertured articles.
In the manufacture of apparatus such as magnetic core memories which use coordinate groupings of small apertured articles threaded by very thin wires, it is customary to utilize needles of various kinds for guiding the wires through the respective rows and columns of aligned apertures in the articles. For example, in the multiple threading of wires through parallel rows of magnetic cores according to conventional practice, a parallel group of hollow needles is passed simultaneously through the holes in several rows of toroidal magnetic cores, and the wires then are fed respectively through the hollow centers of these needles, following which the needles are withdrawn. In the special hand-wiring operations which also are required in assembling core memory planes according to conventional practice, a solid needle having a smaller diameter than a hollow needle is used to guide the wire, the leading end of this wire being secured by a suitable technique (such as percussive welding) to the trailing end of the needle.
Needle threading methods of the types just described have been employed very effectively in the past for wiring large groups of apertured articles such as the core planes of magnetic core memories. However, a recent trend in the design of such apparatus contemplates reducing the size of the cores through which the wires are threaded, there by to improve the performance of the core array. Where such reduction of the hole size is contemplated, the use of conventional needle threading techniques for wiring the core planes becomes very questionable, if not impossible. A hollow needle requires a hole diameter in the cores greater than is considered desirable for obtaining the improved performance expected of. such memory elements in the newer designs. Solid needles can be passed through holes of smaller size, but the use of such needles is not considered economically feasible in multiple wire threading operations inasmuch as this would require making a large number of highly accurate and reliable bond (as by percussive welding) between a plurality of needles and their respective wires prior to each wire feeding operation. Moreover, the danger of damaging the cores with such needles tends to increase as the core size decreases. Making the wires out of material that is inherently rigid or stiff would be one way of eliminating the use of needles, but such a proposal has very limited utility because in most cases it is desired that the wire be flexible enough so that it can be fed from a spool or reel into the core assembly.
Magnetic core memory planes often use combination bit-sense wires that are too thick to be threaded through the cores by means of hollow needles. Furthermore, such arrays often are designed so that these wires must be skewed or zigz-agged at certain places in each core plane to provide noise cancellation. Such conditions have made it necessary heretofore to employ skilled and time-consuming hand-wiring operations (using solid needles as above described) for inserting such wires into the array. Mechanization of the entire wiring procedure to eliminate such manual threading operations is considered highly desirable.
A general object of this invention is to expedite the manufacture of apparatus comprising wired assemblies of small, apertured articles by eliminating the necessity for using needles or similar devices to guide. the wires through the apertures in the articles.
Another object is to provide economical means for enabling a large number of thin, flexible wires to be threaded simultaneously through several rows of apertured articles whose holes are too small to permit the passage of hollow needles or similar wire guiding means.
Still another object is to enable the hole diameters 'in apertured magnetic memory elements to be reduced substantially below the minimum diameter which now is considered feasible when the conventional methods for manufacturing such apparatus are employed.
A further object is to expedite the manufacture of magnetic core memories by eliminating the hand-wiring operations which customarily are employed in threading certain of the wires through each core plane assembly and substituting therefor a multiple wire feeding operation by mechanical means.
A still further object is to introduce the desired skews or zigzags in the wiring by a simple mechanical motion instead of requiring a skilled hand threading operation for that purpose.
The invention features a novel method of mechanically pretreating a multiplicity of parallel wires by simultaneously stretching their forward end portions until these portions break, thereby causing the remainder of each wire to have a leading end portion which has been reduced and hardened by the tensile working of the wire in the vicinity of its break point. The hardened end portion on each wire, having a point that resembles the nose of a miniature bullet, then serves as an integral needle for guiding the remainder of the wire into and out of the successive aligned apertures in the cores or other apertured elements as the several wires are fed therethrough. The tensile stressing of the wires also serves to eliminate any ripples or bends in the stressed portions thereof.
Another feature of the invention involves the provision of a novel matrix for supporting the apertured elements while they are being wired, s aid matrix having adjoining fixed and movable portions which can be indexed with respect to each other for thereby skewing certain of the wires that have been threaded through these elements, the skewing action taking place on the lines where the fixed and movable portions of the matrix adjoin.
The foregoing and other objects, features and advantages of the invention will be apparent from the following more particular description of a preferred embodiment of the invention, as illustrated in the accompanying drawings.
In the drawings:
FIG. 1 is a plan view of an exemplary apparatus embodying the invention, said apparatus being utilized in this instance to insert a third set of coordinate wires into a core plane assembly which already contains two other sets of coordinate Wires.
FIG. 2 is a fragmentary, enlarged plan view, partially in section, showing the novel mechanical pretreatment which is given to the wires by the apparatus of FIG. 1
just before said wires are inserted into the core assembly.
FIG. 3 is a partially schematic plan view showing the respective portions of the core supporting matrix in their initial relative position, with the first two sets of coordinate wires positioned in the core assembly.
FIG. 4 is a plan view showing one of the matrix sections displaced relative to the other so as to impart a skew to one of the two sets of wires in the assembly, just before the insertion of the third set of wires therein. Fragmentary portions of the adjacent wire guiding means also are shown in this view.
FIG. 5 is a vertical section along the line 5-5 on FIG. 4.
FIG. 6 is a fragmentary plan view, partially in section, showing the positions of some of the wires in the third coordinate set before the same are inserted into the core assembly.
FIG. 7 is a fragmentary vertical section showing one of the wires in the third set after it has been threaded through the first few cores in its respective row of cores.
FIG. 8 is a fragmentary plan view which shows some of the wires in the third set after they have progressed through the assembly to positions above the skewed portions of the wires in the second set.
As indicated in the drawings, the principles of this invention may be applied very advantageously to the manufacture of core planes (planar core assemblies) which are used in magnetic core memories. This can be done in several ways. Thus, the invention may be utilized for inserting all of the coordinate wires into the core plane by multiple wire inserting operations performed without the use of needles. Even where some of the coordinate wires are inserted by means of hollow needles, however, as is done in the conventional partially mechanized wiring procedure, the invention still may find useful application in eliminating the slow and laborious hand-wiring operations that have been necessary in threading the remaining coordinate wires through the cores according to conventional practice. Not only are such hand-wiring operations intricate and time-consuming, but there is also the danger that the manipulations of the needles may damage the cores or the wiring. These hand-wiring operations have been further complicated by the fact that in the conventional design, those wires which are inserted by hand are also the wires which must be skewed or zigzagged by hand. The present invention simplifies this procedure greatly by making provision for mechanically skewing or zigzagging certain of the wires which have been mechanically inserted into the core plane, thereby providing the desired noise cancelling effect without any hand-wiring operations.
