US45567A - Improvement in sabots for projectiles for rifled ordnance - Google Patents
Improvement in sabots for projectiles for rifled ordnance Download PDFInfo
- Publication number
- US45567A US45567A US45567DA US45567A US 45567 A US45567 A US 45567A US 45567D A US45567D A US 45567DA US 45567 A US45567 A US 45567A
- Authority
- US
- United States
- Prior art keywords
- projectiles
- disk
- sabots
- improvement
- shell
- 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
- 238000010276 construction Methods 0.000 description 6
- 239000007789 gas Substances 0.000 description 6
- 239000002360 explosive Substances 0.000 description 4
- 239000000314 lubricant Substances 0.000 description 4
- 229910001369 Brass Inorganic materials 0.000 description 2
- 239000010951 brass Substances 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 230000000875 corresponding Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/02—Driving bands; Rotating bands
Definitions
- My present invention consists in a peculiar construction of packing for centering and supporting the shot within the bore, closing the .windage, and (when used in a rifled gun) communicating rotary motion to the'shot.
- I employ a compound packing, consisting, essentially, of (first) an annular l flange tting over a wedge-shaped rabbet at the rear of the shot, so that when driven forward it will close the windage, center the shot within the bore, and support it in this position, and (second) an expansible cup-shaped disk, which by the pressure of the expanding gases will be forced into and made to completely fill the grooves, but relieved of the Weight of the shot by the action of the'annular flange above referred to.
- This flange may be of any desired length longitudinally of the.
- the shot may be so proportioned in relation to the depth and length of the rabbet in which it fits as to be forced into the grooves or not, as preferred, when it has been driven forward to the fullest extent by the action of the expanding gases.
- A may represent the main body of the shell, cast with a chamber ⁇ B, for containing the explosive charge.
- the walls of this chamber are formed with V-shaped spiral grooves C C, to adaptit to break at certain times, and thus produce a larger number of fragments.
- D represents a disk of brass or other ductile metal bolted or otherwise secured to the rear end of the shell.
- This disk may or may not be formed with a central aperture fitting a stem or projection on the back of the shell, as illustrated in Fig. 3, and its central part may, if desired, be covered with a rigid washer, to equally distribute the force of the expanding gases.
- the said disk is of cup form, concave at back, so that near its periphery a space, E, will exist between the disk and the back of the shell. .
- This space is covered by an annular' flange, F, formed upon the disk D, and partially occupying a tapering rabbet, G, on the roar part of the shell A.
- the periphery of the disk D is also provide with a groove, H, as described. in my patent issued October 6, 1863.
- This groove and so much of the rabbet G as is not occupied /y the flange F may be filled with tow, satura ed with any suitable lubricant.
- the purpose and effect of the peculiar spiral grooves withinthe shell have already been sufficiently explained.
- the operation of the packing device is as follows: The firs/t/c plosion of the charge, acting against the/disk D and opposed by the inertia of the shell A, presses the disk forward into the cavity E, and -this, owing tothe concave form of the disk, forces its periphery into close contact with the bore,and causes it to fill the grooves if the piece be riiied. At the same time the annular flange F. being pressed forward on the wedge-shaped rabbet G, is thereby forcibly pressed outward in contact with the bore and into the grooves. The entire periphery of the packing is thus made effective. x This packing may be very securely attached to the shot. It is valuable from its simplicity, cheapness, and effectiveness, both as to closing the windage and taking the rifle-grooves.
- cup-shaped packing-disk D provided C. XV. STAFFORD. with' an annular Hang-e, F, itting upon a Witnesses: Wedge-shaped rabbet, G, as herein described, OOTAvIUs KNIGHT,
Description
` Nima PATENT Prion.
O. IV. STAFFORD, OF NEI/V YORK, N. Y., ASSIGNOR TO AMERICAN PROJ ECTILE' COMPANY, OF SAME PLACE.
IMPROVEMENI IN SABOTS FOR PROJECTILES FCR RIFLED ORDNANCE.
Specification forming part of Letters Patent No. 45,567, dated December 20, 1864.
To all whom, it 10mg/concern.-
Be it known that I, GHARLEs WV. STAFFORD, of the city, county, and State of New York, have invented a certain new and useful AImprovement in Projectiles; and I do declare the following to be a full and exact description of the same, reference being had to the accompanying drawings, making part of this specification, in which- Figure l is a side view of a field-shell, illustrating my invention. Fig. 2 is a rear view of the same. Fig. 3 is a longitudinal section thereof at :c x. Fig. 4 is a transverse section at $1/ QJ- Similar letters of reference indicate corresponding parts in the several figures.
