US3710430A - Method for optimizing the making of a laminated fibrous strip - Google Patents

Method for optimizing the making of a laminated fibrous strip Download PDF

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US3710430A
US3710430A US00155073A US3710430DA US3710430A US 3710430 A US3710430 A US 3710430A US 00155073 A US00155073 A US 00155073A US 3710430D A US3710430D A US 3710430DA US 3710430 A US3710430 A US 3710430A
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fibers
supporting surface
theta
longitudinal axis
elongated supporting
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US00155073A
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A Long
J Seidel
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CBS Corp
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Westinghouse Electric Corp
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    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H1/00Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres
    • D04H1/70Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres characterised by the method of forming fleeces or layers, e.g. reorientation of fibres
    • D04H1/74Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres characterised by the method of forming fleeces or layers, e.g. reorientation of fibres the fibres being orientated, e.g. in parallel (anisotropic fleeces)
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M4/00Electrodes
    • H01M4/02Electrodes composed of, or comprising, active material
    • H01M4/64Carriers or collectors
    • H01M4/70Carriers or collectors characterised by shape or form
    • H01M4/72Grids
    • H01M4/74Meshes or woven material; Expanded metal
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/10Battery-grid making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/14Shredding metal or metal wool article making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/496Multiperforated metal article making
    • Y10T29/49604Filter
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49801Shaping fiber or fibered material

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Treatment Of Fiber Materials (AREA)
  • Preliminary Treatment Of Fibers (AREA)
  • Processing Of Solid Wastes (AREA)
  • Primary Cells (AREA)

Abstract

A method for preparing a fibrous laminated strip on an elongated supporting surface, using a continuous fiber shredding apparatus having X shredders each cutting and applying P fibers/min., the strip consisting of N laminated layers of shredded metal fibers having a total weight per unit area of W gr./in2, the fibers having a thickness of f1 in., a width of f2 in. and a density of d gr./cu. in., the fibers of each layer being disposed at an orientation angle theta from the longitudinal axis of the supporting surface; the method comprising the steps: (1) forming a layer having a weight per unit area of w gr./in2 by applying P fibers/min. on the elongated supporting surface in a longitudinal direction, the fibers being disposed substantially parallel to each other and at an angle theta of between 15* and 75* from the longitudinal axis of the elongated supporting surface, the fibers being applied to the supporting surface at a traverse speed of Q in./min. and then (2) forming N layers by applying, at a speed Q, additional layers of loose thin metal fibers substantially parallel to each other within a layer, to cover the previous layer at an angle from the longitudinal axis of the elongated supporting surface alternating between theta and theta '' where theta '' theta wherein the following relationship exists: Q X((d)(N)(P)(f2)/(W)(sin theta or theta '')).

Description

United States Patent [191 Long et al.
[ 1 Jan. 16, 1973 [54] METHOD FOR OPTIMIZING THE MAKING OF A LAMINATED FIBROUS STRIP [75] Inventors: Arthur ll. Long, Jeannette; Joseph Seldel, Pittsburgh, both of Pa.
[73] Assignee: Westinghouse Electric Corporation,
Pittsburgh, Pa.
[22] Filed: June 21, 1971 [21] Appl.No.: 155,073
[52] U.S. C1. ..29/419, 29/2, 29/4.5, 29/l63.5 F [51] Int. Cl. ..B23p 17/00 [58] Field of Search .....29/419, 2, 4.5, 4.51, 163.5 F; 83/87, 155
[56] References Cited UNITED STATES PATENTS 932,782 8/1909 Johnson ..29/4.5l 1,605,371 11/1926 Pedersen ....29/4.5l 3,293,965 12/1966 Habicht ..83/87 3,491,636 l/l970 Braun ..83/355 X 3,504,516 4/1970 Sundberg ..29/4.5 X
Primary ExaminerCharles W. Lanham Assistant Examiner-Donald C. Rieley, lIl Attorney-F. Shapoe et a1.
