US2968986A - Method of fabrication of explosive missiles - Google Patents
Method of fabrication of explosive missiles Download PDFInfo
- Publication number
- US2968986A US2968986A US637339A US63733957A US2968986A US 2968986 A US2968986 A US 2968986A US 637339 A US637339 A US 637339A US 63733957 A US63733957 A US 63733957A US 2968986 A US2968986 A US 2968986A
- Authority
- US
- United States
- Prior art keywords
- container
- shell
- braided
- explosive
- fabrication
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000002360 explosive Substances 0.000 title description 13
- 238000004519 manufacturing process Methods 0.000 title description 7
- 239000000463 material Substances 0.000 description 7
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 238000004901 spalling Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 235000009854 Cucurbita moschata Nutrition 0.000 description 2
- 240000001980 Cucurbita pepo Species 0.000 description 2
- 235000009852 Cucurbita pepo Nutrition 0.000 description 2
- 235000020354 squash Nutrition 0.000 description 2
- 230000009172 bursting Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000000452 restraining effect Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21F—WORKING OR PROCESSING OF METAL WIRE
- B21F99/00—Subject matter not provided for in other groups of this subclass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21F—WORKING OR PROCESSING OF METAL WIRE
- B21F45/00—Wire-working in the manufacture of other particular articles
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04C—BRAIDING OR MANUFACTURE OF LACE, INCLUDING BOBBIN-NET OR CARBONISED LACE; BRAIDING MACHINES; BRAID; LACE
- D04C1/00—Braid or lace, e.g. pillow-lace; Processes for the manufacture thereof
- D04C1/06—Braid or lace serving particular purposes
Definitions
- This invention relates to containers and shells, and more particularly to ordnance shells having means for increasing the spalling or squash'on armor.
- An object of the invention is the method of making high explosive containers or shells for withstanding strains and stresses vastly in excess of ordinary containers whose deformations are controlled by the yield stress of the wall material.
- a further object' is the provision of a triple walled high explosive shell utilizing a straining wall to perr'nit lateral deformation and squash eifect upon contact with armor before splitting.
- a further object is the provision of an impervious high explosive shell or container surrounded by a second shell or container constructed to permit a predetermined material lateral expansion or increase in diameter of the shell upon impact of the forward end thereof with an obstruction, such as armor, to increase the spalling effect.
- a further object of the invention is the provision and method of making an explosive shell which comprises utilizing an impervious thin wall inner shell and surrounding the inner shell by a loosely braided intermediate inclosure or container of interwoven metallic strands with the strands disposed on a bias to the longitudinal axis of the inner shell to function as a laterally yieldable restraining container which permits a material increase in diameter and for shortening thereof upon contact of its forward end with an obstruction, such as armor.
- a further object and method is the provision of an outer thin metallic shell spun over the intermediate braided shell or container to force the outer and inner surfaces of the intermediate braided shell into intimate contact respectively with the inner and outer surfaces of the outer and inner shells.
- Figure 1 is a perspective view of one form of inner shell or body.
- Figure '2 is a perspective view of the intermediate bfialved shell or body, before assembling over the inner s
- Figure 3 is a perspective view of the outer shell or body before assembling over the braided intermediate braided and inner shells.
- Figure 4 is a side elevation of the shells and braided container in the process of being assembled.
- Figure 5 is a side elevation of the shells in assembled relation with the outer shell spun or rolled on the inner shell and braided container to bring the inner and outer shells into intimate contact with the braided bias woven intermediate shell.
- reference numerals 1, 2 and 3 denote respectively the inner shell or container, the intermediate braided shell or container, and the outer shell or container.
- the inner container or shell 1 is preferably a thin wall 2,968,986 Patented Jan. 24, 1961 shell or war head open at its rear end to receive a high explosive powder charge and closed at its forward end to provide an impervious container.
- the shape of the inner shell to a great extent governs the shape of the finished shell or war head and can be used to convert all type of missile war heads into high explosiveplastic armament that can utilize the spalling principle to defeat armor.
- the inner shell may be made of thin wall spun metallic material such as aluminum and adapted to split.
- the intermediate container or shell 2 is composed of a fairly loosely braided tubular body having warp and woof strands disposed on a 45 bias to its longitudinal axis.
- .It is a'cylinder of braided wire (somewhat similar to the shielding used on electrical cables) but preferably stronger andheavier and preferably is compressed at right angles to its circular cross section and is slipped or forced over the preformed inner shell 1.
