US1198056A - Projectile. - Google Patents
Projectile. Download PDFInfo
- Publication number
- US1198056A US1198056A US2970715A US2970715A US1198056A US 1198056 A US1198056 A US 1198056A US 2970715 A US2970715 A US 2970715A US 2970715 A US2970715 A US 2970715A US 1198056 A US1198056 A US 1198056A
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- US
- United States
- Prior art keywords
- shot
- projectile
- grooves
- wall
- charge
- 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
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-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/06—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with hard or heavy core; Kinetic energy penetrators
Definitions
- This invention relates to the wall construction of a projectile in connection with the charge chamber, and has for its object bursting of the projectile into any desired number and size of fragments.
- a further object oi the invention is to increase the sectional density oi the shot without increasing the overall dimensions of the shot.
- This object is attained by reduc ing the diameter of the charge chamber, and thickening the wall of the shot.
- the wall of the shot is thickened by reducing the diameter of the charge chamber. and.to insure bursting on detonation of a reduced charge, grooves are cut in the wall longitudinally ot' the shot to weaken the walls laterally to an internal pressure. and the ell'cctivc j ressure is increased by the additional surface atlorded by the walls of the grooves.
- :tthird object otthe invention is to tacilitalc the manufacture ot the shot, and esp e-,
- the dilliculty of hardening and tempering the walls of a shot without producing internal strains that cause weakening or rupture of the metal is greater than in the thinner walls of shells and is due to unequal contraction.
- the sudden cooling of the outer metal after heating causes a greater hardness and a greater contraction per unit of area than the slower cooling metal interior.
- the grooves cut in the walls of applicants projectile allows contraction without stress upon the inner face of the wall and to a depth corresponding to the depth of the grooves, for under the coinpressive stress oi contraction of the outer metal the unchillcd metal flows to the grooves.
- a fourth object of the invention is to obtain the greatest blast effect that may be secured by a unit weight of bursting charge.
- the blast ett'ect is directly as the velocity of the expanding gases, and in some prbportion to their volume.
- a shot that will burst symmetrically and allow the gases the quickest unobstructed means of expansion will produce the greatest blast ctl'cct. and the greatest eli'ectivc dynamic energy will be secured where the least energy of the dctonating charge is absorbed in bursting the shell.
- a further object of the invention is to produce a thick walled projectile that may be etl'ective against a submarine boat whethe on the surface or submerged.
- a projectile the front end or point of which concave.
- the object of employing this construction is'i'or a dual purpose. 1st. should the boat be awash, its location being known by the presence ot' its periscope above thesurface, the shot bydirect or plunging fire hitting the surface of the water immediately above the boat will not ricochet, and will burst shell, and fragmenting of the projectile disabling or destroying the boat.
- Figure 1 is a longitudinal sectional view of a projectile embodying the invention, in
- Fig. 2 is a crosssection on line a-a of Fi 1, showing the width of the grooves.
- Fig. 3 is a longitudinal sectional view showmg the shape of the front end or point of a modified form of a thick wall projectile provided with grooves. As this projectile is not designed for use against armor plate, the grooves extend nearer the outer surface of the shot.
- Fig. 4 is a cross-section on line Z)b of Fig. 3.
- Fig. 1, 1 indicates the cylinder of the shot which extends from the bourrelet 2 to the seat of the rotating band 3.
- 4 indicates the ogive of the shot proper.
- 5 indicates the charge chamber, other parts of the projectile will not be referred to and as they are well known no description is deemed' necessary. (3, indicates grooves milled or gouged lengthwise of the charge chamber 5, somewhat exceeding in length the cylinder length of the projectile, and to a depth that will admit of the charge burstgrooves so placed as to cause no eccentricity but any desired number may be employed when placed equi-distant.
- the effective gas surface to produce rupture in a 12 shot having a (5" diameter charge chamber equipped with grooves as here shown, each 2" deep, is greater than in an 8 diameter charge chamber in a 12" shot (density of loading in both cases being the same).
