US45567A - Improvement in sabots for projectiles for rifled ordnance - Google Patents

Improvement in sabots for projectiles for rifled ordnance Download PDF

Info

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
Application number
Publication date
Application granted granted Critical
Publication of US45567A publication Critical patent/US45567A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/02Driving 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.
US45567D Improvement in sabots for projectiles for rifled ordnance Expired - Lifetime US45567A (en)

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
US (1) US45567A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
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

Cited By (3)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
US29272A (en) Improvement in projectiles for rifled ordnance
US2856856A (en) Segmented rotating band for artillery projectiles
US34628A (en) Improvement in chain-shot for ordnance
US45567A (en) Improvement in sabots for projectiles for rifled ordnance
US35273A (en) Improvement in wads for ordnance and other fire-arms
US34950A (en) Improvement in expanding sabots for hot shot
US29995A (en) Improvement in bomb-shells
US41668A (en) Improvement in packing projectiles for rifled ordnance
US37661A (en) Improvement in explosive projectiles for ordnance
US36773A (en) Improvement in projectiles for rifled ordnance
US40198A (en) Improvement in incendiary shells
US43835A (en) Improvement in projectiles for rifled ordnance
US22054A (en) Improvement in bomb-lances
US165255A (en) Improvement in projectiles for ordnance
US39427A (en) stafford
US39180A (en) Kviprovement in projectiles
US44660A (en) Improvement in primed metallic catridges
US33100A (en) Improvement in projectiles for rifled ordnance
US34207A (en) Improvement in hot projectiles for ordnance
US33099A (en) Projectile fob rifled ordnance
USRE1098E (en) Improvement in projectiles
US42268A (en) Improvement in packing projectiles for rifled ordnance
US35521A (en) Improvement in explosive shells for ordnance
US38322A (en) Improvement in metal cartridges for cannon
US45079A (en) Improvement in priming metallic cartridges