The invention relates in general to armaments and in particular to blast attenuators for weapon tubes.
When high pressure propellant gases are ejected from a cannon muzzle, they displace the ambient air around the muzzle thereby forming a blast wave. This negative effect of this displaced gas is called blast overpressure (BOP) and at its peak, can reach decibel values well beyond safe limits. High BOP levels may have severe adverse effect on the crew including significant hearing damage and damage to other body organs. Accordingly, many military organizations limit the amount and intensity of BOP exposure. For example, the U.S. Department of Defense uses the MIL-STD-1474E standard to determine the level of BOP that poses a danger and the permissible exposure levels of BOP per day.
Past solutions to mitigate BOP effects involved projecting high pressure gas flow forward of the weapon. However, in existing designs the length of the attenuator is a severe drawback. Current attenuators are not acceptable for use on multiple systems due to the length of the attenuator. In particular, these approaches are not suitable for weapon systems in which projectiles are loaded from the muzzle end, as in mortar weapon systems. The use of such attenuators in these systems presents a physical impediment to the user.
Accordingly, a need exists for an attenuator which has features that allow for blast attenuation and ease of projectile loading from the muzzle of the weapon system.
One aspect of the invention is a blast attenuator assembly for a muzzle loaded weapon system comprising a cone, a collar and a clamp.
The invention will be better understood, and further objects, features and advantages of the invention will become more apparent from the following description, taken in conjunction with the accompanying drawings.
In the drawings, which are not necessarily to scale, like or corresponding parts are denoted by like or corresponding reference numerals.
A blast attenuator for blast overpressure has features that allow for blast attenuation and ease of projectile loading from the muzzle of the weapon system. This combination of physical ease of use and blast reduction allows the system to achieve high levels of performance without making significant concessions to operator safety.
The blast attenuator comprises a collar and a clamp that affix to the muzzle of a weapon system. A cone is threaded onto the collar and extends forward of the collar. Advantageously, the blast attenuator is significantly shorter than existing blast attenuators. While conventional knowledge directed that a longer length was necessary for an effective blast attenuator, the inventors discovered that by significantly increasing the angle of the nozzle (34 degrees), the length of the blast attenuator could be significantly reduced. Numerical results showed that the shorter length did not decrease the effectiveness of the blast attenuator compared to conventional blast attenuators.
The blast attenuator is described herein as being affixed to a 120 mm mortar weapon system. Accordingly, the dimensions described are for a blast attenuator sized for operation on a 120 mm mortar. However, the blast attenuator is not limited to use on a 120 mm mortar and may be scaled for other caliber mortars including 60 mm and 81 mm mortar weapons. Further, while the blast attenuator is suited for use with a mortar weapon system, it is not limited to a mortar weapon system.
The blast attenuator 10 comprises a collar 12, a cone 14 and a clamp 16 that affix to the muzzle of a weapon system. The clamp 16 is affixed to the collar 12. The collar 12 threads onto the cone 14. The final assembly of the blast attenuator 10 is affixed to the muzzle of a weapon system, such as a mortar weapon system. The blast attenuator 10 slides onto the muzzle where the tube has a small lip and the clamp 16 closes to complete the assembly and adhere tightly onto the muzzle.
In the embodiment shown, the divergent nozzle 126 is approximately fifty (50) mm in length and diverges at an angle 122 of thirty-four (34) degrees from the muzzle face.
The divergent nozzle 146 of the cone 14 is at an angle 122 of thirty-four (34) degrees from the muzzle face and has a length of seventy-two (72) mm.
While the invention has been described with reference to certain embodiments, numerous changes, alterations and modifications to the described embodiments are possible without departing from the spirit and scope of the invention as defined in the appended claims, and equivalents thereof
This application claims the benefit under 35 USC § 119(e) of U.S. provisional patent application 63/068,161 filed on Aug. 20, 2020.
The inventions described herein may be manufactured, used and licensed by or for the United States Government.
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20060156804 | Shipman | Jul 2006 | A1 |
20060288854 | Witherell | Dec 2006 | A1 |
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Number | Date | Country | |
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63068161 | Aug 2020 | US |