This disclosure relates to the field of ammunition for weapons systems. More particularly, this disclosure relates to a sabot for stabilizing a projectile fired from a gun barrel having a larger diameter than the projectile.
Sabot round assemblies generally include a projectile, which is typically a narrow metal rod with a pointed nose on its front end and stabilizing fins at its rear end, surrounded by a larger diameter sabot. Prior to firing the projectile, the rear part of the projectile is attached to a shell casing. Upon firing, the shell casing remains in the gun chamber and the propellant from the casing pushes the sabot assembly through the gun barrel. Once the sabot assembly exits the barrel, the sabot separates from the projectile. Because the gun barrel includes a larger diameter than the projectile, the sabot is needed to fill the void between the projectile and the gun barrel to, among other things, stabilize the projectile during firing and prevent the escape of gas from the shell casing ahead of the projectile.
Several problems exist with current sabot designs such as the requirement for precise machining (i.e., added expense) to make sure the diameter of the sabot assembly conforms to the diameter of the gun barrel. Additionally, current sabot designs typically include a front air scoop that essentially acts as a parachute to generate the force needed to separate the sabot from the projectile. This not only has the undesirable effect of slowing down the projectile, but it also tends to generate uneven forces on the sabot assembly resulting in trajectory degradation or failure for the projectile and damage to the gun barrel.
What is needed therefore is a sabot design capable of being efficiently manufactured while separating more efficiently from a projectile.
According to one embodiment of the disclosure, a sabot assembly includes a housing having a front end and a rear end dimensioned and configured for receiving a projectile. An air pressure cavity having a cavity diameter is disposed within the housing between the front end and the rear end of the housing and around a portion of the projectile. A plurality of air intake nozzles are in fluid communication with the air pressure cavity and each has a nozzle diameter less than the cavity diameter. The plurality of air intake nozzles extend from the front end of the housing and in parallel with the projectile to the air pressure cavity. In operation, air flows through the plurality of air intake nozzles and into the air pressure cavity upon firing of the projectile from a gun barrel to pressurize the air pressure cavity, thereby causing expansion of the housing around the projectile and against the internal surface of the gun barrel, and also assisting in separation of the housing from the projectile upon the sabot assembly exiting the gun barrel.
According to certain embodiments, the housing is removeably secured to the projectile along a first connection area disposed between a front end of the air pressure cavity and the front end of the housing and along a second connection area disposed between a rear end of the air pressure cavity and the rear end of the housing. The housing may also be divided into a plurality of independent housing sections such that each housing section is separated from both the projectile and the other housing sections upon the sabot assembly exiting the gun barrel.
According to certain embodiments, the cavity diameter is substantially constant throughout the air pressure cavity. In other embodiments, the cavity diameter may be tapered such that the air pressure cavity includes a greater diameter at a first end of the cavity adjacent to the front end of the housing than at a second end of the cavity adjacent to the rear end of the housing.
According to certain embodiments, the housing includes one or more columnar supports traversing the air pressure cavity and dividing the air pressure cavity into at least two cavity sections.
In another embodiment of the disclosure, a sabot assembly includes a projectile and a housing dimensioned and configured for receiving the projectile. An air pressure cavity is disposed between a front end and a rear end of the housing and includes a cavity diameter. A plurality of air intake nozzles are in fluid communication with the air pressure cavity and each has a nozzle diameter less than the cavity diameter. The plurality of air intake nozzles extend from the front end of the housing to the air pressure cavity. In operation, air flows through the plurality of air intake nozzles and into the air pressure cavity upon firing of the projectile from a gun barrel to pressurize the air pressure cavity for assisting in separation of the housing from the projectile upon the sabot assembly exiting the gun barrel.
According to certain embodiments, the air pressure cavity is disposed adjacent the rear end of the housing and substantially behind the projectile.
Various advantages are apparent by reference to the detailed description in conjunction with the figures, wherein elements are not to scale so as to more clearly show the details, wherein like reference numbers indicate like elements throughout the several views, and wherein:
In the following detailed description of the preferred and other embodiments, reference is made to the accompanying drawings, which form a part hereof, and within which are shown by way of illustration the practice of specific embodiments of the disclosure. It is to be understood that other embodiments may be utilized, and that structural changes may be made and processes may vary in other embodiments.