57] ABSTRACT A method forpreparing a fibrous laminated strip on an elongated supporting surface, using a Continuous fiber shredding apparatus having X shredders each cutting and applying P fibers/min, the strip consisting of N laminated layers of shredded metal fibers having a total weight per unit area of W gr./in the fibers having a thickness off in., a width off, in. and a density of d gr./cu. in., the fibers of each layer being disposed at an orientation angle 0 from the longitudinal axis of the supporting surface; the method comprising the steps: (1) forming a layer having a weight per unit area of w gr./in by applying P fibers/min. on the elongated supporting surface in a longitudinal direction, the fibers being disposed substantially parallel to each other and at an angle 0 of between 15 and 75 from the longitudinal axis of the elongated supporting surface, the fibers being applied to the supporting surface at a traverse speed of Q in./min. and then (2) forming N layers by applying, at a speed Q, additional layers of loose thin metal fibers substantially parallel to each other within a layer, to cover the previous layer at an angle from the longitudinal axis of the elongated sup porting surface alternating between 0 and 0' where 6' 0 wherein the following relationship exists:
Q [(d)( )(P)tf,)/( W) (sin a or (9' 6 Claims, 4 Drawing Figures LONGITUDINAL AXIS PAIENIEIIIIII I 6 I975 3.710.430
SHEET 1 [IF 2 l9? Q L l I I I H l3 I4 I40 I I I TFQB 1 i I V I7 I SHREDDERS LONGITUDINAL DIRECTION OF I30 FIBROUS THE BELT SUPPORTING STRIP SURFACE I l l I I I L I j 20) CARRIAGE LONGIITLDINAL AXIS INIVENTORS WITNESSES Arthur H. Long WM/M BY ATTORNEY PATENTEDJAI 1 6 I975 3.710.430
SHEET 2 n? 2 FIG.3.
0 "ON .0.0.0.0.6.0.0.0.0.Q
BACKGROUND OF THE INVENTION This invention relates to a method for producing 5 continuous laminated fibrous structures.
Prior known procedures for making laminated fibrous structures have been dominated by manual operations. I-Ieretofore, metal foil has been shredded by foil shredding machines into fibers which were collected in a suitable container. The fibers were then manually placed on a flat surface and combed" into come semblance of uniform orientation. This would provide a sub-lamination. Other laminations, with fibers extending at angles to the sub-lamination, were than stacked one .upon the other to yield a complete laminate. That procedure has been followed to provide, for example, laminated fibrous plaques for iron-nickel alkaline batteries.
The disadvantages of the manual procedure are well recognized and have created a demand for automatic shredding apparatus whereby a laminate of two or more layers of metal fiber may be produced in a continuous ribbon or strip. Such an automatic apparatus was disclosed in copending patent application Ser. No.
100,683, now US. Pat. No. 3,685,376, assigned to the assignee of this invention. However, optimization of this apparatus is highly desirable to provide a controllable method for providing optimized battery plaques of desired density, high strength and fiber orientation.
SUMMARY OF THE INVENTION In accordance with this invention, an automatic shredding apparatus to provide laminated fibrous plaques can be controlled to produce a given desired fibrous matrix. The apparatus can include a movable belt supporting surface, and at least one metal foil shredder mounted on a movable carriage over the belt and being rotatable through or fixed at an angle 0 from the longitudinal axis of the plane of the belt.
The relationships to provide the optimized laminated fibrous plaques are:
and
Q: Traverse speed (N o. of fibers cut per unit time) (fiber density) T plaque weight per unit area X (No. of fiber layers) (fiber thickness) (fiber width) sin of the angle of fiber orientation BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic plan view of one embodiment of an automatic apparatus for making a continuous strip of laminated metal fibers;
FIG. 2 is a plan view of the metal fibrous strip;
FIG. 3 is an enlarged fragmentary perspective view of the manner in which the metal fibers of the various layers are disposed; and
FIG. 4 is a perspective view of a battery plate as an example of one product for which the laminated fiber metal strip may be used.