In describing the embodiment of the invention disclosed herein, it is assumed that two of the three sets of coordinate wires employed in the assembly (namely, those sets conventionally designated the X wires and Y wires) already have been inserted into the core Plane by a suitable technique, whether this be a conventional technique as disclosed in United States Patent No. 2,958,126, issued on November 1, 1960 to W. P. Shaw et al., for example, or by some other method such as the one herein disclosed. It will be assumed also (in accordance with conventional practice) that the coordinate wires in the third set, known as the inhibit-sense wires, have diameters such that these wires could not be fed through the cores by means of hollow needles. It is not hereby intended to limit the application of the invention to such a condition, however, for it will be obvious to those skilled in the art that the principle of the invention can be utilized for inserting any or all of the coordinate wires into an assembly of cores or like elements, regardless of whether or not such wires could or could not be inserted by other means.
Referring now to the drawings, FIG. 1 shows the general plan layout of an illustrative apparatus for inserting coordinate wires into a planar assembly of toroidal magnetic cores in accordance with the invention. The principal parts of the apparatus comprise a core sup-porting
unit
10, a wire feeding unit 12 (movable to the left and to the right as viewed in FIG. 1), a wire clamping unit 14 (movable along a transverse path as indicated by the solid-line and broken-line positions thereof in FIG. 1), and a wire receiving unit 16 (movable to the right and to the left as viewed in FIG. 1).
The
core supporting unit
10 has a matrix therein adapted to support the toroidal magnetic cores which are to be threaded by the coordinate wires. This matrix consists of a
stationary section
18 and an adjacent movable section 29, which is capable of being shifted or indexed transversely of the wire path from the position thereof illustrated in FIG. 3 to the position thereof illustrated in FIG. 4, the purpose of this arrangement being described presently. In executing this movement, the
matrix section
20 slides between the
stationary matrix section
18 and another
stationary member
21 on the
core supporting unit
10, as will be described more fully hereinafter.
The
wires
22, FIG. 1, which are to be inserted into the core plane are fed generally from right to left, as viewed in FIG. 1, by the
wire feeding unit
12. During the mechanical pretreatment phase of the wire feeding operation, however, the wires may be pulled to the right, as viewed in FIG. 1, in order to break off their forward end portions which are held by the clamping
unit
14. In performing this wire breaking step, the
wire feeding unit
12 is moved slightly to the right. FIG. 1 shows the
unit
12 in a position intermediate its extreme right-hand and left-hand positions, just prior to the breaking of the wires.
Referring now to FIGS. 1 and 3, the
stationary matrix section
18 and the
movable matrix section
20 are provided with individual core holding recesses 24 (some which are shown in FIG. 7) that are adapted to hold the toroidal cores C in positions to be wired. These
recesses
24 communicate through suction ports as 26, FIG. 7, with an exhaust chamber such as 28 in the
matrix section
18 or 20, as the case may be. The exhaust chamber in each of the
sections
18 and 2t) communicates with a
suction pipe
30, FIG. 1, connected to a suitable air exhausting means (not shown). The suction maintained in the
core receiving apertures
24, FIG. 7, helps to maintain the cores C firmly in place during the subsequent wire inserting operation. This core holding technique is well known and will not be described in further detail herein.
Covers
82 for the
matrix sections
18 and 20 are provided with wire slots as 25, FIGS. 6 and 7, to receive the
wires
34 and 36.
It is assumed herein that the illustrated apparatus is being employed to insert a third set of coordinate
wires
22, FIG. 1, into a core array which already contains two other sets of coordinate wires, the latter respectively comprising the
X wires
34 and the
Y wires
36, FIG. 3. As mentioned hereinabove, conventional means may be employed for threading the coordinate
wires
34 and 36, respectively, through the cores C, if the holes in these cores are large enough to accommodate the hollow needles that are used for guiding the
wires
34 and 36 in conventional practice. However, the principles of the present invention have been extended to the threading of these X and Y wires, too, thereby eliminating all conventional wire threading techniques in the manufacture of core planes. The instant description will be concerned specifically with the insertion of the third set of coordinate wires 22 (commonly known as the inhibit-sense wires) into the core plane as an example of the manner in which such wire threading operations can be performed according to the invention. As shown in FIGS. 6, 7 and 8, the
wires
22 are considerably thicker than the
wires
34 and 36 and could not be threaded through the cores C by means of hollow needles. In conventional practice the
wires
22 would be inserted through the cores by hand, using solid needles welded to these wires for guiding the same.
As shown in FIG. 3, the toroidal cores C are positioned diagonally with respect to the X and Y Wires 34- and 36 on which they are strung, as is customary in this type of apparatus. The
wires
34 and 36 are secured at their outer ends to an open, rectangular, supporting
frame
38 of insulating material, FIGS. 3, 4, 5 and 7, which carries individual metallic contact pieces (such as 40, FIGS. 3 and 7, and 42, FIGS. 3 and 4) to which the
respective wires
34 and 36 are individually secured. Thus, the core array, prior to insertion of the third set of coordinate
wires
22 therein, consists of the open,
rectangular frame
38 to which is secured a gridwork of intersecting coordinate
wires
34 and 36 on which the cores C are strung, these cores being positioned at the individual bit storage positions respectively defined by the intersections of the X and Y coordinate
wires
34 and 36. The upper edge portions of the
stationary support members
13 and 21 are appropriately recessed to receive the
core frame member
38, as indicated in FIGS. 5 and 7, and the movable matrix section 241 is suitably recessed to receive said frame member and still permit the requisite sliding movement of the
matrix section
20. If desired, fastening devices such as the
screws
43, FIG. 3, may be utilized for holding the
frame
38 on the
support members
18 and 21 during the wire threading operation herein described.
It has been explained hereinabove that in order to provide the desired noise cancellation effect in a magnetic core memory plane, certain of the wires are skewed or zigzagged at predetermined places in the assembly. Customarily this is done at the time when the sense wires (or the combination inhibit-sense wires, where such are employed) are inserted into the core plane. In accordance with the present method of wiring a core plane, however, the desired skewing is impaired to one of the other sets of coordinate wires (in this instance the
X wires
34, FIGS. 3 and 4) before the third set of
wires
22 is threaded through the array. Such skewing of the
X wires
34 is accompanied very conveniently in the present apparatus by means of the
movable matrix section
20, which is capable of sliding for a limited distance transversely of the direction in which the
wires
34 extend. This will be explained in detail presently.
