US88689A - Improvement in projectiles - Google Patents
Improvement in projectiles Download PDFInfo
- Publication number
- US88689A US88689A US88689DA US88689A US 88689 A US88689 A US 88689A US 88689D A US88689D A US 88689DA US 88689 A US88689 A US 88689A
- Authority
- US
- United States
- Prior art keywords
- projectile
- brass
- gun
- bore
- projectiles
- 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
- 229910001369 Brass Inorganic materials 0.000 description 32
- 239000010951 brass Substances 0.000 description 32
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 12
- 238000010304 firing Methods 0.000 description 12
- 239000002184 metal Substances 0.000 description 9
- 229910052751 metal Inorganic materials 0.000 description 9
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 6
- 229910052802 copper Inorganic materials 0.000 description 6
- 239000010949 copper Substances 0.000 description 6
- 229910052742 iron Inorganic materials 0.000 description 6
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 5
- 238000012856 packing Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 239000011701 zinc Substances 0.000 description 5
- 229910052725 zinc Inorganic materials 0.000 description 5
- 229910000776 Common brass Inorganic materials 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 230000009172 bursting Effects 0.000 description 4
- 238000005266 casting Methods 0.000 description 4
- 229910000906 Bronze Inorganic materials 0.000 description 3
- 239000010974 bronze Substances 0.000 description 3
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 3
- 238000004880 explosion Methods 0.000 description 3
- 239000004429 Calibre Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229910052586 apatite Inorganic materials 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 239000010436 fluorite Substances 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- VSIIXMUUUJUKCM-UHFFFAOYSA-D pentacalcium;fluoride;triphosphate Chemical compound [F-].[Ca+2].[Ca+2].[Ca+2].[Ca+2].[Ca+2].[O-]P([O-])([O-])=O.[O-]P([O-])([O-])=O.[O-]P([O-])([O-])=O VSIIXMUUUJUKCM-UHFFFAOYSA-D 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000009491 slugging Methods 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
- Figure 2 represents a longitudinal section of the same.
- Figure 3 represents a perspective view of my projectile, without an expanding ring.
- Figure 4 represents a longitudinal section of the same.
- Figure 5 represents the end of the expanding ring B.
- E is the body of the projectile.
- a B are the rings, or hands, of malleable brass, cast girlound the cylindrical part of the body of the projec-
- the natureof my invention consists in grinding the surface of the body of an elongated projectile for riflecannon on an emery-wheehto prevent the wearing off of surface of the bore of the gun.
- the cylinder-gauge which I use for trying the rings A is a littlelarger than the cylinder-gauge which I use for trying the body of theprojectile, in order that the brass may be allowed to project a little beyond the surface of the body of the projectile, thereby forming the bearing-surface for the projectile while in the bore of the gun; but I grind the ring B, to admit of its passing through the same cylinder-gauge which I use for trying the body of the projectile.
- I saw the end of the ring B in several outs, diagonally to the axis of the projectile, as seen at 0, so as to facilitate the expanding of the metal in the grooves of the gun, and to allow the flame from the charge to escape through the cuts, so as to ignite the time-fuse at the end of the projectile.
- the malleable brass which I employ for the rings A B is composed of 60.16 copper and 39.71 zinc; or of 61.44 copper and 38.15 zinc; or of thirty-three parts, by weight, of copper and twenty-five parts, by weight, of zinc; .or of three parts, by. weight, of copper and two parts, by weight, of zinc.
- This metal possesses greater density, or solidity than brass. Its specific gravity at 10 centigrade is 8.44, which, by calculation, ought to be only 8.08, thus showing, that in theformation of the alloy, a condensation must take place.
- This alloy is naturally harder than copper, very tough, and is, in a properly-managed fire, malleableso much so, that a key may be forged-outof a cast rod.
- the brass in being cast in circular cavities, having their rear side tapering inward toward the'basc of the body of the projectile, forms an interlocking-joint with the iron of the body, which becomes tighter by the action of the charge in firing; and, as the projectile is pressed forward, by the charge, through the bore of the gun, the rings are pressing rearward in the taper of the grooves by their inertia, and in being pressed in the rifles of the boreof the gun.
- the sawing of the end of the ring B in several cuts, at oblique angles to the axis of the projectile, facilitates the expanding of the metal into the rifles of the bore, and permits a sufficient amount of flame to escape through the cuts, in order to ignite the paper fuse in the end of the projectile.
- the brass of my projectile has not its strength deteriorated by the heat generated in firing the gun and does not crack in being cast around the body of the projectile.
- my projectile may be heated red hot, and fired, without stripping, a result which cannot be obtained with projectiles provided with common brass or bronze.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Description
J; ABSTERDAM.