DESCRIPTION OF THE PREFERRED EMBODIMENT The method of the present invention prepares an elongated strip of laminated metal fibers to a desired density using an automatic shredding apparatus, by providing the traverse speed and number of layers required. The method comprises the steps of applying on an elongated supporting surface an initial layer of loose, fine discrete metal fibers of known cross section and density disposed substantially parallel to each other, and at an angle 6 of between 15 and from the longitudinal axis of the supporting surface, and then applying at least one other similar layer of fibers on the initial layer and at an angle 0, this angle preferably being in the' opposite direction from the longitudinal axis of the supporting surface and equal to 0. v
One embodiment of a device for performing the foregoing method is shown in FIG. 1. In FIG. 1, an automatic fiber shredding apparatus generally indicated at 10, includes a conveyor belt support 11, a movable carriage generally indicated at 12, and metal foil shredders 13 and 14. The conveyor belt in this embodiment is stationary duringcarriage traverse and is moved a predetermined distance in the direction of arrow 17 at the end of each right carriage traverse and each left carriage traverse. The conveyor belt 11 is disposed around and between a pair of spaced belt support rolls l5 and 16 whereby one or both of the rolls drives the belt in the longitudinal direction of the arrow 17. Thus, the upper portion of the belt provides an elongated movable support surface upon which the metal fiber strip shown as 18 is laid.
The carriage 12 extends between a pair of parallel tracks 19 and 20 which are disposed on opposite sides of the belt 11. The carriage 12 is adapted to traverse longitudinally of the belt 11 in the back and forth direction of the arrow 21. The carriage 12 is provided with means, such as a reversing drive screw for moving the carriage repetitively from one end of the tracks 19 and 20 to the other.
The shredders l3 and 14 each include a cutter head and a metal foil feed roll. The cutter head is a circular member having a plurality of spaced cutting edges extending along the outer surface of the head and from one end to the other. For each full rotation of the head, a fiber for each cutting edge will be produced. The head is mounted between a pair of journals and is driven by a motor and gear box. The foil rolls feed a strip of metal foil into the foil cutting area where the rotating cutting edges cooperate with a shear bar to cut the foil. As a result fibers of metal are dropped upon the belt at a certain rate at spaced intervals depending on the carriage traverse speed.
The metal foil can have a thickness range of from about 0.0005 inch to about 0.0030 inch, preferably about 0.0008 to 0.0015 inches. Each filament or fiber is cut to about 0.0005 to 0.0030 inches, but preferably between about 0.0008 to 0.0015 inches wide and may have a length that is within the confines of the length of the shredder and preferably between 4 to 16 inches. As the fibers are cut by the shredders 13 and 14 they drop onto the belt 1 1 When the carriage 12 moves to the left, the shredders 13 and 14 cut fibers of the metal foil which are deposited onto the belt supporting surface with the fibers from the shredder 13 forming the lowermost layer and the fibers from the shredder 14 being disposed thereon. Accordingly, the lower layer of fibers 23 as shown in FIG. 2, are disposed at an angle from the longitudinal axis of the supporting surface, and the fibers 24 on the next adjacent layer are disposed at an angle 0' on the opposite side of, i.e., in the opposite direction from the longitudinal axis. The fibers are preferably about 0.010 to 0.030 inches apart. As the carriage 12 approaches the end of the tracks 19 and 20, it actuates a limit switch that shuts off the shredder 13. However, the rear shredder l4 continues to operate, dropping fibers 24 on the first layer of fibers 23, until a limit switch is actuated. Thereafter, the shredders 13 and 14 are rotated to alternate positions such as shown by the dotted lines 13a and 14a in FIG. 1. Any suitable means such as a pneumatic cylinder may be provided for rotating the shredders simultaneously. Thus the shredders move between the solid line positions and the broken line positions. The angles of disposition of the shredders, 6 and 0, may vary. The orientation angle alternates, between 6' and 0 where 0 will equal 0', both being an angle of less than 75 to the longitudinal direction of the belt supporting surface. Each angle 'being in an opposite direction from the longitudinal axis of the supporting surface.