The partially wired core plane, consisting of the
frame
38, coordinate
wires
34 and 36 and the cores C, appears initially as shown in FIG. 3 (some of the wires and cores being omitted from this view for clarity). The
X wires
34 initially extend in straight lines through the array and are suitably secured at their outer ends to the
individual contact pieces
40 on the ends of the
frame
38. The
Y wires
36 respectively are secured to
individual contact pieces
42 mounted on the sides of the
core frame
38. For reasons which will be explained presently, transverse rows of anchor pins 44 and 46, FIGS. 3, 4 and 5, are provided respectively on adjacent edge portions of the
matrix sections
18 and 2t and similar transverse rows of anchor pins 48 and 5t] respectively are provided on adjacent edge portions of the
matrix section
20 and the
stationary member
21. These
pins
44, 46, 43 and 50 initially help to locate the
wires
34 on the
core supporting unit
10. Subsequently, when the
matrix section
20 is moved from the position thereof shown in FIG. 3 to the position thereof shown in FIG. 4, these pins serve to anchor and support the skewed and unskewed portions of the
wires
34 and to prevent stress from being exerted upon the cores C and upon the joints between the
wires
34 and their
contact pieces
40.
The purpose of skewing the
wires
34, as represented in FIG. 4, is to provide the desired noise cancellation effect in the finished core plane. As mentioned hereinabove, such noise cancelling property customarily is provided by skewing the inhibit-sense wires of the array, but in the present instance it is preferred to accomplish this objective by skewing the X wires and leaving the inhibit-sense wires straight. In order to effect the desired wire skewing action, the
movable matrix section
24 is actuated by a
thumb screw
51, FIGS. 3 and 4, which isthreaded through a tapped opening in a stationary supporting
bracket
54 to bear against one side of the movable matrix section 2t). It is assumed that the
matrix section
20 is provided with suitable motion limiting means (not shown) for accurately locating it in either of its extreme positions. By turning the
knob
52 on the
screw
51, the
matrix section
20 is moved from the position thereof shown in FIG. 3 to the position thereof shown in FIG. 4, during which movement the
pins
46 and 48 thereon bear against the
respective wires
34 and cause them to be skewed as represented in FIG. 4. The portions of the
wires
34 disposed between the
pins
44 and 46, and also between the
pins
48 and 5-0 are stretched without breaking, leaving them with a permanent set so that they maintain the skewed positions thereof shown in FIG. 4 after the completed core plane assembly is removed from the apparatus. In practice the
pins
44, 4-6, 48 and 50 are made retractable in order to facilitate the removal of the core plane from the apparatus upon completion of the wiring operation. The actual amount of indexing movement imparted to the movable matrix secti-on2t} is on the order of .07 inch in a specific model of the illustrated apparatus which has been constructed. The displacement of the
section
20 always will be a whole number of the row spacings between
wires
34.
With the
X wires
34 properly skewed as represented in FIG. 4, the core array now is ready to receive the third set of coordinate wires comprising, in this instance, the inhibit-
sense wires
22, FIG. 1. Before these
wires
22 are inserted into the array, however, their forward end portions thereof are given a mechanical pretreatment, in accordance with the principle of the invention, to provide needle-like leading ends on these
wires
22. As a first step in this pretreatment process, the
wire clamping unit
14 is moved from the broken-line position thereof, FIG. 1, to the position thereof represented by solid lines in FIG. 1, where it is adapted to grip or clamp the
wires
22 near their forward ends. During the pretreatment operation the
wire clamping unit
14 is intermediate the
core supporting unit
10 and the
wire feeding unit
12 as shown in FIG. 1. The
wires
22 extend from a source thereof (not shown) at the right of FIG. 1 and are passed beneath a wire clamping device 60 (presently in its raised position) on the
wire feeding unit
12, thence beneath a
feed roller
62 and finally beneath the raised clamping device 66 on the
wire clamping unit
14. The
feed roller
62 is provided with a hand wheel or
knob
64, FIG. 1, and is positioned between two wire guide members or
housings
68 and 70 mounted on the
wire feeding unit
12. The members 68 and 7% have suitable wire guiding channels or grooves therein, the
channels
72 in the
guide member
70 being clearly shown in FIGS. 2, 6 and 7. Preferably the
members
68 and 70 are made of clear plastic so that the
wires
22 will be visible therethrough.
In performing the mechanical pretreatment, the
wires
22 first are clamped in three places. The forward portions thereof are gripped by the clamping device 66, which is operated by suitable actuating means (not shown). The
feed roller
62 is clamped by an associated clamping means operated by the
handle
76, FIG. 1, causing the
roller
62 to be secured against rotation and pressing it firmly against the
wires
22 beneath it. The means for clamping the
wire feeding roller
62 is not shown in detail, but it is similar to a well-known mechanism for clamping the needle feeding roller in a conventional wire threading machine as shown, for example, in the aforesaid Shaw et al. Patent No. 2,958,126. The third point at which the
wires
22 are clamped is beneath the clamping device 60, FIG. 1, which is operated by a
handle
78. With the
wires
22 firmly gripped by the clamps 60 and 66 and by the clamped
feed roller
62, the mechanical pretreatment of these wires may commence.
Referring to FIGS. 1 and 2, the pretreatment is administered by retracting the
feed unit
12 to the right, as viewed in these figures, until the
wires
22 break as indicated in FIG. 2, leaving the
forward end portion
22a of each wire disconnected from the remainder of its
wire
22. It will be assumed that suitable means are employed for retracting the
feed unit
12 to accomplish such breakage of the
wires
22, the specific means employed not being pertinent to this invention. With the
wires
22 being clamped as indicated in FIG. 1, and with the retracting force being applied gradually by movement of the
feed unit
12, the portions of the
wires
22 intermediate the clamp 66 and the clamped
feed roller
22 will be stretched gradually beyond their elastic limits and then will break at their weakest points. By experiment it has been found that all of the wires will tend to break within a space of less than 2 inches between the clamping
unit
14 and the forward end of the
wire guide housing
70 on the
feed unit
12.
