Fabricating embedded fragmentation cases for anti-personnel mines
10408589 ยท 2019-09-10
Assignee
Inventors
Cpc classification
Y10T156/1062
GENERAL 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
B32B38/0004
PERFORMING OPERATIONS; TRANSPORTING
Y10T156/1093
GENERAL 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
Y10T156/1002
GENERAL 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
Y10T156/109
GENERAL 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
F41G1/46
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T156/1085
GENERAL 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
F42B12/201
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B33/001
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T156/1322
GENERAL 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
F42B23/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T156/1092
GENERAL 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
Y10T156/1751
GENERAL 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
F42B12/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F42B12/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B23/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B33/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B12/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B38/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method of permanently affixing tungsten cube fragments to the fragmentation warhead in a convex Claymore mine having a plastic case and a housing. Pieces of predetermined sized structural film adhesive are positioned at temperature 60 F.5 F., then pressed into the plastic case while pouring tungsten cubes into the case. The cubes are arranged into desired patterns all at temperature 70 F.2 F. An interface plate and 5 lbs of weight are then placed atop thereof and all are heated in an oven at temperature 205 F.5 F. for four hours for full cure of a desired product.
Claims
1. Method of permanently affixing fragments (105) upon a fragmentation warhead in a convex Claymore matrix (106) having a plastic case and a housing, comprising the steps of: cutting out two (2) pieces of predetermined width and length from a structural film adhesive (104) at temperature 60 F.5 F.; then, positioning and pressing said film adhesive pieces into the plastic case at temperature 70 F.2 F.; then, pouring fragments into the case, at temperature 70 F.2 F.; then, arranging said fragments into the desired pattern while in the case, at temperature 70 F.2 F.; then, pressing the film adhesive pieces into the patterned fragments, at temperature 70 F.2 F.; then, pressing a piece of sheet metal (103) into the film adhesive pieces, at temperature 70 F.2 F.; then, placing an interface plate (102) and 5 lb of weight (101) onto the top of said sheet metal; then, placing all the above assembled items in an oven at temperatures of 205 F.5 F., for four hours, for full cure of the said adhesive pieces in the said Claymore matrix; and, whereupon said fragments have therefore been permanently attached to said Claymore matrix exactly in a desired pattern, and without deforming or degrading of the Claymore matrix housing.
2. The method of claim 1 wherein the fragments are tungsten.
3. The method of claim 1 wherein the fragments are steel.
4. The method of claim 1 wherein the fragments are shaped as balls.
5. The method of claim 1 wherein the fragments are shaped as cubes.
6. The method of claim 1 wherein the fragments are a combination of balls and cubes.
7. The method of claim 1 wherein the structural film adhesive is AF 163-2M with 0.060 WT (weight), color RED.
8. Method of permanently affixing tungsten cube fragments to a fragmentation warhead in a convex Claymore matrix having a plastic case and a housing, comprising the steps of: cutting out two (2) pieces of predetermined width and length of 0.060 WT (weight), AF 163-2M structural film adhesive, at temperature 60 F.5 F.; then, positioning and pressing said film adhesive pieces into the plastic case at temperature 70 F.2 F.; then, pouring tungsten cubes into the case; at temperature 70 F.2 F.; then, arranging said cubes into the desired pattern while in the case, at temperature 70 F.2 F.; then, pressing the film adhesive pieces into the patterned cubes, at temperature 70 F.2 F.; then, pressing a piece of sheet metal into the film adhesive pieces, at temperature 70 F.2 F.; then, placing an interface plate and 5 lb of weight onto the top of said sheet metal; then, placing all the above assembled items in an oven at temperatures of 205 F.5 F., for four hours, for full cure of the said adhesive pieces in the said Claymore matrix; and, whereupon said tungsten cubes have therefore been permanently attached to said Claymore matrix exactly in a desired pattern, and without deforming or degrading of the Claymore matrix housing.
9. The method of claim 1 wherein the quantity of fragments is 700.
Description
DETAILED DESCRIPTION OF THE INVENTION
(1)
(2) A structural adhesive tape which may be used in this invention is product named AF 163-2M with 0.060 WT (weight), color RED, by 3M Company. Ply of structural adhesive can be easily cut into the correct size between 60 F.5 F. to allow for different concept iterations to be prototyped without costly molds. Current methods in this invention utilize an interface plate and weight to keep constant pressure during curing. However, it is conceivable that the interface plate and weight can be replaced with an autoclave or pressure oven. It is noted that light pressure needs to be applied to surface areas being bonded.
(3) The structural adhesive illustrated in
(4) The manufacturing process involves the following steps with their specific processing temperatures.
(5) In a first step, one would cut out two (2) (104) pieces of predetermined width and length from the structural film adhesive at temperature being then 60 F.5 F. The following steps 2-6 are all conducted at temperature being 70 F.2 F. In the second step, one would position and press the film adhesive into the plastic case. In the third step, one would then pour the desired tungsten cubes (105) into the case. In the fourth step, one would then arrange the cubes into the desired pattern while in the case. In the fifth step, one would press the film adhesive into the patterned cubes. In the sixth step, one would press the sheet metal (103) into the film adhesive. In the seventh step, one would place the interface plate (102) and 5 lb of weight (101) onto the top of sheet metal, then cure in an oven at temperatures of 205 F.5 F., for four hours. It can be seen that step 7 involves time and pressure to allow for full cure of the adhesive, without deforming or degrading of the plastic housing. In the result, one has permanently attached tungsten cubes to the plastic case, exactly in a desired pattern, and without the use of epoxy potting or costly and time consuming tooling molds, e.g., as previously needed. These can be used to produce embedded tungsten tiles for fragmentation for various claymore curvatures, geometries and sizes. And, the physical size of the claymore may be reduced while optimizing its lethality nonetheless. In live fire testings, a claymore made by this invention was successfully tested at a 35 meters range showing adequate lethality patterns on witness plates.
OBJECTS OF THE INVENTION
(6) Accordingly, it is an object of the present invention to provide means for fabricating a Claymore mine type matrix without the use of epoxy potting or costly, time consuming tooling molds for instance, according to this invention.
(7) Another object of the present invention is to provide means for permanently affixing fragments into a Claymore mine type matrix.
(8) It is a further object of the present invention to utilize structural film adhesive in the process of fabricating a Claymore type mine to aid in permanently affixing tungsten cubes exactly in a desired pattern according to this invention.
(9) These and other objects, features and advantages of the invention will become more apparent in view of the within detailed descriptions of the invention, the claims, and in light of the following drawings wherein reference numerals may be reused where appropriate to indicate a correspondence between the referenced items. It should be understood that the sizes and shapes of the different components in the figures may not be in exact proportion and are shown here just for visual clarity and for purposes of explanation. It is also to be understood that the specific embodiments of the present invention that have been described herein are merely illustrative of certain applications of the principles of the present invention. It should further be understood that the geometry, compositions, values, and dimensions of the components described herein can be modified within the scope of the invention and are not generally intended to be exclusive. Numerous other modifications can be made when implementing the invention for a particular environment, without departing from the spirit and scope of the invention.
LIST OF FIGURES
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DETAILED DESCRIPTION OF THE INVENTION
(13)