Then the carriage 12 moves to the right, whereupon the shredder 14a becomes the lead shredder and the shredder 13a becomes the lagging shredder. As a result, two additional layers of fibers are laid upon the previous layer of fibers 23 and 24. The additional layers include a third layer of fibers '25 and a fourth layer of fibers 26 shown in FIG. 2. The third layer of fibers 25 is laid by the shredder 14a.
Each time the carriage 12 reaches the end of its travel, either to the right or left the shredders are rotated to their alternate positions as set forth above. In addition the belt 11 is advanced in the direction of the arrow 17 through a preset shift. In that manner the carriage with the shredders lay a continuous strip 18 of a fixed given number of layers of fibers. Each time the belt 11 advances a predetermined distance, the lengthof the strip is extended by an increment equal to the distance of advance of the belt.
As shown in FIG. 3, the initial layer 23 of fibers as provided during the first leftward movement of the shredder 13 is at angle 0 from the movement 17 of the belt, with the second layer 24 of fibers, provided by the shredder 14, being disposed thereon and at an angle 2 0, i.e., (0 0') to the fibers of the adjacent first layer but only at an angle 0 from the axis of the belt.
Although the laminated strip 18 may be used for various purposes, a primary use for the strip is that of a plaque or plate for storage batteries. For that purpose the strip 18 may be cut into suitable lengths and sintered to serve as plaques 40 as shown in FIG. 4. The upper and lower edges can be reinforced by metal clips 41 and 42 and an electric contact lug 43 can be provided on the clip 41. Where the plaque 40 is to be used as a positive plate in abattery, it can be filled with oxides and/or hydrated oxides of nickel. Where the plaque 40 is to serve as the negative plate in a battery, it can be filled with a mixture of iron oxides and sulfur.
In our process, using a continuous shredding apparatus, we can sequentially combine operations to produce uniform fiber matrices of given fiber cross-section, weight, thickness, porosity and density using the I equations developed below.
To control the system to produce a given fiber matrix the following relationships were used:
F P/(Q sin 6) 1 where:
F= Number of fibers per normal inch of supporting surface P Shredder speed in revolutions per minute x number of blades per shredder, i.e., fibers/minute Q Traverse speed in inches per minute 0= Shredder orientation where 15 2 6 2 (sin 0 normalizes the value of F., i.e., corrects for the fact that the fibers are not laid normal to the direction of traverse of the supporting surface The weight, w, of a matrix layer is related to the number of fibers per normal inch by the relationship:
w F X f f x d 2 where w weight ofa layer in g/in f F Iber thickness (foil thickness) in inches f Fiber width (shredded width) in inches d Solid foil density in g/in The weight, W, of a matrix of N layers would be:
W=N(FXf,Xf d)g/in 3 The number of layers, N, for a matrix of a given final thickness, was developed empirically using the relationship:
N=(t /f,) (l+e) 4 where:
N Empirical number of layers for the requisite final thickness i Given final plaque thickness in inches e An empirical value approximately 0.20 to obtain the nearest integer of N., i.e., the value e adds about 20 percent to t /f, to compensate for plaque settlement during subsequent sintering to bond the fibers together. The combination of expressions (1 and (3) relates the functions of the three operating components to the matrix weight, fiber cross-section, and the number of fiber layers in the matrix using a single shredder:
P/(Qsin 0)= W/(NXflXf Xd) 5 Q= f1 f2)/s n 6 Equation (6) is a generalized formula. For one layer using one shredder head it becomes:
If X number of shredder heads are used, the generalsurface. The method for obtaining this single layer having the weight w gr/in comprises a single back and forth traversing motion between the shredder and the elongated supporting surface in the direction of the longitudinal axis of the surface at a speed of Q in./min. wherein the following relationship exists:
Q=P(f,Xf Xd)/(wXsin 0) 7 We also provide a method wherein X shredders are used for applying, on an elongated supporting surface, shredded metal fibers to form a matrix of N distinct layers, the matrix having the weight of W gr/in the fibers being shredded by each shredder at the rate of P fibers/min, the fibers having a thickness. of f, in. a width of f in. and a density of d gr/in, the fibers in each layer being disposed substantially parallel to each other and at an angle 0 of between and 75 from the longitudinal axis of the elongated supporting surface. The method of obtaining this matrix having the weight of W gr/in and N layers comprises N traversing motions between the X shredders as a group and the elongated supporting surfaces in the direction of the longitudinal axis of the surface at a speed of Q in/min., the X shredders being grouped along the longitudinal axis of the surface alternately at angles 6 0', which at the end of each traverse, angles 0 and 0' change into angles 6' and 0 respectively, wherein the following relationship exists:
Q=XNP(f Xf- Xd)/(W sin6) 8 and the number of traverses N/X EXAMPLE 1 The system we used in this Example had a single stationary shredder with 18 helical cutting blades, a fixed cutting edge and a foil feeding mechanism. At recommended speeds of between 300 and 700 revolutions per minute, the shredder produced between 5,400 and 12,600 8 inch long fibers per minute. An 8 inch X 72 inch board was used as the supporting surface and was mounted below the stationary shredder on a trolley which provided for an effective reversible horizontal traverse of 48 inches at speeds up to 360 inches per minute. The shredder base swivelled in a horizontal plane to position the shredder at a selected angle, 0, to the traverse direction of the supporting surface, i.e., the longitudinal direction of the belt supporting surface of the fiber matrices to be formed.
The nickel fiber dimensions were 0.001 X 0.00125 X 8 inches. Nickel density was 145.9 gr/in: The required plaque weight was 0.61 gr/in and the required thickness was 0.050 inches. The shredder speed and orientation angle was 510 rpm and 60 to the longitudinal direction of the belt respectively. The number of cutting blades was 18. Using expressions (4), (6) and layers and Since we used only a single shredder X was equal to 1.
A suitable matrix was machine duplicated with a supporting surface traverse speed of 190 in/min. and 60 traverses of the supporting surface. The actual matrix weight was approximately 3 percent below the requisite weight of 0.61 g/in but within the allowed weight tolerance (:5 percent). The 60 layers provided sufficient thickness to obtain a final plaque thickness of 0.050 inches after sintering in a 1,150C furnace to bond the fibers at points of crossover of adjacent layers.
in summary, in this Example we have disclosed a basic approach to a controlled and automated shredding/ laminating process for the production of sintered matrices with long metal fibers. We demonstrated this approach by the construction of-an experimental prototype system for the production of 7 inch wide (8 sin 60) X 36 inch sample plaques with 8 inch long nickel fibers. It is apparent that the three operating components of the prototype can be synchronized into a total system for better product control. It is also apparent that the system can be enlarged and modified, as in the two shredder moveable carriage system, all within the intent of the basic approach, for the production of wider and longer plaques at faster rates and with greater material economy.
The disclosed process does more than duplicate the required weight and requisite final plaque thickness of the manually laminated developmental battery plaques. The controllable geometry of the disclosed matrix offers the machine-laminated plaque, in addition to uniformity, complete control over the plaque porosity, percent plaque density, and the fiber surface. Thus this process offers a greater opportunity for the optimization of the battery plaque in terms of electrical output per weight, and/or surface area. For example, it is apparent from expression (3) that, without changing the plaque weight the plaque porosity can be increased and the percent plaque density can be decreased (by the proportionate increase and decrease of N and F) to provide for improved loading of the active materials.
The disclosed process for laminating fiber matrices with long fibers can be used in other applications requiring controlled porosity such as metallic filters and metallic wicks for heat pipes.