- the unit per effective gas surface per unit of cross-section of metal to be ruptured in blowing off the head, base and sides of the projectile is, as 1.83 to 1.43 respectively, and the shattering effect of detonation in applicants projectile will be localized to the segments formed by the grooves thus controlling fragmenting of the projectile.
- this figure represents a shot having a somewhat longer cylinder length than would be used in either a long range or armor piercing shot, and in connection with the thick wall is to compensate for the loss of weight due to the point cor. struction, and also to incrcasc the capacity of the charge chamber.
- 7 indicates a. concave surface extending inward on the front end of the projectile As here shown there are 4:
- An armor piercing projectile provided with a head, a cylindrical portion of uniform columnar strength throughout. the cylinder length of the projectile integral with the head and forming an interior charge chamber, grooves extending parallel with the axis of the projectile in the wall of said chamber throughout the cylinder length of the projectile, the lands between the grooves being unbroken, and a base plug for closing the rear end of said chamber,
- A, hollow projectile provided with a concave head, a cylindrical portion, a.centrally disposed chamber and grooves parallel with the axis of the projectile in the wall oi said chamber forming unbroken lands.
- a hollow jn'ojcc'tile provided with a concave head, a cylindrical portion, a longitudinal charge chamber, radial grooves parallel with the axis of the projectile in the wall oi said chamber "r'orming unbroken lands of greater width than said grooves.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
Description
W. K. RICHARDSON.
PROJECTILE. ION FILED MA I915. I 1 1 98,05 6. Patented Sept. 12, 1916.
' tirnrnn strata PATENT t rrors.
WILLIAM KING RICHARDSON, LEAVENWORTH, KANSAS.
PROJECTILE.
Specification of Letters Iatent. Patented Sept. 12, 1916.
Apnlication filed May 22, 1915. Serial No. 29,707.
certain new and useful Improvements in Projectiles, of which the following is a speci fication.
This invention relates to the wall construction of a projectile in connection with the charge chamber, and has for its object bursting of the projectile into any desired number and size of fragments.
Under the present form of construction it cannot be determined before detonation of the charge, whether a projectile will burst in twain, or into many fragments, a probable average is between 100 and 150 fragments, and they range in mass from the entire projectile to fragments too small to be efi'ective against the vulnerable material of the ship, and the velocity with which these fragments are thrown by detonation of the charge are inversely relatively proportional to the square root of thcirmass, multiplied by the effective gas surface, Therefore it is evident that at least the mass of the projectile will not have sullicient velocity to render .it destructive, while many of the fragments will be too small to be effective against the ship other than its personnel. The result of this object of the invention is attained by milling or gouging grooves lengthwise ot' the charge chamber of the projectile to a, depth corrcspoinling to the capacity of the charge chamber, considering the number o'l groovesemployed.
A further object oi the invention is to increase the sectional density oi the shot without increasing the overall dimensions of the shot. This object is attained by reduc ing the diameter of the charge chamber, and thickening the wall of the shot. The wall of the shot is thickened by reducing the diameter of the charge chamber. and.to insure bursting on detonation of a reduced charge, grooves are cut in the wall longitudinally ot' the shot to weaken the walls laterally to an internal pressure. and the ell'cctivc j ressure is increased by the additional surface atlorded by the walls of the grooves.
:tthird object otthe invention is to tacilitalc the manufacture ot the shot, and esp e-,
eially armor piercing projectiles. The manufacturers of armor piercing pro ectiles experience considerable trouble producing a shot that will fill the requirements of the U. S. ()rdnance Department. The shot must withstand the shock of impact upon the face ot' the armor plate, and after piercing the plate be in condition for ett'ectivc bursting. The conditions must approach exactness. If the wall of the shot is too light impact will crush it, if too heavy the charge will not burst it, if of proper thickness of wall though not properly hardened and tempered they are subjected to cracking before use, or rupture on tiring, due to internal strains. The dilliculty of hardening and tempering the walls of a shot without producing internal strains that cause weakening or rupture of the metal is greater than in the thinner walls of shells and is due to unequal contraction. The sudden cooling of the outer metal after heating causes a greater hardness and a greater contraction per unit of area than the slower cooling metal interior. The grooves cut in the walls of applicants projectile allows contraction without stress upon the inner face of the wall and to a depth corresponding to the depth of the grooves, for under the coinpressive stress oi contraction of the outer metal the unchillcd metal flows to the grooves.