My present invention consists in a peculiar construction of packing for centering and supporting the shot within the bore, closing the .windage, and (when used in a rifled gun) communicating rotary motion to the'shot. For this purpose I employ a compound packing, consisting, essentially, of (first) an annular l flange tting over a wedge-shaped rabbet at the rear of the shot, so that when driven forward it will close the windage, center the shot within the bore, and support it in this position, and (second) an expansible cup-shaped disk, which by the pressure of the expanding gases will be forced into and made to completely fill the grooves, but relieved of the Weight of the shot by the action of the'annular flange above referred to. This flange may be of any desired length longitudinally of the.
shot, and may be so proportioned in relation to the depth and length of the rabbet in which it fits as to be forced into the grooves or not, as preferred, when it has been driven forward to the fullest extent by the action of the expanding gases.
In order that others skilled in the art to which my invention appertains may be enabled to fully understand and use the same, I
will proceed to describe its construction and operations.
A may represent the main body of the shell, cast with a chamber` B, for containing the explosive charge. The walls of this chamber are formed with V-shaped spiral grooves C C, to adaptit to break at certain times, and thus produce a larger number of fragments.
By forming the grooves in spiral and V shape, as explained, the difficulty of construction is lessened by reason of the facility afforded for the withdrawal of the core from the pattern. Grooves in this form are also very effective in their operation.
D represents a disk of brass or other ductile metal bolted or otherwise secured to the rear end of the shell. This disk may or may not be formed with a central aperture fitting a stem or projection on the back of the shell, as illustrated in Fig. 3, and its central part may, if desired, be covered with a rigid washer, to equally distribute the force of the expanding gases. The said disk is of cup form, concave at back, so that near its periphery a space, E, will exist between the disk and the back of the shell. .This space is covered by an annular' flange, F, formed upon the disk D, and partially occupying a tapering rabbet, G, on the roar part of the shell A. The periphery of the disk D is also provide with a groove, H, as described. in my patent issued October 6, 1863. This groove and so much of the rabbet G as is not occupied /y the flange F may be filled with tow, satura ed with any suitable lubricant. The purpose and effect of the peculiar spiral grooves withinthe shell have already been sufficiently explained.
The operation of the packing device is as follows: The firs/t/c plosion of the charge, acting against the/disk D and opposed by the inertia of the shell A, presses the disk forward into the cavity E, and -this, owing tothe concave form of the disk, forces its periphery into close contact with the bore,and causes it to fill the grooves if the piece be riiied. At the same time the annular flange F. being pressed forward on the wedge-shaped rabbet G, is thereby forcibly pressed outward in contact with the bore and into the grooves. The entire periphery of the packing is thus made effective. x This packing may be very securely attached to the shot. It is valuable from its simplicity, cheapness, and effectiveness, both as to closing the windage and taking the rifle-grooves.
It provides two spaces for lubricants, and is expanded radially by two causes-to wit: the oblique position or concave form of the disk and the wedge shape of the end of the shell over which it is driven.
Having thus described my invention, what The above speeiiozttion of my improvement I Claim as new therein, and desire to secure in explosive shells signed this 26th day of by Letters Patent, is- September, 1863.
The cup-shaped packing-disk D, provided C. XV. STAFFORD. with' an annular Hang-e, F, itting upon a Witnesses: Wedge-shaped rabbet, G, as herein described, OOTAvIUs KNIGHT,
and for the purpose set forth. CHARLES SMITH.
Publications (1)
Publication Number | Publication Date |
---|---|
US45567A true US45567A (en) | 1864-12-20 |
Family
ID=2115127
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US45567D Expired - Lifetime US45567A (en) | Improvement in sabots for projectiles for rifled ordnance |
Country Status (1)
Country | Link |
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US (1) | US45567A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6363856B1 (en) * | 1999-06-08 | 2002-04-02 | Roscoe R. Stoker, Jr. | Projectile for a small arms cartridge and method for making same |
US20050224631A1 (en) * | 2004-03-05 | 2005-10-13 | The Boeing Company | Mortar shell ring tail and associated method |
-
0
- US US45567D patent/US45567A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6363856B1 (en) * | 1999-06-08 | 2002-04-02 | Roscoe R. Stoker, Jr. | Projectile for a small arms cartridge and method for making same |
US20050224631A1 (en) * | 2004-03-05 | 2005-10-13 | The Boeing Company | Mortar shell ring tail and associated method |
US7262394B2 (en) * | 2004-03-05 | 2007-08-28 | The Boeing Company | Mortar shell ring tail and associated method |
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