We claim:
1. In the method of preparing a laminated fibrous strip wherein a single layer of shredded metal fibers are applied on an elongated supporting surface, the single layer having the weight of w gr/in the fibers being shredded by a single shredder at the rate of P fibers/min, the fibers having a thickness off, in., a width of f, in. and a density of d gr/in, the fibers being disposed substantially parallel to each other and at an angle 8 of between 15 and from the longitudinal axis of the elongated supporting surface, the improvement comprising the step of moving the shredder over the elongated supporting surface in a single back and forth traversing motion in the direction of the longitudinal axis of the supporting surface at a speed of Q in./min., wherein the following relationship exists:
2. The method of preparing a laminated strip, wherein X shredders are used for applying on an elongated supporting surface shredded metal fibers which define a matrix of N distinct layers, the matrix having the weight of W grlin the fibers being shredded by each shredder at the rate of P fibers/min, the fibers having a thickness of f in., a width of f in. and a density of d grlin the fibers in each layer being disposed substantially parallel to each other and at an angle of between and 75 from the longitudinal axis of the elongated supporting surface, the improvement comprising the steps of moving the X shredders as a group over the elongated supporting surface in N traversing motions in the direction of the longitudinal axis of the supporting surface at a speed of Q in/min., the X shredders being grouped along the longitudinal axis of the surface alternately at angles 6 0', which at the end of each traverse angles 0 and 0' change into angles 6' and 0 respectively, wherein the following relationship exists:
Q= XNP (f (f X d)/( W)(sin 0) and the number of traverses N/X.
3. The method of claim 2 wherein the fiber length is between about 4 to 16 in. the fiber thickness is between about 0.0005 to 0.0030 in. and the fiber width is between about 0.0005 to 0.0030 in.
4. The method of claim 3 wherein the elongated supporting surface is a belt movable in the longitudinal direction and the shredders are not moved in the longitudinal direction.
5. The method of claim 3 wherein the shredders are movable in the longitudinal direction and the supporting surface is not moved in the longitudinal direction.
6. The method of claim 3 wherein fibers of adjacent layers are disposed at an angle in opposite directions from the longitudinal axis of the elongated supporting surface.

Claims (6)

1. In the method of preparing a laminated fibrous strip wherein a single layer of shredded metal fibers are applied on an elongated supporting surface, the single layer having the weight of w gr/in2, the fibers being shredded by a single shredder at the rate of P fibers/min., the fibers having a thickness of f1 in., a width of f2 in. and a density of d gr/in3, the fibers being disposed substantially parallel to each other and at an angle theta of between 15* and 75* from the longitudinal axis of the elongated supporting surface, the improvement comprising the step of moving the shredder over the elongated supporting surface in a single back and forth traversing motion in the direction of the longitudinal axis of the supporting surface at a speed of Q in./min., wherein the following relationship exists: Q P(f1 X f2 X d)/(w sin theta ).
2. The method of preparing a laminated strip, wherein X shredders are used for applying on an elongated supporting surface shredded metal fibers which define a matrix of N distinct layers, the matrix having the weight of W gr/in2, the fibers being shredded by each shredder at the rate of P fibers/min., the fibers having a thickness of f1 in., a width of f2 in. and a density of d gr/in3, the fibers in each layer being disposed substantially parallel to each other and at an angle theta of between 15* and 75* from the longitudinal axis of the elongated supporting surface, the improvement comprising the steps of moving the X shredders as a group over the elongated supporting surface in N traversing motions in the direction of the longitudinal axis of the supporting surface at a speed of Q in/min., the X shredders being grouped along the longitudinal axis of the surface alternately at angles theta theta '', which at the end of each traverse angles theta and theta '' change into angles theta '' and theta respectively, wherein the following relationship exists: Q XNP (f1 X f2 X d)/(W)(sin theta ) and the number of traverses N/X.
3. The method of claim 2 wherein the fiber length is between about 4 to 16 in. the fiber thickness is between about 0.0005 to 0.0030 in. and the fiber width is between about 0.0005 to 0.0030 in.
4. The mEthod of claim 3 wherein the elongated supporting surface is a belt movable in the longitudinal direction and the shredders are not moved in the longitudinal direction.
5. The method of claim 3 wherein the shredders are movable in the longitudinal direction and the supporting surface is not moved in the longitudinal direction.
6. The method of claim 3 wherein fibers of adjacent layers are disposed at an angle in opposite directions from the longitudinal axis of the elongated supporting surface.