The
wires
22 are made of a suitable material such as copper or copper alloy which tends to harden when subjected to tensile stress beyond its elastic limit. Such tensile working of the material in each of the
wires
22 therefore causes the stressed portion of this wire to be come hard and straight for a substantial distance. Moreover, as each
wire
22 breaks, the leading end on the unbroken remainder of the
wire
22 is reduced to a
miniature bullet nose
80, as shown in FIGS. 2, 6, 7 and 8. Hence, by applying tensile stress to the
wires
22 until the forward portions of 22a thereof are broken away as shown in FIG. 2, the remainder of each
wire
22 is left with a hardened leading end portion terminating in a
pointed nose
80, and this hardened end portion is equivalent to a solid needle integral with the
wire
22 and having a diameter no greater than that of the trailing portion of such wire.
After the
forward end portions
22a have been separated from the remainders of their
respective wires
22 as shown in FlG. 2, the clamping
unit
14 is withdrawn to the broken-line position thereof indicated in FIG. 1. The
handles
76 and 78 then are turned to release the clamping
roller
62 and the clamping device 60, respectively. The
knob
64 is turned sufficiently in the proper direction to retract the pretreated
wires
22 within the
guide member
70 of the
feed unit
12. As indicated in FIG. 2, the
wires
22 break at various points in the gap between the clamping
unit
14 and the
guide member
70, so that the
handle
64 must be turned through a sufiicient angle for retracting the longest protruding length of
wire
22 back within the
guide member
70. The wire supply means (not shown) is assumed to take up the slack when the
wires
22 are thus retracted into the
guide member
70.
After the hardened leading end portions of the
wires
22 have been retracted as just described, and the
clamping unit
12 has been withdrawn from the wire path, the entire
wire feeding unit
12 now is advanced bodily to the left as viewed in FIG. 1, bringing the forward end of the
guide member
70 into proximity with the
stationary matrix section
18, as shown in FIGS. 6 and 7. The
guide member
70 is adapted to overlap a part of the
matrix section
18, extending past the nearest end of the
core frame member
38 to within a short distance of the first column of magnetic cores C on the
matrix section
18.
To assist in holding the cores C in place, a
suitable cover
82, FIGS. 4, 5 and 7, is placed on each of the
matrix sections
18 and 20, each of these
covers
82 having individual recesses in its under surface for receiving the cores C and also being provided with channels or
wire slots
25 therein for receiving the
wires
22 as the latter are fed through the array. With the
wire feeding unit
12 in its extreme left-hand position as viewed in FIGS. 6 and 7, the gap between the
guide member
76 and the
cover
82 is quite small. The
cover
82, like the
guide member
70, may be made of clear plastic in order to facilitate viewing the
wires
22 as they are fed through the core array.
FIG. 6 shows, on an enlarged scale, the leading end portions of the
wires
22 after they have been retracted back into the
guide housing
70 and the
housing
70 has been advanced to within a short distance of the first column of cores C. The
wires
22 are fed into the core plane by turning the
knob
64, FIG. 1, to rotate the
feed roller
62. As the
wires
22 are being fed, the hardened leading end portions of the
wires
22 serve to guide these such parts of the structure as the
guide slots
72, the inner edges of the cores C, and the guide pins such as 44 and 46, FIGS. 6, 7 and 8. The arrangement preferably is such that the greatest distance between successive wire guiding points during the travel of each
wire
22 will be on the order of 0.15 inch. The reduced nose portions on the leading ends of the
wires
22 enhance the self-guiding action afforded by the hardened leading end portions of these wires. FIG. 8 represents the leading end portions of the
wires
22 as they leave the first part of the core plane, which is positioned on the
stationary matrix section
18, and enter the second part of the core plane, positioned on the
movable matrix section
20. It will be noted that the
nose portions
80 of the
wires
22 are not transversely aligned with each other in view of the fact that the
wires
22 usually do not break in corresponding places when these wires are mechanically pretreated as above described.
The
wire receiving unit
16, FIGS. 1 and 4, is adapted to receive the leading ends of the
wires
22 after the same have emerged from the core plane. The
unit
16 includes a guide member or housing 90, preferably made of clear plastic, which is appropriately grooved to receive the
respective wires
22. The
wire receiving unit
16 is movable from a position thereof shown in FIG. 1 to the position thereof schematically represented in FIG. 4, in order to receive the leading wire ends after they pass between $16 final guide pins 59 and out of the core plane assem- Briefly summarizing the operation of the illustrated apparatus, a partially wired core plane, containing the
X wires
34, the
Y wires
36 and the toroidal cores C strung on the intersections thereof, is placed on the
core supporting unit
10 as shown in FIG. 3. The
movable matrix section
20 then is indexed by turning the
knob
52, causing the
matrix section
20 to move from the position thereof shown in FIG. 3 to the position thereof shown in FIG. 4. This displaces those portions of the wires 34- which are disposed on the
matrix section
20 relative to those portions of the same wires which are disposed on the
matrix
18, the amount of displacement being a whole number of the row spaces between
adjacent wires
34. The portions of the
wires
34 disposed between the anchor pins 44 and 46, and between the anchor pins 48 and 50, respectively, are skewed as shown in FIG. 4 so that the final core memory array will have the desired noise cancelling property.
The core plane now is ready to receive the third set of coordinate
wires
22, which are assumed herein to be the inhibit-sense wires of the core plane. However, these
wires
22 first must be pretreated mechanically so that they can be threaded through the cores without the aid of needles. To do this, the forward end portions of the
wires
22 are clamped by the
wire clamping unit
14, FIG. 1, whereupon the
wire feeding unit
12 is retracted to the r ght as viewed in FIG. 1, causing the forward end portlons 22a of the
wires
22 to break off as indicated in FIG. 2. All of these wire breakages occur within the gap that now exists between the
units
12 and 14. The
wire clamping unit
14 now is retracted out of the wire path, while the broken ends of wires held thereby are released and disposed of. The tensile working of the
wires
22 causes the material therein (principally copper) to become hardened, and it also removes any ripples in the end portions of the
wires
22 so that the leading ends of these wires are hard and straight, thereby adapting them to perform a function comparable to that of the solid needles which are employed in the conventional handw1r1ng practice to thread the inhibit-sense wires through the core array. The hardening of the
wires
22 occurs principally in the tensioned portions thereof that are disposed in advance of the clamped
feed roller
62, FIG. 1. However, it is believed that some tensioning and consequent hardening of the material occurs also in the portions of the
wires
22 between the
roller
62 and the wire clamping device 60, inasmuch as the clamped
roller
62 probably does not completely restrain the
wires
22 against movement relative thereto.
