US2408252A

US2408252A - Ammunition

Info

Publication number: US2408252A
Application number: US469871A
Authority: US
Inventors: Ganahl Carl De
Original assignee: KAISER CARGO Inc
Current assignee: KAISER CARGO Inc
Priority date: 1942-12-23
Filing date: 1942-12-23
Publication date: 1946-09-24
Anticipated expiration: 1963-09-24

Description

Sept 1946. c. DE GANAHL 2,408,252

AMMUNITION Filed Dec. 23, 1942 INVENTOR CARL de GANAHL BY ATTORNEYS I Patented Sept. 24,1946

AMIVIUNITION Carl de Ganahl, Trenton, N. J., assignor, by mesne assignments, to Kaiser Cargo, 1110., Bristol, Pa., a corporation of California.

Application December 23, 1942, Serial No. 469,871

8 Claims.

This invention relates to ammunition and particularly to projectiles carrying a charge of gasf orming material which may be ignited to afford a jet capable of accelerating the flight of a projectile after initial discharge thereof.

The invention may be applied to projectiles of various kinds, including shells, bombs and torpedoes. The flight of such projectiles may be initiated in any suitable manner. In the case of light artillery ammunition, the shell may be assembled with a casing carrying the usual powder charge. In heavy artillery, the shell may be separate from the powder charge which is introduced behind it in the gun. Bombs may be released in the usual manner, and torpedoes discharged in accordance with customary practice. In various types of ammunition as heretofore used, the velocity, trajectory, etc., have depended upon the charge employed for initial propulsion or upon gravity.

It is the object of the present invention to pro-- vide an improved type of ammunition in which acceleration is accomplished by the discharge of combustion gases afiording jet propulsion for the projectile.

Another object of the invention is to increase the mass of the combustion gases so as to aiford a substantial increase in the acceleration of the projectile.

Another object of the invention is to provide an additional quantity of high density gas in the products of combustion ejected from the projectile.

Other objects and advantages of the invention will be apparent as it is better understood by reference to the following specification and the accompanying drawing, in which Fig. 1 is a longitudinal section through a projectile and shell casing;

Fig. 2 is a section on the line 2-2 of Fig. 1;

Fig. 3 is a section on the line 33 of Fig. 1; and

Fig. 4 is an enlarged transverse section through the charge of combustible material indicating the arrangement thereof.

In describing the invention, reference is made The application of the invention to the various forms of projectiles will be readily comprehended.

to a simple form of projectile associated with a casing carrying the powder charge to initiate the flight of the projectile. It is to be understood that the drawing is merely illustrative and that the invention may be applied as hereinbefore indicated to free shells, bombs and torpedoes. The details of construction of these various forms of projectiles form no part of the present invention, and such details are not, therefore, illustrated.

The invention depends upon the provision of a chamber within the projectile adapted to receive the charge of combustible material, as hereinafter more fully described, the chamber merging into a Venturi passage affording means for escape of the gases formed when the combustible material is ignited. The mass of the gases evolved by the combustion of ordinary powder is relatively slight in comparison with the mass of a projectile capable of enclosing the powder charge. In order to obtain the desired acceleration of the projectile, it is desirable to increase the mass of the combustion gases.

In my co-pending application Ser. No. 458,791, filed September 18, 1942, I have described means for increasing the mass of the combustion gases by the inclusion with the powder of oxides of metals of the highest available density. The most available metals for the purposeare mercury, lead and bismuth, all of which are members of series 11 of theperiodic system of elements having atomic weights of 200 or higher. Of these, the oxides of mercury afford the most desirable characteristics.

I prefer to employ the oxides of the heavy metals, and particularly mercuric or mercurous oxide, since these oxides are capable of giving up oxygen, thus affording an additional source of oxygen for the combustion of the gas-forming material, such for example as the cellulose compounds normally employed as explosives. Since these cellulose compounds are invariably deficient in oxygen, the additional oxygen supplied by the inclusion of a metallic oxide ensures rapid and complete combustion, provided a sufficient quanof the heavy metals as described provides a sur- There are numerous forms of carbon available which may be utilized to attain the desired results. When the carbon is consumed, carbon dioxide is formed and mingled with the combustion gases. The density of carbon dioxide is relatively high as compared, for example, with water, the combustion product of hydrogen. Hence the addition of carbon dioxide to the gases adds to the mass and thus to the propulsive efiect of the gases discharged.