' Projectile.
Patented April 6, 1869.
N. Pmcnsi Phomum hu, Was! Q I 'SNQW- 6 v s amiml 5mm gem iii-ti ew JOHN ABSTERDAM, 0F NEW YORK, N. Y.
' Letters PM No. 88,689, dated April 6, 1869.
IMPROVEMENT IN PROJ'EO'I'ILES. I
The Schedule referred to in these Letters Patent and making part of the name.
HQ -o To all whom it may concern:
Be it known that I, JOHN ABSTERDAM, scientific and mechanical engineer, of the city, county, and State of New York, have invented a new and useful Projectile for rifle-cannon; and I do hereby declare that 'the following is a full and exact description thereof, reference being had to the accompanying drawings, and to the letters of reference marked thereon, in which- Figure 1 represents a perspective view of my projectile, with an expanding ring.
Figure 2 represents a longitudinal section of the same.
Figure 3 represents a perspective view of my projectile, without an expanding ring.
Figure 4 represents a longitudinal section of the same.
Figure 5 represents the end of the expanding ring B.
E is the body of the projectile.
A B are the rings, or hands, of malleable brass, cast girlound the cylindrical part of the body of the projec- The natureof my invention consists in grinding the surface of the body of an elongated projectile for riflecannon on an emery-wheehto prevent the wearing off of surface of the bore of the gun.
It alsoconsists in constructing an elongated projectile for rifle-cannon with'an expanding s abot-ring, or band, of brass, or other suitable metal, cast around the base of the body of the shot, with sides projecting rearward, having its inner surface cast parallel to the iongitudinal section of the projectile, to prevent the sides of the expanding metal from wedging in the bore of the gun, in case the same or part of the same should strip from the body of the shot.-
To enable others skilled in the art to make and use my invention, I will describe its construction and opera run.
I make my projectile cylindro-conical in shape, or I make it in any other desired form, or shape. I cast it with one or more circular cavities running around its cylindrical part, perpendicular to the axis of the proectiles, as seen at A B. These cavities, I afterward fill with malleable brass; that is to say, with a brass thatis malleable while hot.
Before filling the circular cavities with the malleable brass, I grind the surface of the body of the projectile on an emery-wheel, to admit of its passing through the cylinder-gauge.
And in order to cast the rings, bands, or bearings, I place the projectile upright in a mould, having its inner diameter a little larger than the diameter of the bore of the cylinder-gauge. I then fill the cavities A Bwith the melted malleable brass, which forms its surface against the sides of the bore of the mould; but,
immediately after pouring the melted brass in the circular cavities, I extract the projectile from the mould, and plunge it immediately in water, while the brass is yet red hot or thereabout.
I afterward grind and polish the malleable-brass rings on an emery-wheeh'to admit of their passing through the cylinder-gauge.
The cylinder-gauge which I use for trying the rings A is a littlelarger than the cylinder-gauge which I use for trying the body of theprojectile, in order that the brass may be allowed to project a little beyond the surface of the body of the projectile, thereby forming the bearing-surface for the projectile while in the bore of the gun; but I grind the ring B, to admit of its passing through the same cylinder-gauge which I use for trying the body of the projectile.
It is not necessary that-the ring B should project beyond the surface of thetbody of the projectile, on account of its being expanded, by the explosion of the charge into the rifles of the bore of the gun, in firing.
It is not necessary to turn or plane my projectile, as the bearing-surfaces of malleable brass remove the necessity of its being turned or planed, whereas other projectiles are either turned on a lathe or planed in being forced through circular dies, a process which deteriorates the strength of the iron, in removing the skin from the surface of the same.
When my projectile is intended to be fired with cannon rifled with shallow grooves, I let the ring B project beyond the base of the body of the projectile, as seen at a, thereby forming a cup with 'thebase of the body, as seen at X.
But when my projectile is intended to be fired with cannon rifled with deep grooves, I dispense with the ring B, and use only the rings A, which in their being cast with a number of projections, or buttons m, corresponding with the number of .the rifles of the bore, the projectile is made to take the grooves in inserting the projections in the rifles of the bore, in loadingthe un. g I cast the rings A B in circular cavities, having their rear side tapering inward toward the base of the body of the projectile, as seen at o, and I regulate the dimensions of the rings, bands, or bearings according to the calibre of my projectiles.
I saw the end of the ring B in several outs, diagonally to the axis of the projectile, as seen at 0, so as to facilitate the expanding of the metal in the grooves of the gun, and to allow the flame from the charge to escape through the cuts, so as to ignite the time-fuse at the end of the projectile.