- This comprises a geodetic liner of braided wire which is utilized as a straining wall since this material exhibits the property of substantially stress-free deformation.
- the braided container has the strands thereof disposed on a substantially 45 bias to the longitudinal dimension or axis of the container as shown in Figure 2.
- the outer container 3 is preferably also a thin wall spun aluminum shell which may split longitudinally after extreme deformation of the braided intermediate container 2. As shown in the drawing the outer container is telescoped over the inner shell 1 and the braided container 2 with a snug sliding fit requiring some force, to seat the forward end of the outer container on the forward end of the braided container 2.
- the outer shell 3 After the outer shell 3 has been forced home over the inner shell 1 and intermediate braided container 2 the outer shell 3 is preferably rolled or spun down tight on the braided container 2 to force the inner and outer surfaces respectively of the braided container 2 into intimate contact with the outer and inner surface of the inner and outer containers 1 and 3'.
- the shape of the final shell or container is somewhat optional, depending upon the use to which it is employed,
- the initial shape of the preformed inner thin metallic shell 1 determines substantially the final shape of the finished outer shell.
- the inner shell or liner is first spun out of thin material such as aluminum to form a high explosive container or war head of the desired shape.
- a braided container composed of wire strands woven to dispose the strands on a bias to its longitudinal axis is now slipped over the inner container 1 so as to inclose the inner container within the braided metallic cylindrical container.
- the thin metallic cylindrical container 3 preferably of thin guage aluminum is next fabricated so as to slip snugly over the exterior of the braided container or cylinder 2.
- the outer shell 3 is now spun or rolled down toward the inner shell 1 to force the inner braided surface into intimate contact with the outer surface of the inner shell 1 and simultaneously force the inner surface of the outer shell into intimate contact with the outer surface of the braided container 2.
- the inner shellr may now be loaded with a high explosive and its rear end closed. Upon projection thereof and the'forward end striking an obstruction such as armor or a tank the braided hias woven wire cylindrical container will allow the shell ,to materially expand in diameter'before bursting and thus materially increase the spelling effect on a rmorL Convention detonation means, not shown, for the explosiye chargem ay be employed.
- the method of explosiye missile fabrication to incr'ease'the spallingeffect of the missile on armor comprising, inclosing an inner thin walled elongated cylindrical receptacle adapted to contain an explosive with a loosely braided elongated wire stranded cylindrical intermediate container withthe wire braided strands disposedton a.bias to the longitudinal axis of the inner receptacle and said intermediate container compressed 4 laterally into encircling contact with the outer surface of the inner receptacle, inclosing said intermediate bias braided wire container with; a closely fitting outer thin walled elongated metal receptacle, and spinning said outer receptacle over the length of said intermediate bias woven metallic receptacleuto force the inner surface of the intermediate braided wire container into intimate contact with the outer surface of "the inner receptacle throughout substantially the length thereof and loadns t i e e t t 'en XP1Q Yew
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Textile Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
Jan. 24, 1961 R. J. swlFT ETAL METHOD OF FABRICATION OF EXPLOSIVE MISSILES Filed Jan. 30, 1957 IN V EN TORS wee m snmmj La 4 7 r w a; n 86 am i M w United States Patent 7 2,968,986 METHOD OF FABRICATION on EXPLOSIVE 'MISSILES Filed Jan. '30, 1957, Ser. No. 637,339
1 Claim. CI. 86-20) This invention relates to containers and shells, and more particularly to ordnance shells having means for increasing the spalling or squash'on armor.
An object of the invention is the method of making high explosive containers or shells for withstanding strains and stresses vastly in excess of ordinary containers whose deformations are controlled by the yield stress of the wall material. A further object'is the provision of a triple walled high explosive shell utilizing a straining wall to perr'nit lateral deformation and squash eifect upon contact with armor before splitting.
A further object is the provision of an impervious high explosive shell or container surrounded by a second shell or container constructed to permit a predetermined material lateral expansion or increase in diameter of the shell upon impact of the forward end thereof with an obstruction, such as armor, to increase the spalling effect.
A further object of the invention is the provision and method of making an explosive shell which comprises utilizing an impervious thin wall inner shell and surrounding the inner shell by a loosely braided intermediate inclosure or container of interwoven metallic strands with the strands disposed on a bias to the longitudinal axis of the inner shell to function as a laterally yieldable restraining container which permits a material increase in diameter and for shortening thereof upon contact of its forward end with an obstruction, such as armor.
