GB2555579A - Noise attenuation device - Google Patents
Noise attenuation device Download PDFInfo
- Publication number
- GB2555579A GB2555579A GB1618226.3A GB201618226A GB2555579A GB 2555579 A GB2555579 A GB 2555579A GB 201618226 A GB201618226 A GB 201618226A GB 2555579 A GB2555579 A GB 2555579A
- Authority
- GB
- United Kingdom
- Prior art keywords
- barrel
- munition
- extension portion
- range
- barrel extension
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/30—Silencers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/32—Muzzle attachments or glands
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/32—Muzzle attachments or glands
- F41A21/325—Mountings for muzzle attachments
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
- F41F1/06—Mortars
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
A noise attenuation device 1 suitable for use on a munition barrel (e.g. a mortar), comprising a barrel extension portion 3. At a first end of the barrel extension portion 3 there is a tapered portion 2 which tapers outwardly from said barrel extension portion 3. At a second end of the barrel extension portion 3 a connector 4 secures the device onto a munition barrel. The device may allow a reduced mass propellant munition to be used.
Description
(71) Applicant(s):
BAE SYSTEMS PLC 6 Carlton Gardens, London, SW1 5AD, United Kingdom (72) Inventor(s):
Mark Edward Roper Craig Ian Young
(51) INT CL: | |
F41A 21/30 (2006.01) F41F1/06 (2006.01) | F41A 21/32 (2006.01) |
(56) Documents Cited: GB 0247900 A WO 2013/160330 A1 US 20060288854 A1 | EP 1837618 A1 WO 1993/008439 A1 |
(58) Field of Search: INT CL F41A, F41F Other: WPI, EPODOC |
(74) Agent and/or Address for Service:
BAE SYSTEMS IP Dept
PO BOX 87, Farnborough Aerospace Centre,
Farnborough, Hampshire, GU14 6YU, United Kingdom (54) Title ofthe Invention: Noise attenuation device Abstract Title: Noise attenuation device (57) A noise attenuation device 1 suitable for use on a munition barrel (e.g. a mortar), comprising a barrel extension portion 3. At a first end of the barrel extension portion 3 there is a tapered portion 2 which tapers outwardly from said barrel extension portion 3. At a second end ofthe barrel extension portion 3 a connector 4 secures the device onto a munition barrel. The device may allow a reduced mass propellant munition to be used.
At least one drawing originally filed was informal and the print reproduced here is taken from a later filed formal copy.
1/2
01 18
Fig. 1
3
2/2
01 18
Fig. 2a
Fig. 2b je
-1 Noise attenuation device
FIELD OF THE INVENTION
This invention relates to a noise attenuation device and in particular a 5 device which provides an increased performance in the range of a mortar system.
BACKGROUND
Blast attenuation devices such as muzzle brakes are well known in the 10 art. They typically provide a means of allowing the rapid dispersion of the hot gases. Further features on these device is that they use apertures, such as slits or holes to allow the gases to disperse radially outwardly, to reduce the recoil of the barrel and attached ordnance.
SUMMARY OF THE INVENTION
In a first aspect, the present invention provides a noise attenuation device suitable for use on a munition barrel, said device comprising an barrel extension portion, at a first end of said barrel extension portion there is a tapered portion which tapers outwardly from said barrel extension portion, at a second end of the barrel extension portion a connector to secure the device onto a munition barrel.
The tapered portion may be is frustroconical, cupola, parabola, flared portion, to allow the controlled dispersion of the gases produced as the munition leaves the barrel.
Detailed optimised modelling has found that when the tapered portion is 25 a frustroconical portion, has a cone angle a° in the range of 22° to 28°, highly preferably a cone angle of substantially 25°.
Preferably the height of the tapered portion is in the range of from 5cm to 30cm, more preferably in the range of 10cm to 20 cm more preferably the
-2height of the frustroconical portion is in the range of 10 cm to 20 cm, most preferably 13.34cm.
The tapered portion may have sides which may be substantially straight, parabolic, curved, trumpet shaped sides, in a highly preferred arrangement the tapered portion has substantially straight sides.
The frustroconical portion has a base. The plane of the base may be substantially perpendicular to the plane of the barrel extension portion or it may be an elliptical/parabolic conic section, or slant cut. The base may have any shaped cross section, such as for example elliptical, circular, square, highly preferably a right angled frustrated cone with a substantially circular base.