Referring to
To assist in separating the sabot housing 16 from the projectile 12 after the sabot assembly 10 exits the gun barrel, the sabot housing 16 includes a plurality of air intake nozzles 22 in fluid communication with an air pressure cavity 24. As shown in
In preferred embodiments, the sabot housing 16 is removeably connected to the projectile 12 preferably using a tooth-threaded connection 26 as known in the art and exemplified in, for example, U.S. Pat. No. 3,620,167. It is noted that this tooth/groove connection, or any other type of connection that may otherwise be used, must be sufficient to keep the sabot housing 16 connected to the projectile while the assembly 10 is disposed in the sabot housing 16 despite the extreme g-forces acting upon the assembly, particularly towards the front end 18 of the housing 16, yet capable of smoothly and efficiently allowing the housing 16 to separate from the projectile 12 once the assembly 10 exits the barrel. Due to the air pressure cavity 24 surrounding a portion of the projectile 12, the housing 16 is removeably secured to the projectile 12 at a front connection area 25 adjacent to the front end 18 of the housing 16, and disposed circumferentially between the projectile 12 and air intake nozzles 22, and at a rear connection area 27 adjacent to the rear end 20 of the housing 16. It is noted that the length of the air intake nozzles 22 is at least in part dependent on the needed length of the front connection area 25. In preferred embodiments, the front connection area and resulting length of the air intake nozzles 22 is between about 50 mm and about 150 mm for an assembly configured for a 120 mm diameter gun barrel.
Referring to the overhead view of
In operation, air enters the air nozzles 22 upon firing of the projectile 12 from a gun barrel. The air travels through the air nozzles 22 to the air pressure cavity 24 resulting in equal pressure being applied to the immediate areas of the housing 16 surrounding the air pressure cavity. In other words, the assembly 10 uses the tremendous muzzle velocity upon firing of the projectile 12 to pressurize the air pressure cavity 24 via the air intake nozzles 22. In preferred embodiments, the pressurized cavity 24 causes the housing 16 to slightly expand and thereby push the sabot housing 16 against the projectile for greater stability and against the internal surface of the gun barrel. As noted above, in order for proper firing of the projectile 12, the sabot must form a tight seal between the gun barrel and the projectile. This generally requires very precise machining of the sabot to make sure it conforms to the diameter of the gun barrel. However, providing for expansion of the sabot housing 16 upon firing according to the present disclosure allows the sabot housing 16 to be fabricated with more relaxed tolerances and, thus, less expensively.
Once the projectile 12 and associated sabot housing 16 exit the gun barrel, the internal pressure in the pressure cavity 24 exceeds the air pressure external to the gun barrel and therefore operates to smoothly and efficiently separate the sabot housing 16 from the projectile 12 without subjecting the projectile 12 to unnecessarily high mechanical stresses. As noted above, the sabot housing 16 is preferably separated into multiple sections 16a, 16b, and 16c loosely attached to each other while the assembly 10 is inside the gun barrel. Upon exiting the gun barrel, the internal pressure of the pressure cavity 24 causes each section of the housing 16 to separate and push away from the projectile 12 and the other sections.
In another aspect of the disclosure, the internal pressure of the pressure cavity 24 may be altered in various ways. One way is by changing the diameter of the air intake nozzles 22. In this regard, an increase in the air intake nozzle diameter 22 increases the air pressure of the pressure cavity 24. In preferred embodiments, the diameter of the air nozzles remains in a range of about 2 mm to 4 mm for a 120 mm diameter gun barrel while the diameter of the pressure cavity is in a range of about 70 mm to about 90 mm. Another way to alter the internal pressure of the pressure cavity 24 is to alter the dimensions and configuration of the pressure cavity 24. For example, the front end 18 of the housing 16 generally requires a stronger connection (e.g., larger surface connection area) between the housing 16 and projectile 12 because it exits the gun barrel before the rear end of the housing. Thus, in certain embodiments, it may be advantageous to provide a stronger front connection area 25. As a result, it may be desired to apply a greater separation pressure toward the front end of the cavity 24. This may be accomplished by tapering the cavity 24 such that it includes a greater diameter towards the front of the cavity 24 and a smaller diameter towards the rear of the cavity.
Referring to
Referring to
The foregoing descriptions of embodiments have been presented for purposes of illustration and exposition. They are not intended to be exhaustive or to limit the embodiments to the precise forms disclosed. Obvious modifications or variations are possible in light of the above teachings. The embodiments are chosen and described in an effort to provide the best illustrations of principles and practical applications, and to thereby enable one of ordinary skill in the art to utilize the various embodiments as described and with various modifications as are suited to the particular use contemplated. All such modifications and variations are within the scope of the appended claims when interpreted in accordance with the breadth to which they are fairly, legally, and equitably entitled.
The U.S. Government has rights to this invention pursuant to contract number DE-NA0001942 between the U.S. Department of Energy and Consolidated Nuclear Security, LLC.
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Number | Date | Country |
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102010044003 | May 2012 | DE |