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US3798093A (en) * 1970-12-22 1974-03-19 Westinghouse Electric Corp Method of making a laminated fibrous strip
EP0129627A1 (en) * 1983-06-28 1985-01-02 Westinghouse Electric Corporation Method of loading porous fibrous plaques
US6228537B1 (en) * 1997-08-27 2001-05-08 Vb Autobatterie Gmbh Electrode grid for lead batteries
US20090258299A1 (en) * 2005-05-23 2009-10-15 Johnson Controls Technology Company Battery grid
US20100101078A1 (en) * 2007-03-02 2010-04-29 Johnson Controls Technology Company Negative grid for battery
US8252464B2 (en) 1999-07-09 2012-08-28 Johnson Controls Technology Company Method of making a battery grid
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US9130232B2 (en) 2010-03-03 2015-09-08 Johnson Controls Technology Company Battery grids and methods for manufacturing same
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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DE10301646B4 (en) * 2003-01-17 2010-11-04 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Thread or fiber fabric, method and apparatus for its manufacture and fiber reinforced body
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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US932782A (en) * 1907-11-29 1909-08-31 Alfred E Johnson Zinc-lathe.
US1605371A (en) * 1923-03-14 1926-11-02 Arthur Brock Tool & Mfg Works Machine for making metal wool
US3293965A (en) * 1965-08-24 1966-12-27 Emil Hoogland G M B H Apparatus for subdividing and stacking webs of textile materials or the like
US3491636A (en) * 1968-03-15 1970-01-27 Mcfall Co Carey Apparatus for cutting strip material
US3504516A (en) * 1964-08-24 1970-04-07 Brunswick Corp Metal product and method and machine for making same

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US932782A (en) * 1907-11-29 1909-08-31 Alfred E Johnson Zinc-lathe.
US1605371A (en) * 1923-03-14 1926-11-02 Arthur Brock Tool & Mfg Works Machine for making metal wool
US3504516A (en) * 1964-08-24 1970-04-07 Brunswick Corp Metal product and method and machine for making same
US3293965A (en) * 1965-08-24 1966-12-27 Emil Hoogland G M B H Apparatus for subdividing and stacking webs of textile materials or the like
US3491636A (en) * 1968-03-15 1970-01-27 Mcfall Co Carey Apparatus for cutting strip material

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3798093A (en) * 1970-12-22 1974-03-19 Westinghouse Electric Corp Method of making a laminated fibrous strip
EP0129627A1 (en) * 1983-06-28 1985-01-02 Westinghouse Electric Corporation Method of loading porous fibrous plaques
US4519425A (en) * 1983-06-28 1985-05-28 Westinghouse Electric Corp. Control method for loading battery electrodes
US6228537B1 (en) * 1997-08-27 2001-05-08 Vb Autobatterie Gmbh Electrode grid for lead batteries
US8252464B2 (en) 1999-07-09 2012-08-28 Johnson Controls Technology Company Method of making a battery grid
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US11824204B2 (en) 2010-04-14 2023-11-21 Cps Technology Holdings Llc Battery and battery plate assembly with absorbent separator
US10892491B2 (en) 2011-11-03 2021-01-12 CPS Technology Holdings LLP Battery grid with varied corrosion resistance
US11539051B2 (en) 2011-11-03 2022-12-27 Cps Technology Holdings Llc Battery grid with varied corrosion resistance
US10170768B2 (en) 2013-10-08 2019-01-01 Johnson Controls Autobatterie Gmbh & Co. Kgaa Grid assembly for a plate-shaped battery electrode of an electrochemical accumulator battery
US10840515B2 (en) 2013-10-08 2020-11-17 Clarios Germany Gmbh & Co. Kgaa Grid assembly for a plate-shaped battery electrode of an electrochemical accumulator battery
US11611082B2 (en) 2013-10-08 2023-03-21 Clarios Germany Gmbh & Co. Kg Grid assembly for a plate-shaped battery electrode of an electrochemical accumulator battery
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Publication number Publication date
CA959635A (en) 1974-12-24
FR2143212A1 (en) 1973-02-02
FR2143212B1 (en) 1977-12-23
GB1392384A (en) 1975-04-30
DE2229914A1 (en) 1973-01-11

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