The proportions of the several constituents employed in the rocket charge may vary over a wide range and will depend to some extent upon the type of explosive used. Nitrocellulose difiers in degree of nitration and it maybe desirable to employ deco-nitrocellulose or in some cases a product of lower nitration. In any event, the proportion of carbon to the heavy metal oxide hould be such as to utilize excess oxygen supplied by the metal oxide. Merely as an illustration of the invention, the following combinations may be employed, assuming the explosive to be deca-nitrO- cellulose. The quantities are expressed in mols.

Explosive Carbon ag-i The distribution of the combustible and oxidizing agents in the charge employed in the projectile is a matter of some importance since it is necessary to maintain as much uniformity as practicable and particularly to control the rate of combustion. The explosive is usually prepared in the form of extruded rods which are cut to afford relatively short elements. Since the explosive is a plastic, the carbonaceous material may be introduced as a filler and the explosive may be formed as desired. In various forms, the explosive material may be incorporated with the auxiliary oxidizing material consisting of the oxides of the heavy metals to afford mixtures as uniform as possible.

I find it desirable, however, to first form the explosive material with the carbonaceous filler into sheets. The plastic may be easily prepared in this form. Similarly the oxide or oxides of the heavy metals may be mixed with any suitable adhesive material and likewise formed into sheets. The sheets may be cut into pieces of suitable size and arranged to form a laminated structure in which the sheets containing the oxide or oxides of the heavy metal are interposed between the sheets consisting of the explosive and carbonaceeus filler. In this manner a charge of suitable size for the capacity of the projectile may be prepared readily.

To avoid premature contact between the explosive and the auxiliary oxidizing material, any suitable coating may be applied to the sheets before they are assembled. Paraffin may be employed as the coating composition. There are various other compounds of a comparable nature which may be utilized for this purpose. By adjustment of the thickness of the laminations and the amount and nature of the auxiliary oxidizing material in relation to the quantity of explosive and carbonaceous filler, sufficient oxygen may be supplied to ensure complete combustion both of the explosive and of the carbonaceous filler, and the rate of combustion can be regulated by such adjustment so as to afiord. the discharge gases of relatively large mass. The laminated arrangement as described ensures a uniform rate of combustion.

The application of the invention, for example to a shell of given size which is ejected from a gun at a predetermined muzzle velocity, will actually increase the velocity of the shell so that the energy of impact at the end of its flight for a given range will be at least twice the energy available if the flight were not assisted by jet propulsion.

As an example of the invention, reference is made to the drawing in which 5 indicates the shell casing and 6 the projectile which is assembled therewith. The details of an armor-piercing nose for the projectile form no part of the present invention and are not illustrated and described. Likewise it is unnecessary to describe the provision for high explosive in the nose of the projectile, this being common in some types of ammunition. It is to be understood that the projectile may be of any of the well known types. In the present case the projectile carries the usual band I of copper or other soft metal adapted to co-operate with the rifiing of the gun. This, of course, will be omitted in cases where it is unnecessary.

A chamber 8 is provided in the projectile and merges with a smooth curved surface 9 into a Venturi passage l0 which flares outwardly at the tail of the projectile. The inclusive angle of the walls of the passage should not exceed approximately 10-12". Preferably the walls of the chamber 8 and of the Venturi passage H! are lined with a suitable heat-insulating material II such as asbestos cement or the like. The outer wall 12 o'f the tail of the projectile should have a reduced cross-sectional diameter to avoid possible expansion under the eifect of pressure which might otherwise prevent the projectile from leaving the shell casing 5.

In order to permit the introduction of the powder charge in the form of a cylinder, the projectile may be manufactured in two parts, the rear end being threadedly or otherwise secured at 13 to the body of the projectile.

As hereinbefore indicated, the charge of explosive with the carbonaceous filler and the auxiliary and oxidizing material may be introduced to the chamber 8 in any suitable form. Preferably, as shown in Fig. 4, the explosive and carbonaceous filler are formed in sheets I4, and the oxidizing material in sheets I5 which are cut to propersize and laminated to provide a cylindrical body which is adapted to fill the chamber 8 of the projectile.

The powder IS used in the shell casing 5 may be of the usual kind employed for similar purposes and designed to permit increased rate of burnin following ignition, in order that pressure may be maintained in the gun barrel after the projectile leaves the shell casing. The powder may be ignited by a primer IT. The passage [0 is likewise filled with powder which becomes ignited and in turn ignites the combustible material within the chamber 8. The latter ignition should occur as the projectile commences its flight and ejection of the combustion gases through the passage Ill affords jet propulsion and accelerates the projectile. The provision of the high density auxiliary material consisting of 0xides of the heavy metal increases the density 'of the gases ejected. Likewise, combustion of the carbonaceous material affords carbon dioxide which also increases the density of the ejected g gases. This assures maximum available mass in the propelling jet and hence increased acceleration.

