The invention relates to a blast diffuser for reducing the sound pressure level caused by the high-pressure combustion gases generated by the firing of a gun. Although the description relates to the use of the blast diffuser to reduce the blast pressure from a mortar gun of preferably 120 mm calibre, it should be appreciated that the invention may be applied to guns with other calibres with suitable modifications.
During the firing of large calibre guns, the combustion gases and pressure waves generated by the blast of the gun can be considerable. As a result, especially for guns of 120 mm calibre or greater, the operator of the gun has to station himself at a safe distance from the blast area to avoid injuries that may be caused by such pressure levels. In the case of muzzle-loaded weapons, such as mortars, the problem is more acute as it is necessary for the operator to be in relatively close proximity to the barrel in order to operate the weapon effectively.
Due to a desire to increase the rate of fire of a mortar gun, the peak sound pressure level at the operator's position when firing the mortar artillery system would tend to exceed the safety limit of the “Z line zone” as defined in the military standardization specifications MIL-STD 1474C (“Noise limits for military material”). This problem has constrained the firepower of the mortar system as it limits the total number of rounds that can be safely fired per day by an operator.
Conventionally, this problem may be resolved by remotely triggering the mortar firing. However, the rate of fire will be significantly reduced. The problem is accentuated by the development of modern mortar systems that are designed for high rates of fire with semi-automatic bomb loading systems.
There are various devices that have been developed to attenuate the sound pressure levels generated by the firing of a gun. A majority of these devices seek to divert the propellant gases leaving the gun barrel so that they may be allowed to expand or cool inside a chamber, or by drawing the propellant gases out of the barrel in a controlled manner. An example is U.S. Pat. No. 5,610,360 for a “Large Caliber Gun Muffler”. The patent describes a muffler for a large calibre gun having a gun tube that includes a transition section fitted around the gun tube and engaging the gun tube for preventing the escape of residual combustion gases caused by the firing of a projectile by the gun. The transition section further includes a pressure vessel, vent stack, valve and exhaust blower to draw propellant gases out of the gun tube.
The device described in the patent is elaborate and contains many parts. It also includes external attachments such as an exhaust blower which increases the complexity of the operation. Whilst it may be workable in a gun-testing environment, it is not practical for field combat operations because of its complexity and bulk, that would add to the operational overheads.
It is thus an objective of the present invention to provide an improved blast diffuser to reduce the sound pressure levels affecting the operators of guns, especially large calibre guns.
One aspect of the present invention provides a blast diffuser for a gun, comprising bore means having a surface defining a barrel through which a projectile may be discharged when the diffuser is attached, in use to a gun barrel, the blast diffuser further comprising a plurality of primary chambers arranged around the outside of the bore means and a plurality of secondary chambers which are each adjacent to an outer surface of a respective one of the primary chambers, wherein a plurality of holes is arranged in the surface of the bore means to allow the passage of combustion gases from the bore means to the primary chambers, and a plurality of holes is arranged in the outer surface of each primary chamber to allow the passage of combustion gases from each primary chamber to a respective one of the secondary chambers, each secondary chamber further comprising an opening to allow the escape of combustion gases into the atmosphere.
Another aspect of the invention provides a gun having a blast diffuser, the gun comprising a gun barrel, a plurality of primary chambers arranged around the outside of the gun barrel and a plurality of secondary chambers which are each adjacent to an outer surface of a respective one of the primary chambers, wherein a plurality of holes is arranged in the surface of the gun barrel to allow the passage of combustion gases from the gun barrel to the primary chambers, and a plurality of holes is arranged in the outer surface of each primary chamber to allow the passage of combustion gases from each primary chamber to a respective one of the secondary chambers, each secondary chamber further comprising an opening to allow the escape of combustion gases into the atmosphere.
It will be convenient to hereinafter describe an embodiment of the present invention with reference to the accompanying drawings which illustrate one form of diffuser incorporating the invention. It is to be understood that the particularity of the drawings and the related description is not to be understood as superseding the generality of the broad description of the invention as defined in the claims.
Adjacent to the diffuser barrel 14 are affixed attenuation attachments 18 on opposite sides of the diffuser barrel 14 consisting of primary chambers 20 connected to the diffuser barrel 14 and secondary chambers 22 connected to the primary chambers 20. It would be appreciated that during firing of a mortar bomb, the bomb projectile would travel past the muzzle adapter 12, diffuser barrel 14 and be discharged through the opening 16.
As illustrated in
During firing, a projectile (not shown) is propelled by high-pressure combustion gases. As the projectile passes through the blast diffuser 10, some of the gases will escape through the inner holes 24 of the diffuser barrel 14. These gases will expand into the primary chambers 20. Thereafter, these gases will escape through the outer holes 26 and further expand into the secondary chambers 22. The gases will then be discharged through the secondary chamber opening 28. Therefore, the gas pressure will be significantly reduced before the projectile leaves the barrel. Hence, the peak sound pressure level at the operator's position is also significantly reduced.
In addition, there are a series of deflection plates 30 interspersed in the secondary chambers 22 along the surface of the secondary chambers 22 next to the outer holes 26. The deflection plates 30 prevent smooth flow of the high-pressure gases to the secondary chamber openings 28 and thus further reduces the energy possessed by the gases before discharge into the atmosphere.
The blast diffuser will serve to reduce the peak sound pressure level at the operator's position to a safer level when firing large-calibre artillery systems. The improvement will assist substantially in the operation of modern artillery systems that are designed for high rates of fire and semi-automatic operation, in particular mortar systems.
The test results of the blast diffuser that were conducted in accordance with MIL-STD-1474C are tabulated in Tables 1 & 2 of FIG. 5. The results show that the blast diffuser is able to reduce peak sound pressure level at one meter away from the barrel muzzle by 184% in pressure or 9.0 dB when firing charge 8 bombs and to reduce the peak sound pressure level by 167% in pressure or 8.6 dB when firing charge 9 bombs. Both these results bring the sound pressure levels to below the “Z line zone” as defined in the MIL-STD 1474C.
While a particular embodiment of the invention has been shown and described, it will be appreciated by those skilled in the art that changes and modifications of the present invention may be made without departing from the invention in broadest aspects. As such, the scope of the invention should not be limited by the particular embodiment and specific construction described herein but should be defined by the appended claims and equivalents thereof. Accordingly, the aim in the appended claims is to cover all such changes and modifications as fall within the spirit and scope of the invention.
Number | Date | Country | Kind |
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200104409-8 | Jul 2001 | SG | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCTSG02/00159 | 7/10/2002 | WO | 00 | 4/2/2004 |
Publishing Document | Publishing Date | Country | Kind |
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WO0300889 | 1/30/2003 | WO | A |
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Number | Date | Country | |
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20040154462 A1 | Aug 2004 | US |