A fourth object of the invention is to obtain the greatest blast effect that may be secured by a unit weight of bursting charge. The blast ett'ectis directly as the velocity of the expanding gases, and in some prbportion to their volume. A shot that will burst symmetrically and allow the gases the quickest unobstructed means of expansion will produce the greatest blast ctl'cct. and the greatest eli'ectivc dynamic energy will be secured where the least energy of the dctonating charge is absorbed in bursting the shell.
A further object of the invention is to produce a thick walled projectile that may be etl'ective against a submarine boat whethe on the surface or submerged. To accomplish this object I use a projectile the front end or point of which concave. The object of employing this construction is'i'or a dual purpose. 1st. should the boat be awash, its location being known by the presence ot' its periscope above thesurface, the shot bydirect or plunging lire hitting the surface of the water immediately above the boat will not ricochet, and will burst shell, and fragmenting of the projectile disabling or destroying the boat.
lVith these and other objects in view the invention will be described in connection with the accompanying drawings in which: Figure 1 is a longitudinal sectional view of a projectile embodying the invention, in
ing the shell.
to the shot,
which the dot-ted lines represent the outlines of grooves cut in the wall of the projectile. Fig. 2 is a crosssection on line a-a of Fi 1, showing the width of the grooves. Fig. 3 is a longitudinal sectional view showmg the shape of the front end or point of a modified form of a thick wall projectile provided with grooves. As this projectile is not designed for use against armor plate, the grooves extend nearer the outer surface of the shot. Fig. 4, is a cross-section on line Z)b of Fig. 3.
Referring to Fig. 1, 1 indicates the cylinder of the shot which extends from the bourrelet 2 to the seat of the rotating band 3. 4 indicates the ogive of the shot proper. 5 indicates the charge chamber, other parts of the projectile will not be referred to and as they are well known no description is deemed' necessary. (3, indicates grooves milled or gouged lengthwise of the charge chamber 5, somewhat exceeding in length the cylinder length of the projectile, and to a depth that will admit of the charge burstgrooves so placed as to cause no eccentricity but any desired number may be employed when placed equi-distant. The effective gas surface to produce rupture in a 12 shot having a (5" diameter charge chamber equipped with grooves as here shown, each 2" deep, is greater than in an 8 diameter charge chamber in a 12" shot (density of loading in both cases being the same). The unit per effective gas surface per unit of cross-section of metal to be ruptured in blowing off the head, base and sides of the projectile is, as 1.83 to 1.43 respectively, and the shattering effect of detonation in applicants projectile will be localized to the segments formed by the grooves thus controlling fragmenting of the projectile.
Referring to Fi I}, this figure represents a shot having a somewhat longer cylinder length than would be used in either a long range or armor piercing shot, and in connection with the thick wall is to compensate for the loss of weight due to the point cor. struction, and also to incrcasc the capacity of the charge chamber. in this figure, 7, indicates a. concave surface extending inward on the front end of the projectile As here shown there are 4:
from a point on the beveled surface of the shot forward of the bourrelet 2. This con struction is to prevent the shot from ricocheting on impact with the water, the concave surface tending to bite on the Water and to turn the shot downward as it checks its velocity. 6, indicates grooves out lengthwise of the shot on the inner face of the wall. These grooves approach nearer to the outer surface of the wall than the grooves shown in Fi 1.
By employing the construction herein described for armor piercing projectiles, it is evident the sectional density of the shot is increased without an increase in its superficial measurements, therefore the coeflicient of reduction for any range is reduced, giving a flatter trajectory, and for'a. given range a greater striking energy. It also secures greater accuracy of fire for it eliminates some of the time which the deviating causes, such as gravity and the wind produce. It produces the maximum result on bursting by insuring a uniformity in fragmenting the projectile which cannot be attained by present construction. It admits the use of high explosives for the bursting charge, as explosive gelatin and picric acid.