The malleable brass which I employ for the rings A B is composed of 60.16 copper and 39.71 zinc; or of 61.44 copper and 38.15 zinc; or of thirty-three parts, by weight, of copper and twenty-five parts, by weight, of zinc; .or of three parts, by. weight, of copper and two parts, by weight, of zinc.
This metal possesses greater density, or solidity than brass. Its specific gravity at 10 centigrade is 8.44, which, by calculation, ought to be only 8.08, thus showing, that in theformation of the alloy, a condensation must take place.
Calculation shows that this alloy may be considered as a determinate chemical combination, for the results (3 cu. X 2 zn.) I
The hardness of this alloy, if not cooled immediately while hot, is the same as that of fluor-spar. It can be scratched by apatite, (glass) Consequently its hardness is 4; but, when suddenly immersed in water while red hot, its hardness is considerably diminished, and becomes very pliable-so much so, that a cast rod may be coiled spirally, without danger of cracking the metal.
This alloy is naturally harder than copper, very tough, and is, in a properly-managed fire, malleableso much so, that a key may be forged-outof a cast rod.
It is a well-known fact that common brass containing from 27 .4 to 31.8 per cent. of zinc, and from 71.9 to 65.8 per cent. of copper, is not malleable while hot, and that the only way to work it is while cold.
The operation of my invention is as follows, viz:
It being known that common brass or bronze is extremely-brittle while hot, therefore it can readily be seen that all projectiles having their sabots, or packing made of either of those metals are extremely dangerous in firing, for the heat generated by the explosion of the charge is sufiiciently intense to heat the brass to a degree that will cause the projectile to strip in firing. The projectile, in being stripped of its brass, loses its range and accuracy of flight, and the fragments of brass arenot the less dangerous to life when fired over the heads of troops, but the brass packing, or sabot, in breaking in the bore of the. gun, is also liable to slug, or wedge the projectile in the bore, thereby causing the bursting of the piece in firing. So it will be seen, that in casting the ring, or band B, of figs. l and 2, with projecting sides, of one thickness, the danger of bursting the gun by slugging, or wedging is entirely obviated, even if the expanding metal of my projectile from the body of the same should be stripped in firing.
Lead, and a variety of other soft metals, have been used for taking the grooves of the gun, and have been found to be liable to strip, in not possessing sufficient tenacity to resist the torsion ofthe projectile while passing through the bore of the gun. Therefore, brass has been substituted, on account of possessing greater tenacity. But those who have witnessed the firing of projectiles with brass sabots have also seen the stripping of projectiles, and the bursting of guns, especially guns of large calibre, where large charges of powder are used, in which large charges produce intense heat, in firing, showing that brass is totally unfit for the packing, or sabots of projectiles unless malleable while hot, on account of otherwise becoming brittle from the heat generated by the explosion of the charge. Now,
my brass does not-become brittle'in being heated, but
-. becomes more pliable in firing my projectile. My malleable brass takes the grooves of the gun, Without stripping, and, if red-hot shot should .be requiredto be fired, my projectile may be heated red hot, and fired, without danger of stripping. All that is required,
- in heating my projectile red hot, is simply to sprinkle the brass with water, so as to prevent it from melting.
The brass, in being cast in circular cavities, having their rear side tapering inward toward the'basc of the body of the projectile, forms an interlocking-joint with the iron of the body, which becomes tighter by the action of the charge in firing; and, as the projectile is pressed forward, by the charge, through the bore of the gun, the rings are pressing rearward in the taper of the grooves by their inertia, and in being pressed in the rifles of the boreof the gun.
My brass, by being plunged in water while hot, be-
asses comes soft and pliable, which otherwise would be too hard, and is also shrinked arpund the iron, by sudden cooling, tighter than could be obtained by cooling gradually.
The sawing of the end of the ring B in several cuts, at oblique angles to the axis of the projectile, facilitates the expanding of the metal into the rifles of the bore, and permits a sufficient amount of flame to escape through the cuts, in order to ignite the paper fuse in the end of the projectile.
' The advantages of my invention are as follows, viz:
By grinding the cylindrical surface of the body of my projectile on an emery-wheel, I polish the same with a smooth surface, that prevents the wearing or deteriorating of the surface of the bore of the gun, at the same time preserving the strength of the casting, as the grinding takes ofi only the rough surface, without destroying the strength of the iron, in contradistiuction to otherprojectiles now made, where theskin of the iron is taken ofi in planing, or forcing the projectile through dies.
Also, in casting the band, or ring B with projecting sides, of even thickness, parallel to the longitudinal section of the projectile, I obviate the danger of bursting the gun fromstripping, even if said ring should'be loose, cracked, or detached from the body of the shot; and the other advantages of my projectile may be described in the manner following, viz: 1
First, the brass of my projectile has not its strength deteriorated by the heat generated in firing the gun and does not crack in being cast around the body of the projectile.