A further object and method is the provision of an outer thin metallic shell spun over the intermediate braided shell or container to force the outer and inner surfaces of the intermediate braided shell into intimate contact respectively with the inner and outer surfaces of the outer and inner shells.
Other objects and advantages of the invention will become apparent from the following description and accompanying drawings in which like reference characters refer to like parts in the several figures of the drawings.
Figure 1 is a perspective view of one form of inner shell or body.
Figure '2 is a perspective view of the intermediate bfialiiled shell or body, before assembling over the inner s e Figure 3 is a perspective view of the outer shell or body before assembling over the braided intermediate braided and inner shells.
Figure 4 is a side elevation of the shells and braided container in the process of being assembled.
Figure 5 is a side elevation of the shells in assembled relation with the outer shell spun or rolled on the inner shell and braided container to bring the inner and outer shells into intimate contact with the braided bias woven intermediate shell.
In the drawings the reference numerals 1, 2 and 3 denote respectively the inner shell or container, the intermediate braided shell or container, and the outer shell or container.
The inner container or shell 1 is preferably a thin wall 2,968,986 Patented Jan. 24, 1961 shell or war head open at its rear end to receive a high explosive powder charge and closed at its forward end to provide an impervious container. The shape of the inner shell to a great extent governs the shape of the finished shell or war head and can be used to convert all type of missile war heads into high explosiveplastic armament that can utilize the spalling principle to defeat armor. The inner shell may be made of thin wall spun metallic material such as aluminum and adapted to split.
The intermediate container or shell 2 is composed of a fairly loosely braided tubular body having warp and woof strands disposed on a 45 bias to its longitudinal axis. .It is a'cylinder of braided wire (somewhat similar to the shielding used on electrical cables) but preferably stronger andheavier and preferably is compressed at right angles to its circular cross section and is slipped or forced over the preformed inner shell 1.
. This comprises a geodetic liner of braided wire which is utilized as a straining wall since this material exhibits the property of substantially stress-free deformation. Thus if the intermediate container 2 of braided wire is compressed longitudinally by contact at its front end with an obstruction, such as armor, a material increase in diameter (and a decrease in length) will result before rupture, even though the inner and outer thin containers split longitudinally.
The extent of the deformation depends, naturally, on the orientation of one braided strand to the other and the tightness of the woven material before and after compression. As shown, the braided container has the strands thereof disposed on a substantially 45 bias to the longitudinal dimension or axis of the container as shown in Figure 2. The outer container 3 is preferably also a thin wall spun aluminum shell which may split longitudinally after extreme deformation of the braided intermediate container 2. As shown in the drawing the outer container is telescoped over the inner shell 1 and the braided container 2 with a snug sliding fit requiring some force, to seat the forward end of the outer container on the forward end of the braided container 2.
After the outer shell 3 has been forced home over the inner shell 1 and intermediate braided container 2 the outer shell 3 is preferably rolled or spun down tight on the braided container 2 to force the inner and outer surfaces respectively of the braided container 2 into intimate contact with the outer and inner surface of the inner and outer containers 1 and 3'.
The shape of the final shell or container is somewhat optional, depending upon the use to which it is employed,
it may be more streamlined in connection with high explosive ordinance shells than with bombs and some types of missiles. Of course the initial shape of the preformed inner thin metallic shell 1 determines substantially the final shape of the finished outer shell. In the method of making the high explosive shells of the subject invention which have a high yieldable lateral deformation characteristic the inner shell or liner is first spun out of thin material such as aluminum to form a high explosive container or war head of the desired shape.
A braided container composed of wire strands woven to dispose the strands on a bias to its longitudinal axis is now slipped over the inner container 1 so as to inclose the inner container within the braided metallic cylindrical container.
The thin metallic cylindrical container 3 preferably of thin guage aluminum is next fabricated so as to slip snugly over the exterior of the braided container or cylinder 2.
The outer shell 3 is now spun or rolled down toward the inner shell 1 to force the inner braided surface into intimate contact with the outer surface of the inner shell 1 and simultaneously force the inner surface of the outer shell into intimate contact with the outer surface of the braided container 2.
The inner shellrmay now be loaded with a high explosive and its rear end closed. Upon projection thereof and the'forward end striking an obstruction such as armor or a tank the braided hias woven wire cylindrical container will allow the shell ,to materially expand in diameter'before bursting and thus materially increase the spelling effect on a rmorL Convention detonation means, not shown, for the explosiye chargem ay be employed.