After being pretreated as just described, the
wires
22 temporarily are retracted within the guide housing 70 (as indicated in FIG. 6) by rotating the now-released
feed roller
62. The
wires
22 then are brought to a point near the core plane by moving the
wire feeding unit
12 to the position thereof shown in FIGS. 4, and 6, following which these wires are advanced through the core array by turning the
feed roller
62. As illustrated in PEG. 7, the
wires
22 pass above the
wires
34 in parallel relation therewith and cross over the
wires
36 at right angles thereto. Due to the preliminary skewing of the
wires
34, as described above, each
wire
22 will overlie different ones of the
wires
34 in the two sections of the core array that are respectively positioned on the
matrix sections
18 and 20. This is clearly indicated in FIG. 8. After the
wires
22 have advanced through the core plane and into the
Wire receiving unit
16, FIG. 1, they are trimmed by a cutting means (not shown). Following this, the
wires
22 may be bonded to individual contact pieces (not shown) mounted on the
core plane frame
38. Assembly of the core plane with its three sets of coordinate wires now is completed.
The term wire as employed herein is intended to denote a thin, normally flexible filament, especially one made of copper, copper alloy or other suitable material which has the property of becoming relatively hard, rigid or stiff when subjected to a tensile stress beyond its elastic limit. The tensile working of such material which occurs upon stretching and breaking off a portion of the wire tends to straighten any ripples in the wire and conveniently provides it with a needle-like end portion which is relatively hard or stiff for a substantial distance back of the breakage point. After receiving such pretreatment, the wire can readily be fed by a roller through the aligned holes in a row of toroidal cores in the array, the hardened leading portion of the wire being of sufiicient length to bridge the greatest distance between successive wire guiding points in the path of the wire and to maintain the desired direction thereof, from the
feeding unit
12 to the receiving unit 1.6. Wires having a diameter as small as 0.0022 inch (No. 44 wfre) have been successfully used in accordance with the disclosed method.
This invention makes it feasible to insert all of the coordinate conductors into a magnetic core plane by mechanized, multiple Wire threading operations, thereby eliminating the slow handwiring techniques that must otherwise be employed. The instant method also eliminates the damage that may be caused to the cores or to the wiring of the array by unskillful hand threading. It furthermore enables the core memory designer to choose which set of coordinate wires will be skewed to provide the desired noise cancelling effect, rather than limiting this choice to one particular set of wires, the only re quirement now being that the set of wires to be skewed must be inserted into the plane before the superposed set of straight wires (if any) is inserted.
To practice the present novel method of inserting coordinate wires into a planar assembly of apertured articles,
one is not necessarily limited to the specific type of apparatus herein disclosed. In an experimental model of this invention adapted to operate on the same principle, but without the refinements of the later improved design, good results were obtained by using a conventional needle and wire feeding apparatus of the type disclosed in the above-mentioned Patent No. 2,958,126, such apparatus being modified only to the extent of enabling the forward ends of a set of wires to be clamped for pretreatment purposes before such wires enter the core plane rather than being clamped after leaving the core plane as dis closed in said patent. In the particular adaptation just described, all of the feed rollers cooperated directly with the wires, since no needles were used when feeding the mechanically pretreated wires.
While the invention has been particularly shown and 10 described with reference to a preferred embodiment thereof, it will be understood by those skilled in the art that changes in form and details may be made therein without departing from the spirit and scope of the invention.
What is claimed is:
1. A method of threading a row of aligned apertured articles with a wire made of material that normally is flexible but which is capable of being hardened by the application thereto of tensile stress in excess of its elastic limit, said method comprising the steps of subjecting a leading portion of the wire to tension which causes the material in said portion of the wire to be stressed in excess of its elastic limit, thereby hardening the stressed material in a substantial length of the wire extending from the leading end thereof, and feeding the wire through the aligned apertures in said row of apertured articles in such. manner that the hardened leading portion of the wire maintains the wire in the desired direction as it ruoves through said row of articles. 2. A method of threading a row of aligned apertured articles with a wire made of material that normally is flexible but which is capable of being hardened by the application thereto of tensile stress in excess of its elastic limit, said method comprising the steps of subjecting an end portion of the wire to a tensile stress which causes a forward part thereof to break away from the remainder of the wire, thereby causing the stressed material in a leading end portion of said remainder to be hardened for a substantial length of the wire behind the point of breakage, and
feeding said remainder of the wire through the aligned apertures in said row of apertured articles in such manner that the hardened leading portion of the wire maintains the desired direction of the wire as it moves through said row of articles.
3. A method of threading a wire of cupreous materialthrough a substantiaily straight guide path at least part of which is defined by a succession of spaced apertured articles having their apertures aligned on said path, said method comprising the steps of applying to said wire tensile stress sufiicient to harden the cupreous material in a leading portion of the wire the length of which is at least equal to the maximum distance between successive wire guiding points in said path, and
feeding the wire through said path in such manner that the hardened leading portion of the wire serves to maintain the desired direction of the wire as it passes between successive wire guiding points in said path.
4. A method of threading a wire of cupreous material through a substantially straight guide path at least part of which is defined by a succession of spaced apertured articles having their apertures aligned on said path, said method comprising the steps of applying to said wire tensile stress sulficient to break a forward portion of the wire away from the remainder of the wire and cause the leading end portion of said remainder to become hardened by the tensile working of the cupreous material therein throughout a length of the wire at least equal to the maximum distance between successive wire guiding points in said path, and
feeding said remainder of the wire through said path in such manner that the hardened leading portion thereof serves to maintain the desired direction of the wire as it passes between successive wire guiding points on said path.
5. A method of threading a row of aligned apertured articles with a wire made of material that normally is flexible but which is capable of being hardened by the application thereto of tensile stress in excess of its elastic limit, said method comprising the steps of subjecting an end portion of the wire to a tensile stress which causes a forward part thereof to break away 1 i from the remainder of the wire, thereby reducing the wire in the vicinity of the break to form a substantially pointed end on said remainder and causing the leading portion of said remainder to be hardened for a substantial length behind said pointed end thereof, and feeding said remainder of the wire through the aligned apertures in said row of ape-rtured articles in such manner that the hardened leading portion of the wire maintains the desired direction of the wire as it moves through said row of articles. 6. A method of threading a wire of cupreous material through a substantially straight guide path at least part of which is defined by a succession of spaced apertured articles having their apertures aligned on said path, said method comprising the steps of applying to said wire tensile stress sufficient to break a forward portion of the wire away from the remainder of the wire, thereby reducing the wire in the vicinity of the break to form a substantially pointed end of said remainder and causing the leading portion of said remainder to be hardened for a substantial length behind said pointed end thereof, and
feeding said remainder of the wire through said path in such manner that the hardened leading portion thereof serves to maintain the desired direction of the Wire as it passes between successive wire guiding points on said path.