Second, it may be cast around the body of the projectile, with as much facility as lead, by following the process herein described; whereas,
Third, common brass or bronze cannot be cast around a body of iron without danger of parting asunder or cracking.
Fourth, my projectile may be heated red hot, and fired, without stripping, a result which cannot be obtained with projectiles provided with common brass or bronze.
Fifth, in casting the brass in circular cavities, havin g their rear side tapering inward toward the baseof the body of the projectile, the packing has a tendency to become tighter in firing; whereas,
Sixth, in other projectiles now in use, the packing has always a tendency of becoming loose in firing.
Seventh, in plunging the projectile suddenly in water while the brass is hot, I soften the brass, to such an extent as to render it very soft and pliable, whereas otherwise it would be too hard, and also shrink the brass firmly around the body of the projectile by the sudden shrinkage of the brass.
Eighth, in sawing the end of the expanding ring B .at-oblique angles to the axis of the projectile, I facilitate the expanding of the brass into the rifles of the bore, at the same. time allowing a sufficient amount of flame to escape through the cuts, so as to ignite the paper fuse with great facility.
Having thus described my invention,
What I claim as new, and desire to secure by Letters Patent, is-- The cup x, having sides parallel to the major axis of the projectile, and immovably secured and retained thereon by the interlocking-dovetail B, substantially as herein described and shown.
I hereby set my signature, in the city of Philadelphia, Pennsylvania, this 2d day of June, 1865.
JOHN ABSTERDAM.
Witnesses:
J. H. WEBB, A. R. REDSEGKER.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US88689A true US88689A (en) | 1869-04-06 |
Family
ID=2158171
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US88689D Expired - Lifetime US88689A (en) | Improvement in projectiles |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US88689A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080257139A1 (en) * | 2005-03-31 | 2008-10-23 | Leslie Mervyn Harrison | Method of manufacturing ammunition |
| US20090145320A1 (en) * | 2004-04-02 | 2009-06-11 | Leslie Mervyn Harrison | Projectile |
| US20090178585A1 (en) * | 2004-04-02 | 2009-07-16 | Leslie Mervyn Harrison | Projectile |
-
0
- US US88689D patent/US88689A/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090145320A1 (en) * | 2004-04-02 | 2009-06-11 | Leslie Mervyn Harrison | Projectile |
| US20090178585A1 (en) * | 2004-04-02 | 2009-07-16 | Leslie Mervyn Harrison | Projectile |
| US7921780B2 (en) * | 2004-04-02 | 2011-04-12 | Techventure Investments Pty Ltd | Projectile |
| US20080257139A1 (en) * | 2005-03-31 | 2008-10-23 | Leslie Mervyn Harrison | Method of manufacturing ammunition |
| US7665402B2 (en) | 2005-03-31 | 2010-02-23 | Techventure Investments Pty Ltd. | Method of manufacturing ammunition |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4381692A (en) | Method of making an incendiary munition | |
| US3797396A (en) | Reinforced lightweight cartridge | |
| CA2554491C (en) | Jacketed one-piece core ammunition | |
| US5299501A (en) | Frangible armor piercing incendiary projectile | |
| US2393648A (en) | Projectile | |
| US6115894A (en) | Process of making obstacle piercing frangible bullet | |
| US2411862A (en) | Method of forming frangible explosive containers and the product so produced | |
| SE450294B (en) | GRANATHOLE INCLUDING FORMAT SPLITS AND SETS FOR ITS MANUFACTURING | |
| SE441784B (en) | SPLIT PICTURING EXPLOSIVE GRANDE WAVE, AS WELL AS ASTADCOMMETE THIS BY A POWDER METALLURGICAL PROCEDURE | |
| US1502925A (en) | Projectile | |
| US88689A (en) | Improvement in projectiles | |
| US36449A (en) | Improvement in the | |
| US293337A (en) | Projectile | |
| US41668A (en) | Improvement in packing projectiles for rifled ordnance | |
| US43835A (en) | Improvement in projectiles for rifled ordnance | |
| US1276082A (en) | Projectile. | |
| US3261121A (en) | Gun barrel with explosively welded liner | |
| US20100212535A1 (en) | Traceable Frangible Projectile | |
| US2970543A (en) | Ammunition | |
| US122014A (en) | Improvement in projectiles | |
| US2021685A (en) | Armor piercing projectile | |
| US50783A (en) | Improvement in banding and covering projectiles | |
| US1202162A (en) | Bullet. | |
| EP0158828A1 (en) | Method of manufacture of a metallic sabot | |
| US437262A (en) | Bullet |