Among other advantages of the invention, it is possible to secure thereby the greatest possible propelling force (momentum reaction) from a given explosive-containing space within the rocket chamber of the shell. The presence of heavy metal oxide such as mercuric oxide will serve, by absorption of heat, to reduce the temperature of the explosive reaction within the rocket chamber to practicable limits. The inclusion of relatively large proportions of carbon and heavy metal OX- ide affords means of controlling the rate of burning and causing the charge to burn from its rearward face forwardly, in a uniform manner. If necessary, the speed of burning may be reduced by reduction of the degree of nitration of the explosive.

Owing to the increased acceleration, the trajectory will be flattened, the speed of travel to the target increased, and the available energy at the target for impact materially improved. The invention assures greater accuracy in firing because of the accelerated speed and flatter trajectory of the projectile. The increase in destructive hitting power for ammunition of a given weight alTords a substantial improvement.

While the invention has been described in connection with a light artillery shell, the shell casing may, of course, be eliminated in heavier types of artillery where the powder for initial ejection of the projectile is separately handled and introduced to the gun behind the shell. Likewise the principles employed in providing jet propulsion improved by the inclusion of high density material and particularly of oxides and carbonaceous material may be applied to projectiles of the bomb and torpedo types. The details of construction of these various forms of projectiles are not a part of the present invention except for the provision therein of a chamber and a Venturi passage through which combustion gases may be ejected.

Various changes may be made in the form, arrangement and construction of the projectiles, and in the nature of the added materials employed to improve the flight thereof without departing from the invention or sacrificing any of the advantages thereof.

I claim:

1. In a projectile, a chamber having a restricted outlet passage communicating therewith, a charge of combustible material including explosive and a non-explosive carbonaceous filler in the chamber, and auxiliary material comprising an oxide of a metal of the eleventh series of the periodic system of elements associated with the combustible material and adapted to increase the mass of the combustion gases ejected through the passage when the combustible material is ignited.

2. In a projectile, a chamber having a re-- stricted outlet passage communicating therewith, a charge of combustible material including 3.

explosive and a non-explosive carbonaceous filler in the chamber, and auxiliary material comprising a mercury oxide associated with the combustible material and adapted to increase the mass of the combustion gases ejected through 6 the passage when the combustible material is ignited.

3. In a projectile, a chamber having a restricted outlet passage communicating therewith, a charge of combustible material including explosive and a non-explosive carbonaceous filler in the chamber, and auxiliary material associated with and capable of supplying oxygen for combustion to the combustible material and adapted to increase the mass of the combustion gases ejected through the passage when the combustible material is ignited, the combustible and auxiliary material being arranged in alternating layers.

l. In a projectile, a chamber having a restricted outlet passage communicating therewith, a charge of combustible material including explosive and a non-explosive carbonaceous filler in the chamber, and auxiliary material comprising an oxide of a metal of the eleventh series of the periodic system of elements associated with the combustihis material and adapted to increase th mass of the combustion gases ejected through the passage when the combustible material is ignited, the combustible and auxiliary material being arranged in alternating layers.

5. In a projectile, a chamber having a restricted I outlet passage communicating therewith, a charge of combustible material including explosive and a non-explosive carbonaceous filler in the chamber, and auxiliary material comprising a mercury oxide associated with the combustible material and adapted to increase the mass of the combustion gases ejected through the passage when the combustible material is ignited, the combustible and auxiliary material being arranged in alternating layers.

6. In a projectile, a chamber having a restricted outlet passage communicating therewith, a charge of combustible material including explosiveand a non-explosive material in the chamber, and auxiliary material associated with and capable of supplying oxygen for combustion to the combustible material and adapted to increase the mass of the combustion gases ejected through the passage when the combustible material is ignited, the combustible and auxiliary material being arranged in alternating layer extending axially of the projectile.

'7. A propellant charge for rocket projectiles consisting of combustible material including explosive and a non-explosive carbonaceous filler and auxiliary material comprising an oxide of the eleventh series of the periodic system of elements associated with and capable of supplying oxygen for combustion to the combustible material and adapted to increase the mass of the combustion gases ejected when the combustible material is ignited.

8. A propellant charge for rocket projectiles consisting of combustible material including explosive and a non-explosive carbonaceous filler and auxiliary material comprising mercuric oxide associated with and capable of supplying oxygen for combustion to the combustible material and adapted to increase the mass of the combustion gases ejected when the combustible material is ignited.

CARL nu GANAHL.