7. A method of threading a row of aligned apertured articles with a wire made of material that normally is flexible but which is capable of being hardened by the application thereto of tensile stress in excess of its elastic limit, said method comprising the steps of longitudinally moving the wire in a forward direction to a postion near the row of apertured articles, restraining a forward portion of the wire against further movement,
longitudinally moving the remainder of the Wire in a reverse direction to stretch it and break it away from the restrained forward portion thereof, thereby causing a leading portion of said remainder to be reduced and hardened by the tensile working of the material therein,
removing the broken forward portion of the wire, and
longitudinally moving the remainder of the wire forwardly through the row of apertured articles in such manner that the hardened leading portion thereof maintains the desired direction of the wire as it moves through the aligned apertures in said articles.
8. A method of threading a wire of cupreous material through a substantially straight guide path at least part of which is defined by a succession of spaced apertured articles having their apertures aligned on said path, said method comprising the steps of longitudinally moving the wire in a forward direction to a position near the row of apertured articles, restraining a forward portion of the wire against further movement,
longitudinally moving an adjoining portion of the wire in a reverse direction to stretch it and break it away from the restrained forward portion thereof, thereby causing the stretched portion of the wire to be hardened by the tensile working of the cupreous material therein for a distance at least equal to the maximum distance between successive wire guiding points in said path,
removing the broken forward portion of the wire, and
longitudinally moving the remainder of the wire forwardly through the row of apertured articles with the hardened portion thereof in the lead for maintaining the desired direction of the wire as it passes through the aligned apertures in said articles.
9. A method of simultaneously threading several parallel rows of aligned apertured articles with wires each made of a material that normally is flexible but which is capable 12 of being hardened by the application thereto of tensile stress in excess of its elastic limit, said method comprising the steps of simultaneously subjectin the leading portions of the several wires to tension which causes the material in the leading portion of each wire to be stressed in excess of its elastic limit, thereby hardening the stressed material in a substantial length of the wire extending from the leading end thereof, and simultaneously feeding the wires respectively through said rows of apertured articles in such manner that the hardened leading portion of each wire maintains the wire in the desired direction as it moves through its row of articles. in. A method of simultaneously threading a plurality of wires of cupreous material respectively through a plurality of parallel guide paths each defined in part 'by a succession of spaced apertured articles aligned on the respective path, said method comprising the steps of simultaneously applying to said wires tensile stress suificient to harden the cupreous material in a leading portion of each wire, the length of such leading portion being at least equal to the maximum distance between successive wire guiding points in the respective one of said paths, and feeding the wires simultaneously through said paths in such manner that the hardened leading portion of each wire serves to maintain the desired direction of the wire as it passes between successive wire guiding points in its respective path. fl. A method of threading a plurality of parallel rows of apertured articles respectively with wires made of material that normally is flexible but which is capable of being hardened by the application thereto of tensile stress in excess of its elastic limit, said method comprising the steps of longitudinally moving the wires simultaneously in a forward direction to positions near the respective rows of apertured articles, simultaneously restraining the forward portions of the respective wires against movement, longitudinally moving the adjoining unrestrained portions of the respective wires simulatneously in a reverse direction to stretch them and break them away from the restrained forward portions thereof, thereby causing the leading portion of the remainder of each wi e to be reduced and hardened by the tensile working of the material therein, removing the broken forward portions of the wires, and longitudinally moving the remainders of the respective wires forwardly simultaneously through the rows of apertured articles in such manner that the hardened leading portion of each Wire maintains the desired direction of such wire as it moves through the aligned apertures in its respective row of articles. 12. A method of threading a plurality of wires of cupreous material respectively through substantially parallel guide paths each defined in part by a succession of spaced apertured articles aligned on the respective path, said method comprising the steps of longitudinally moving the wires simultaneously in a forward direction to positions near the respective rows of apertured articles, simultaneously restraining the forward portions of the respective wires against movement, longitudinally moving the adjoining unrestrained portions of the respective wires simultaneously in a reverse direction to stretch them and break them away from the restrained forward portions thereof, thereby causing the stretched portion of each wire to be hardened by the tensile working of the cupreous material therein for a distance at least equal to the maximum distance between successive wire guiding points in its respective path,
removing the broken forward portions of the wires,
and longitudinally moving the remainders of the respective wires forwardly simultaneously through the rows of apertured articles with the hardened portion of each wire being in the lead to maintain the desired direction of the wire as it passes through the aligned articles in its path. 13. In the manufacture of a magnetic core memory plane which contains rows and columns of magnetic cores threaded =by sets of coordinate wires, the wires in one of said sets extending generally parallel to the wires in another of said sets through the several rows of cores in said plane, a method of producing a partially offset relationship between the wires of said one set and the wires of said other set to provide for noise cancellation in the completed core plane, said method comprising the steps of shifting the position of one group of magnetic cores in said plane relative to the position of another group of magnetic cores in said plane through a limited distance equal to a whole number of row spacings transversely of the general direction in which said one set of wires extends, thereby causing the portions of those wires threading said one group of cores to be oifset by one or more rows with respect to the portions of the same wires threading the other group of cores in said plane and concurrently imparting a skew to the portions of such wires intermediate the relatively offset portions thereof, and
advancing the wires of said other set along substantially straight paths for threading the same through the newly aligned rows of cores in the relatively shifted groups thereof, whereby the relatively offset portions of each wire in said one set are positioned respectively adjacent to different wires of said other set. 14. A method as set forth in claim 13 wherein the intermediate portions of the wires in said one set are stretched as they are skewed, thereby imparting a set to these skewed intermediate portions.