The tapered portion comprises an inner surface and an outer surface, the inner surface may comprise a textured surface, such as for example concave convex portions, such as for example ridges, grooves, voids, such as to alter the flow of the combustion gases.
The inner surface of the tapered portion may comprise a coating or layer, to alter the friction of the surface, such as paints, polymers etc.
The barrel extension portion is a tube with an internal diameter (bore) substantially the same as the internal diameter(bore) as the munition barrel to which it is attached, such that the munition to be launched retains substantially the same gas tight seal in the barrel extension portion. In a preferred arrangement the barrel extension portion has a length in the range of from 10 cm to 60cm, more preferably 30 cm to 50cm, more preferably 45cm.
The device may be manufactured from any suitable material, such as a metal, polymer, composite, preferably a metal, preferably steel. Preferably the barrel extension portion and taper are selected from the same material.
The barrel extension portion, when deployed on the munition barrel, provides a temporary increase in overall barrel length, thereby increasing the time that the munition experiences the impulse from the hot expanding gases from the burning propellant. This may allow a reduction in the mass of propellant required to achieve the same range usually achievable with the
-3munition’s normal propellant mass. The reduction of propellant required to achieve the current maximum range, reduces the blast pressure. The combination of reduced propellant mass munition and a device according to the invention comprising a tapered portion may provide a reduction in noise to operators located around the weapon.
The use of a device on a 81mm standard mortar barrel in combination with an 81mm mortar with 20% reduced propellant mass, has been demonstrated to provide a 5dB reduction in noise to operators located proximate to the device, whilst maintaining the required distance for the mortar bomb.
Ii has been shown that a device when attached to a munition barrel allows a reduced mass propellant munition to be launched and to achieve substantially the same range.
The connector must provide a gas tight seal between the device and the munition barrel. The connector and munition barrel may comprise co-operatively engaging surfaces, such as threads, collets, locking rings.
The tapered portion may be reversibly attached to the barrel extension portion, such that the device may be more conveniently stored.
According to a further aspect of the invention there is provided a munition system comprising a munition barrel, a munition capable of being launched via said barrel, and a noise attenuation device as defined herein, said attenuation device attached by a connector to said munition barrel, wherein the munition has a reduced mass of propellant. The reduction may be at least 1%wt, preferably at least 10%wt, more preferably in the range of 5 to 20%wt.
BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1 a, b cross section of a noise reduction device, with a connector.
Figure 2a, 2b, show a side view of a mortar barrel with a noise reduction device attached thereto, and a mortar.
-4DETAILED DESCRIPTION
Turing to figure 1 there is provided a noise attenuation device 1, the device comprises a barrel extension portion 3. At a first end of the barrel extension portion 3 is a tapered portion 2, which is preferably in the form of a frustrated cone. The tapered portion 2, is tapered such that the sides expand outwardly as a function of distance from the barrel extension portion. The cone angle a° is 25°. At the second end of the barrel extension portion 3 is a connector 4. The connector 4 allows the barrel extension portion 3 to be connected to an existing munition barrel, such as a mortar barrel. The inner surface (bore) 5 of the barrel extension portion 3, should be substantially the same bore as the munition barrel to ensuring a gas tight seal with a munition progressing up the barrel extension portion.
Turing to fig 2a, there is provided a L16 81mm mortar 10, which has been in service since 1965. The mortar launcher 10 comprises a barrel portion 15, which is supported by a base plate 16, which may be sunk into the ground. The mortar launcher 10, is further supported by a bi-pod 17, to allow the mortar launcher 10 to be arranged at a specific elevation. At the open end of the mortar barrel 15, is located a noise reduction device 11. The noise reduction device 11 comprises a barrel extension portion 13. At a first end of the barrel extension portion 13 is a tapered portion 12, which is preferably in the form of a frustrated cone. The connector 14 reversibly connects the noise reduction device 11 to the open end of the barrel 15.
A mortar bomb 18 is then deposited down the elongate barrel portion 12 and barrel 15. It is essential that the elongate barrel portion 12 and barrel 15 are of substantially the same bore, (same inner diameters) such that the mortar bomb 18 forms a gas tight seal via the obturator 19, with the inner wall of the barrel 15 and elongate barrel portion 12.
Claims (2)
1 A noise attenuation device suitable for use on a munition barrel, said device comprising an barrel extension portion, at a first end of said barrel
5 extension portion there is a tapered portion which tapers outwardly from said barrel extension portion, at a second end of the barrel extension portion a connector to secure the device onto a munition barrel.
