US33099A - Projectile fob rifled ordnance - Google Patents
Projectile fob rifled ordnance Download PDFInfo
- Publication number
- US33099A US33099A US33099DA US33099A US 33099 A US33099 A US 33099A US 33099D A US33099D A US 33099DA US 33099 A US33099 A US 33099A
- Authority
- US
- United States
- Prior art keywords
- projectile
- ring
- fob
- rifled
- ordnance
- 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
- 239000002184 metal Substances 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 210000003746 feather Anatomy 0.000 description 4
- 229910001369 Brass Inorganic materials 0.000 description 2
- 239000010951 brass Substances 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
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
- This invention consists in an improved mode of fitting the rear portion of an elongated projectile for rifled ordnance, with a packing-ring of brass or other sufficiently soft metal or alloy, to be upset and expanded laterally and so driven into the grooves of the gun by the force developed by the explosion of the charge of powder.
- Figure l exhibits a side view of the body of the projectile with the ring in section, showing it in the bore of a gun ready to be discharged therefrom.
- Fig. 2 exhibits a rear view of the projectile and a transverse section of the bore of the gun.
- Fig. 3 is a transverse section of the projectile, taken through the ring'in the plane indicated by the line a m of Fig. 1.
- Fig. 4 exhibits a side view of the projectile with the ring in section, showing the ring in the condition it assumes in the discharge of the projectile; and
- Fig. 5 is a rear view corresponding with Fig. 4.
- A is the body of the projectile, which may be made solid or hollow and of cylindro-conoidal or other partly cylindrical form.
- the rear portion is of circular form,
- the groove 0 has two or more small feathers or ribs, 7 f, running across it, parallel or nearly so with the axis of the projectile, said feathers or ribs being formed in the casting of the body.
- B is the packing-ring of brass or other metal or alloy softer than the body of the projectile, cast upon the reduced portion 0 d, by' placing the body of the projectile in a suitable mold and pouring the metal or alloy around it.
- the body of the projectile should'be heated before the casting of the ring upon it, in order to prevent the injury that would result to the ring by its shrinkage upon an unshrinking substance like cold cast-iron.
- the said ring after having cooled is turned or otherwise finished ex-. ternally to correspond in size with the exterior of the cylindrical portion of the body A, as shown in Fig. 1, and its rear end is leftexposed as shown at z i in Figs. 1 and 2, and flush with the base of the body A.
- the packing-ring thus cast on the body of the shell fits very tightly upon the portion V 0 cl, on whichit can neither move lengthwise nor turn, the longitudinal movement beings prevented by the shoulder band the portion d, and the turning being prevented by'the ribs or feathers f f.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Adornments (AREA)
Description
R. P. PARROTT.
Projectile.
Patented Aug. 20, 1861.
STATES PATENT onnion.
ROBERT P. PARROTT,.OF COLD SPRING, NEW YORK.
PROJECTILE FOB RIFLED ORDNANCE.
Specification of Letters Patent No. 33,099, dated August 20, 1861.
To all whom it may concern:
Be it known that 1, ROBERT P. PARROTT, of Cold Spring, in the county of Putnam and State of New York, have invented a new and useful Improvement in Projectiles for Rifled Ordnance; and I do hereby declare that the following is a full, clear, and'exact description of the same, reference being had to the accompanying drawings, forming part of this specification.
This invention consists in an improved mode of fitting the rear portion of an elongated projectile for rifled ordnance, with a packing-ring of brass or other sufficiently soft metal or alloy, to be upset and expanded laterally and so driven into the grooves of the gun by the force developed by the explosion of the charge of powder.
To enable others skilled in the art to fully understand my invention, I will proceed to describe it with reference to the drawings.
Figure l, exhibits a side view of the body of the projectile with the ring in section, showing it in the bore of a gun ready to be discharged therefrom. Fig. 2, exhibits a rear view of the projectile and a transverse section of the bore of the gun. Fig. 3, is a transverse section of the projectile, taken through the ring'in the plane indicated by the line a m of Fig. 1. Fig. 4, exhibits a side view of the projectile with the ring in section, showing the ring in the condition it assumes in the discharge of the projectile; and Fig. 5, is a rear view corresponding with Fig. 4.