15. In the manufacture of a magnetic core memory plane which contains rows and columns of magnetic cores threaded by sets of coordinate wires made of cupreous material, the wires in one of said sets extending generally parallel to the wires in another of said sets through the rows of cores in said plane, the fabrication steps comprising shifting the position of one group of magnetic cores in said plane relative to the position of another group of magnetic cores in said plane through a limited distance equal to a whole number of row spacings transversely of the general direction in which said one set of wires extends, thereby causing the portions of those wires threading said one group of cores to be offset by one or more rows with respect to the portions of the same wires threading the other group of cores in said plane and concurrently imparting a skew to the portions of such wires intermediate the relatively offset portions thereof,
advancing the wires of said other set from outside said core plane to a position near the respective rows of cores in one of said groups of cores,
restraining the forward end portions of said other wires against movement,
momentarily imparting a reverse movement to the adjoining portions of said other wires to stretch and break said other wires near the forward ends thereof, thereby to produce hardened leading ends on said other wires due to the tensile working of the cupreous material therein,
removing the broken forward ends of said other wires,
and
advancing the remaining portions of said other wires along substantially straight paths through the aligned rows of cores in the relatively shifted groups thereof, with the hardened leading ends of said other wires serving to maintain the straight directions of these wires between successive guide points in said paths, whereby each of said other wires eventually is positioned adjacent to different. wires of said one set in the respective groups of cores. 16. Apparatus for causing an alignment of apertured articles to be threaded with 'a wire made of material that normally is flexible but which is capable of being hardened by the application of tensile stress thereto beyond its elastic limit, said apparatus comprising means for applying longitudinal stresses in opposite directions respectively to adjoining portions of the wire, thereby to break a forward portion of the wire away from the remainder of the wire and leave said remainder with a hardened leading portion, and
means for longitudinally advancing said remainder of the wire through said apertured articles with the hardened leading portion thereof being directed along the line of apertures therein.
1'7. Apparatus for threading a row of aligned apertured articles with a wire made of material that normally is flexible but which is capable of being hardened by the application of tensile stress thereto beyond its elastic limit, said apparatus comprising means for applying to a forward portion of the wire tensile stress sufficient to break the wire, thereby producing a hardened leading end portion on the remainder of the wire,
means for feeding the wire with its hardened leading end through the aligned apertures in the row of apertured articles, and
guide means for giving at least partial guidance to the wire as the same is fed through the row of apertured articles,
18. Apparatus for threading a wire of cupreous material through a substantially straight guide path at least part of which is defined by a succession of spaced apertured articles having their apertures aligned on said path, said apparatus comprising means for applying to said wire tensile stress sufiicient to break a forward portion of the wire away from the remainder of the wire and cause the leading end portion of said remainder to become hardened by the tensile working of the cupreous material therein throughout a length of the wire at least equal to the maximum distance between successive wire guiding points in said path, and
feeding means for longitudinally advancing said remainder of the wire through said path in such manner that the hardened leading portion thereof serves to maintain the desired direction of the wire as it passes between successive wire guiding points on said path.
19. Apparatus for threading a wire of cupreous material through a substantially straight wire guiding path including a succession of spaced apertured articles having their apertures aligned on said path, said apparatus comprising feeding means for longitudinally moving the wire along said path,
first clamping means for clamping a forward portion of the wire at a point intermediate the apertured articles and said feeding means, and
second clamping means for causing the wire to be clamped at a point substantially spaced from the point at which the wire is clamped by said first clamping means,
said first and second clamping means being relatively movable for causing the wire to be stretched and broken between them and being so spaced from each other that the main portion of the Wire is hardened by the application of the tensile stress thereto for a distance at least equal to the maximum distance between successive wire guiding points in said path, said feeding means being adapted to feed the wire along said path through the aligned apertures in said articles with the hardened part thereof in the lead for maintaining the desired direction of the wire as it passes through the successive apertures in the articles. 20. Apparatus for threading a wire of cupreous material through a substantially straight wire guiding path which includes a succession of spaced apertured articles having their apertures aligned on said path, said apparatus comprising feeding means including a feed roller engaged with said wire and normally rotatable for longitudinally moving the wire along said path, first clamping means for clamping a forward portion of the wire at a point intermediate the apertured articles and said feeding means, second clamping means for restraining rotation of said feed roller and thereby causing the wire to be clamped by said roller at a point longitudinally spaced from the point at which the wire is clamped by said first clamping means, third clamping means for clamping the wire at a point still further spaced from said first clamping means, and means for bodily moving said feed roller and said second and third clamping means away from said first clamping means to stretch and break the wire between said first and second clamping means, thereby causing the wire to become hardened by the tensile working of the cupreous material therein for a substantial distance from the point of breakage, said feeding means being effective upon release of said second and third clamping means for feeding the unbroken remainder of the Wire along said path through said apertured articles with the hardened portion of the wire in the lead for maintaining the desired direction of the wire as it passes through said articles. 21. Apparatus for threading a plurality of parallel rows of apertured articles respectively with wires made of a material that normally is flexible but which is capable of being hardened by the application thereto of tensile stress in excess of its elastic limit, said apparatus comprising means for subjecting the end portions of the respective wire simultaneously to tensile stresses which cause the material in such end portions to be hardened by the tensile working thereof, and means for simultaneously feeding the Wires respectively through said rows of apertured articles with the hardened end portions thereof in the lead for maintaining the desired directions of the wires as they advance.
22. Apparatus for threading parallel rows of apertured articles respectively with wires made of material that normally is flexible but which is capable of being hardened by the application thereto of tensile stress in excess of its elastic limit, said apparatus comprising means for subjecting the end portions of the wires simultaneously to tensile stresses which cause the forward parts of the wires to break away from the remainders of the wires, thereby causing the stressed material in the leading portion of the remainder of each wire to be hardened for a substantial distance from the point of breakage, and
means for simultaneously feeding the remainders of the Wires respectively through the rows of apertured articles with the hardened leading port-ions of these wires serving to maintain them in the desired directions as they pass through said articles.
23. Apparatus for threading wires of cupreous material respectively through parallel rows of apertured articles, comprising means for simultaneously applying to the forward portions of the respective wires longitudinal stresses in opposite directions for breaking the wires and thereby providing the remainder of each wire with a hardened leading portion terminating in a substantially pointed end, and
means for simultaneously feeding these wires respectively through the rows of apertured articles with the hardened leading ends of such wires serving to maintain them in the desired directions as they pass through the apertured articles.