2. A device according to claim 1 wherein said tapered portion, is frustroconical, cupola, parabola, flared portion.
10
3 A device according to claim 2, wherein the frustroconical portion has a cone angle in the range of 22° to 28°
4 A device according to claim 3, wherein the frustroconical portion has a cone angle of substantially 25°.
5 A device according to any one of the preceding claims wherein the
15 barrel extension portion has a length in the range of 30cm to 60cm.
5 A device according to any one of claims 2 to 4, wherein the height of the frustroconical portion is in the range of 10 cm to 17 cm.
6 A device according to any one of the preceding claims wherein the device when attached to a munition barrel allows a reduced mass propellant
20 munition to be launched and to achieve substantially the same range.
7 A device according to any one of the preceding claims wherein the connector and munition barrel comprise co-operatively engaging surfaces.
8 A device according to any one of the preceding claims wherein the tapered portion is reversibly attached to the barrel extension portion
25 9 A munition system comprising a munition barrel, a munition capable of being launched via said barrel, and a noise attenuation device according to any one of the preceding claims, said attenuation device attached by a connector to said munition barrel, wherein the munition has a reduced mass of propellant.
-βίο A system according to claim 9, wherein the reduction of propellant is in the range of 5 to 20%wt.
Intellectual
Property
Office
Application No: Claims searched:
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1618226.3A GB2555579B (en) | 2016-10-28 | 2016-10-28 | Noise attenuation device |
LTEP17784672.2T LT3532794T (en) | 2016-10-28 | 2017-10-05 | Noise attenuation device |
PCT/GB2017/053013 WO2018078320A1 (en) | 2016-10-28 | 2017-10-05 | Noise attenuation device |
US16/345,567 US10670363B2 (en) | 2016-10-28 | 2017-10-05 | Noise attenuation device |
EP17784672.2A EP3532794B1 (en) | 2016-10-28 | 2017-10-05 | Noise attenuation device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1618226.3A GB2555579B (en) | 2016-10-28 | 2016-10-28 | Noise attenuation device |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201618226D0 GB201618226D0 (en) | 2016-12-14 |
GB2555579A true GB2555579A (en) | 2018-05-09 |
GB2555579B GB2555579B (en) | 2021-08-25 |
Family
ID=57963554
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1618226.3A Active GB2555579B (en) | 2016-10-28 | 2016-10-28 | Noise attenuation device |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2555579B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11609060B1 (en) * | 2020-08-20 | 2023-03-21 | The United States Of America As Represented By The Secretary Of The Army | Attenuating blast cone |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB247900A (en) * | 1925-02-23 | 1926-06-24 | Edgar William Brandt | Improvements in trench guns, infantry guns and the like |
WO1993008439A1 (en) * | 1991-10-17 | 1993-04-29 | Vinghøgs Mek. Verksted As | Pressure reducer for a gun muzzle |
US20060288854A1 (en) * | 2004-10-07 | 2006-12-28 | Mark Witherell | Superalloy mortar tube |
EP1837618A1 (en) * | 2006-03-21 | 2007-09-26 | Honeywell International, Inc. | Mortar blast attenuator diffuser |
WO2013160330A1 (en) * | 2012-04-24 | 2013-10-31 | Tda Armements S.A.S | Noise attenuator for a mortar |
-
2016
- 2016-10-28 GB GB1618226.3A patent/GB2555579B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB247900A (en) * | 1925-02-23 | 1926-06-24 | Edgar William Brandt | Improvements in trench guns, infantry guns and the like |
WO1993008439A1 (en) * | 1991-10-17 | 1993-04-29 | Vinghøgs Mek. Verksted As | Pressure reducer for a gun muzzle |
US20060288854A1 (en) * | 2004-10-07 | 2006-12-28 | Mark Witherell | Superalloy mortar tube |
EP1837618A1 (en) * | 2006-03-21 | 2007-09-26 | Honeywell International, Inc. | Mortar blast attenuator diffuser |
WO2013160330A1 (en) * | 2012-04-24 | 2013-10-31 | Tda Armements S.A.S | Noise attenuator for a mortar |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11609060B1 (en) * | 2020-08-20 | 2023-03-21 | The United States Of America As Represented By The Secretary Of The Army | Attenuating blast cone |
Also Published As
Publication number | Publication date |
---|---|
GB2555579B (en) | 2021-08-25 |
GB201618226D0 (en) | 2016-12-14 |
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