The shattering effect of picric acid is excessive and under present construction of armor piercing projectiles the average fragment of ap'rojectile when-this explosive is employed is too small to be effective against the vulnerable material of,th'e ship, such as the mechanism of the guns, engines, boilers and electric installatimis, and for this reason picric acid is not employed as a filler in armor piercing projectiles.
Due to applicants construction this most desirable explosive can be. used, for frag menting of the pro ectile will be controlled by the grooves. This explosive being almost insenslble to shock makes it a desirable filler, and the blast effect, the corrosive. and
suffocating effect of its gases, insures the greatest maximum destructive effect to both the ship and its personnel.
From the foregoing it is evident that I have produced means for controlling the fragmenting of a shot, without weakening the wall of the shot to resist either torsional or transverse strains the shot is subjected to, for l have thickened the wall of the shot, and to compensate for this added strength to the wall, I employ grooves which weaken the wall of the shot to an internal force. To compensate for a greater cross-sectional area of metal to be ruptured, I pr'opose the cmplojuucnt of a higher explosive than is now generally used as a bursting charge, which is unsuitable under present construc tion of armor piercing projectiles to be em ploycd. It is also evident that 1 have not weakened the wall of the shot to the force of a given caliber will have a given Weight, therefore my thick walled shot must have a reduced cylinder length, and L8 to these two dimensions the shot has less tendency to buckle andrupture under the shock of impact. By employing my mean'sfor controlling the fragmenting of a shot, a higher average velocity of the fragments on detonation of the charge is attained. Where a large number of fragments are produced in bursting of the shot, the gases flow to the line of least resistance, imparting a 'high velocity to the smaller fragments under the pressure and expansion of the gases.
" This correspondingly reduces the acceleration of the larger fragments,.for the gases are dissipated behind the smaller fragments of said chamber throughout the cylinder length of the projectile, and a base plug for closing the rear end of said chamber.
An armor piercing projectile provided with a head, a cylindrical portion of uniform columnar strength throughout. the cylinder length of the projectile integral with the head and forming an interior charge chamber, grooves extending parallel with the axis of the projectile in the wall of said chamber throughout the cylinder length of the projectile, the lands between the grooves being unbroken, and a base plug for closing the rear end of said chamber,
3. A, hollow projectile provided with a concave head, a cylindrical portion, a.centrally disposed chamber and grooves parallel with the axis of the projectile in the wall oi said chamber forming unbroken lands.
4-. A hollow jn'ojcc'tile provided with a concave head, a cylindrical portion, a longitudinal charge chamber, radial grooves parallel with the axis of the projectile in the wall oi said chamber "r'orming unbroken lands of greater width than said grooves.
In besttmony whereof I atlix my signature.
W'lLhlAM KING RICHARDSON.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US2970715A US1198056A (en) | 1915-05-22 | 1915-05-22 | Projectile. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US2970715A US1198056A (en) | 1915-05-22 | 1915-05-22 | Projectile. |
Publications (1)
Publication Number | Publication Date |
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US1198056A true US1198056A (en) | 1916-09-12 |
Family
ID=3266000
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US2970715A Expired - Lifetime US1198056A (en) | 1915-05-22 | 1915-05-22 | Projectile. |
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US (1) | US1198056A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3298312A (en) * | 1965-06-14 | 1967-01-17 | Kenneth W Adams | High pressure nose for a body in flight |
DE4033754A1 (en) * | 1990-10-24 | 1992-04-30 | Rheinmetall Gmbh | Projectile for destruction of targets protected by steel concrete - contains effective charge and has ogival or chisel type point |
-
1915
- 1915-05-22 US US2970715A patent/US1198056A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3298312A (en) * | 1965-06-14 | 1967-01-17 | Kenneth W Adams | High pressure nose for a body in flight |
DE4033754A1 (en) * | 1990-10-24 | 1992-04-30 | Rheinmetall Gmbh | Projectile for destruction of targets protected by steel concrete - contains effective charge and has ogival or chisel type point |
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