Similar letters of reference indicate corresponding parts in the several figures.
A, is the body of the projectile, which may be made solid or hollow and of cylindro-conoidal or other partly cylindrical form. The rear portion is of circular form,
' but reduced in size to form a shoulder, Z),
at a short distance, say from half an inch to one inch and a half, from the base, 64, according to the diameter and length of the projectile; the reduction in size being in the form of an ogee, as shown in Figs. 1 and't, making a rounded groove, 0, immediately in rear of the shoulder Z), and increasing in size from the said groove to the base (Z, which is somewhat smaller than the external diameter of the cylindrical portion of the body; but instead of being curved, the portion (Z in rear of the groove 0 may have a regular taper.' The groove 0 has two or more small feathers or ribs, 7 f, running across it, parallel or nearly so with the axis of the projectile, said feathers or ribs being formed in the casting of the body.
B, is the packing-ring of brass or other metal or alloy softer than the body of the projectile, cast upon the reduced portion 0 d, by' placing the body of the projectile in a suitable mold and pouring the metal or alloy around it.
The body of the projectile should'be heated before the casting of the ring upon it, in order to prevent the injury that would result to the ring by its shrinkage upon an unshrinking substance like cold cast-iron.
The degree to which the body should be.
heated will vary according to the fusibility of the metal or alloy of which the ring is composed. The said ring, after having cooled is turned or otherwise finished ex-. ternally to correspond in size with the exterior of the cylindrical portion of the body A, as shown in Fig. 1, and its rear end is leftexposed as shown at z i in Figs. 1 and 2, and flush with the base of the body A. The packing-ring thus cast on the body of the shell fits very tightly upon the portion V 0 cl, on whichit can neither move lengthwise nor turn, the longitudinal movement beings prevented by the shoulder band the portion d, and the turning being prevented by'the ribs or feathers f f. The projectile thus fitted with the packing-ring, fits easily with in the lands of the bore of the gun, as shown in Figs. 1 and 2, which portions of the gun are shown in blue outline, and so passes easily along the bore in loading. When the charge is fired, the gases evolved by the explosion of the powder, by their pressure on the exposed rear end of the ring B, tend to drive the said ring forward against the.
shoulder Z2 and so upset the said ring to some extent and expand it laterally; and as the rear end of the ring moves forward, it
passes into a smaller portion of the part 0? of the body, and a slight opening isformed between the rear of the ring and rear of the body; and the gas rushing into this opening, drives outward those portions of the ring which are opposite the grooves, g g, of the series of projections, h h, (Figs. 4c and 5,) gun, into the said grooves, and so causes a to be formed upon the exterior of the ring, the said projections fitting closely to the grooves and preventing windage, and causing a rotary motion to be given to the ring as it passes along the bore; and the ring being prevented from turning on tliebody f j, or their equivalents, formed upon the 10 carries the body around With it and gives body, and having its rear edge, 2', exposed it the necessary rotary motion. flush or thereabout With the base of the What I claim as my invention and desire body; all siibstantially as herein described.
to secure by Letters Patent is: l g
The soft metal ring B, cast in a groove, 0, ROBERT PARROTT' in the body of the projectile and upon a Witnesses:
taper portion, cl, extending from the said M. M. LiVi'N'sfoif,
groove to the base, and upon ribs or feathers, JAMES LAIRD.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US33099A true US33099A (en) | 1861-08-20 |
Family
ID=2102703
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US33099D Expired - Lifetime US33099A (en) | Projectile fob rifled ordnance |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US33099A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9599444B2 (en) * | 2013-11-07 | 2017-03-21 | Felix RACHLIN | Accelerator |
-
0
- US US33099D patent/US33099A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9599444B2 (en) * | 2013-11-07 | 2017-03-21 | Felix RACHLIN | Accelerator |
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