24. Apparatus for threading parallel rows of apertured articles respectively with wires made of a material that normally is flexible but is capable of being hardened by the application of tensile stress thereto beyond its elastic limit, said apparatus comprising means for simultaneously applying to the forward portions of the wires tensile stress sufficient to break such portions away from the remainders of the respective wires, thereby producing a hardened end portion on the remainder of each wire,
means for simultaneously feeding the wires with their hardened end portions in the lead through the aligned apertures in the respective rows of apertured articles, and
guide means effective in cooperation with said apertured articles for guiding the respective wires as they advance through the respective rows of apertured articles, the hardened portion of each wire being at least equal in length to the maximum distance between successive guide points in its path.
25. In an apparatus for threading parallel rows of apertured articles respectively with wires of cupreous material, the combination of a supporting unit for holding the rows of apertured articles in positions to be threaded 'by the wires,
a movable member adapted to be moved toward or away from said supporting unit along a path parallel with the direction in which the rows of apertured articles extend, said member also being adapted to remain in a fixed position when desired,
rotatable wire feeding means mounted on said movable member and operable to feed a plurality of wires simultaneously along paths respectively aligned with the rows of apertured articles,
a wire clamping device movable into and out of the paths of the wires between said supporting unit and said movable member, said device being operable to grip the forward end portions of the respective wires and hold the same stationary, and
a second wire clamping device mounted on said movable member for gripping the wires and substantially preventing movement thereof relative to said movable member,
said movable member being operable when both of said wire clamping devices are engaged with the wires to impart reverse movement to the wires for stretching and breaking the same at points intermediate said first clamping device and said feeding means, thereby causing the cupreous material in the leading portions of the remaining lengths of wire to become hardened by the tensile working thereof prior to being advanced by said feeding means through the respective rows of apertured articles.
26. An apparatus as set forth in
claim
25 including means for preventing rotation of said rotatable wire feeding means while said movable member is being operated to stretch and break the wires as aforesaid, thereby enabling said wire feeding means to exert a temporary clamping action upon the wires.
27. Apparatus for simultaneously threading wires of cupreous material through parallel rows of toroidal magetic cores in a magnetic core plane comprising core supporting means for holding the cores of the plane in positions to be Wired,
a movable member adapted to be moved toward or away from said core supporting means along a path parallel with the direction in which the rows of cores extend, said member also being adapted to remain in a fixed position when desired,
a feed roller on said movable member rotatable to feed a plurality of wires simultaneously along wire paths respectively aligned with the rows of cores,
wire guiding means carried by said movable member for guiding the wires fed by said feed roller along said wire paths,
a first wire clamping device movable into and out of the wire paths between said core supporting means and said movable member and operable to grip the forward end portions of the wires to prevent movement thereof, and
a second wire clamping device carried by said movable member operable to engage the wires and substantially prevent movement thereof relative to said movable member,
said movable member being capable of retrograde movement for stretching the portions of the wires intermediate said wire clamping devices sufliciently to break said wires at points between said first Wire clamping device and said feed roller, thereby caus ing the cupreous material in the unbroken leading portions of the wire to become hardened by the tensile working thereof prior to being advanced by said feed roller through the respective rows of cores positioned on said core supporting means.
28. Apparatus as set forth in claim 27 including restraining means operable to prevent rotation of said feed roller while the wires are being stretched and broken and thereafter operable to release said feed roller so that the same may be rotated for retracting the hardened leading portions of the wires within said wire guiding means,
said movable member thereupon being operable to advance said wire guiding means into proximity with the rows of cores which are to receive the respective wires fed by said roller.
29. In an apparatus for manufacturing a magnetic core memory plane assembly containing rows and columns of toroidal magnetic cores threaded by sets of coordinate wires, the wires of one set extending generally parallel to the wires of another set through the rows of cores in said assembly, the combination comprising a supporting unit for supporting two groups of cores in coplanar relationship, said unit including a stationary section having a portion thereof adapted to support one of said groups of cores, and
a movable section for supporting the other of said groups of cores, said latter section being movable transversely of said core rows between predetermined positions respectively defining different alignments of the rows in said two groups of cores,
means for shifting the position of said movable section from one predetermined position thereof to the other predetermined position thereof while said cores are threaded by said one set of coordiate wires, thereby causing the portions of those wires threading said one group of cores to be offset by one or more rows relative to the portions of those same wires threading said other group of cores, and
wire feeding means for passing the wires of said other set along substantially straight paths through the newly aligned rows of cores in the relatively shifted groups thereof, whereby the relatively offset portions of each wire in said one set are respectively positioned adjacent to different wires of said other set for providing the core plane assembly with a desired noise cancelling property.
31 In an apparatus for manufacturing a magnetic core memory plane assembly containing rows and columns of toroidal magnetic cores threaded by sets of coordinate wires, the wires of one set extending generally parallel to the wires of another set through the rows of cores in said assembly and being secured at opposite ends thereof to fixed portions of said assembly, the combination comprising a supporting unit for supporting two groups of cores in coplanar relationship, said unit including a stationary section having a portion thereof adapted to support one of said groups of cores, and a movable section for supporting the other of said groups of cores, said latter section being mova-ble transversely of said core rows between predetermined positions respectively defining different alignments of the rows in said two groups of cores, means for shifting the position of said movable section from one predetermined position thereof to the other predetermined position thereof while said cores are threaded by said one set of coordinate wires, thereby causing the portions of those wires threading said one group of cores to be offset by one or more rows relative to the portions of those same wires threading said other group of cores and concurrently imparting a skew to those portions of such wires intermediate the relatively offset portions thereof,
sets of pins respectively positioned on the different sections of said supporting unit to apply bending and tensile stresses to said intermediate portions of the wires in said one set as said movable section is shifted, thereby preventing any substantial stress from being exerted upon the cores by such wires while they are being skewed and concentrating the resultant strain upon the skewed portions of these wires,
wire feeding means for passing the wires of said other set along substantially straight paths through the newly aligned rows of cores in the relatively shifted groups thereof, whereby the relatively offset portions of each wire in said one set are respectively positioned adjacent to different wires of said other set for providing the core plane assembly with a desired noise cancelling property.
References Cited by the Examiner UNITED STATES PATENTS 2,797,608 7/1957 Huyett 29-203 X 2,958,126 11/1960 Shaw et a1. 29-433 3,031,649 4/1962 Snyder et al 340174 3,111,651 11/1963 Foulkes 29-155.5 X 3,117,368 1/1964 Bartik 29-45556 3,134,635 5/1964 Luhn 29-205 X JOHN F. CAMPBELL, Primary Examiner, THOMAS I -I. EAGER, Examiner,