'The'aboye description and accompanying drawings are for exemplary, rather than restrictive purposes, and therefore it is evident that those skilled in the art, may vary the details of construction as well as the arrangement of parts without departing from the spirit of the invention'and therefore wedo not wish to be limited to the above disclosure, except asmay, be required by the claims.
[The method of explosiye missile fabrication to incr'ease'the spallingeffect of the missile on armor comprising, inclosing an inner thin walled elongated cylindrical receptacle adapted to contain an explosive with a loosely braided elongated wire stranded cylindrical intermediate container withthe wire braided strands disposedton a.bias to the longitudinal axis of the inner receptacle and said intermediate container compressed 4 laterally into encircling contact with the outer surface of the inner receptacle, inclosing said intermediate bias braided wire container with; a closely fitting outer thin walled elongated metal receptacle, and spinning said outer receptacle over the length of said intermediate bias woven metallic receptacleuto force the inner surface of the intermediate braided wire container into intimate contact with the outer surface of "the inner receptacle throughout substantially the length thereof and loadns t i e e t t 'en XP1Q Yewherby when the missile is projected against arrnor theubiashwoven sleeve will .be expanded transverse, to its longitudinal axis to cause splitting of the thinwalled outer receptacle and increase the spalling effect onthe armor.
References Cited in the file of this patent UNITED STATES PATENTS
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US637339A US2968986A (en) | 1957-01-30 | 1957-01-30 | Method of fabrication of explosive missiles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US637339A US2968986A (en) | 1957-01-30 | 1957-01-30 | Method of fabrication of explosive missiles |
Publications (1)
Publication Number | Publication Date |
---|---|
US2968986A true US2968986A (en) | 1961-01-24 |
Family
ID=24555507
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US637339A Expired - Lifetime US2968986A (en) | 1957-01-30 | 1957-01-30 | Method of fabrication of explosive missiles |
Country Status (1)
Country | Link |
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US (1) | US2968986A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3518942A (en) * | 1960-10-14 | 1970-07-07 | Us Navy | Antiaircraft projectile |
US3960049A (en) * | 1975-03-19 | 1976-06-01 | The United States Of America As Represented By The Secretary Of The Navy | Reinforcement of cast or pressed explosives |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE310061C (en) * | ||||
US34539A (en) * | 1862-02-25 | Improved s-hips armor-plates | ||
US1301380A (en) * | 1917-07-02 | 1919-04-22 | James Frank Buckingham | Incendiary projectile. |
US1376304A (en) * | 1917-06-07 | 1921-04-26 | Zeglen Casimir | Wire-fabric armor-plate |
US2041950A (en) * | 1935-08-05 | 1936-05-26 | Nat Standard Co | Expansible cover |
US2373038A (en) * | 1943-03-03 | 1945-04-03 | American La France Fomaite Cor | Process of making reinforced gas flasks |
GB745078A (en) * | 1952-09-29 | 1956-02-22 | Jose Luis Amilibia Urdapilleta | Improvements in the construction of projectiles |
US2744043A (en) * | 1950-01-23 | 1956-05-01 | Fels & Company | Method of producing pressure containers for fluids |
-
1957
- 1957-01-30 US US637339A patent/US2968986A/en not_active Expired - Lifetime
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE310061C (en) * | ||||
US34539A (en) * | 1862-02-25 | Improved s-hips armor-plates | ||
US1376304A (en) * | 1917-06-07 | 1921-04-26 | Zeglen Casimir | Wire-fabric armor-plate |
US1301380A (en) * | 1917-07-02 | 1919-04-22 | James Frank Buckingham | Incendiary projectile. |
US2041950A (en) * | 1935-08-05 | 1936-05-26 | Nat Standard Co | Expansible cover |
US2373038A (en) * | 1943-03-03 | 1945-04-03 | American La France Fomaite Cor | Process of making reinforced gas flasks |
US2744043A (en) * | 1950-01-23 | 1956-05-01 | Fels & Company | Method of producing pressure containers for fluids |
GB745078A (en) * | 1952-09-29 | 1956-02-22 | Jose Luis Amilibia Urdapilleta | Improvements in the construction of projectiles |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3518942A (en) * | 1960-10-14 | 1970-07-07 | Us Navy | Antiaircraft projectile |
US3960049A (en) * | 1975-03-19 | 1976-06-01 | The United States Of America As Represented By The Secretary Of The Navy | Reinforcement of cast or pressed explosives |
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