EP3315892A1 - Noise attenuation device - Google Patents

Noise attenuation device Download PDF

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Publication number
EP3315892A1
EP3315892A1 EP16275159.8A EP16275159A EP3315892A1 EP 3315892 A1 EP3315892 A1 EP 3315892A1 EP 16275159 A EP16275159 A EP 16275159A EP 3315892 A1 EP3315892 A1 EP 3315892A1
Authority
EP
European Patent Office
Prior art keywords
barrel
munition
extension portion
barrel extension
range
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.)
Ceased
Application number
EP16275159.8A
Other languages
German (de)
French (fr)
Inventor
designation of the inventor has not yet been filed The
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by BAE Systems PLC filed Critical BAE Systems PLC
Priority to EP16275159.8A priority Critical patent/EP3315892A1/en
Priority to US16/345,567 priority patent/US10670363B2/en
Priority to PT177846722T priority patent/PT3532794T/en
Priority to PCT/GB2017/053013 priority patent/WO2018078320A1/en
Priority to LTEP17784672.2T priority patent/LT3532794T/en
Priority to EP17784672.2A priority patent/EP3532794B1/en
Publication of EP3315892A1 publication Critical patent/EP3315892A1/en
Ceased legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/30Silencers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/32Muzzle attachments or glands
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/32Muzzle attachments or glands
    • F41A21/325Mountings for muzzle attachments
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/32Muzzle attachments or glands
    • F41A21/34Flash dampers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/32Muzzle attachments or glands
    • F41A21/36Muzzle attachments or glands for recoil reduction ; Stabilisators; Compensators, e.g. for muzzle climb prevention

Definitions

  • This invention relates to a noise attenuation device and in particular a device which provides an increased performance in the range of a mortar system.
  • Blast attenuation devices such as muzzle brakes are well known in the 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.
  • 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.
  • 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 height 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.
  • 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.
  • a metal such as a metal, polymer, composite, preferably a metal, preferably steel.
  • 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 munition'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.
  • 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.
  • 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.
  • a noise attenuation device 1 the device comprises a barrel extension portion 3.
  • 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 ⁇ ° is 25°.
  • 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.
  • 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.
  • a noise reduction device 11 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.
  • a tapered portion 12 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.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Percussive Tools And Related Accessories (AREA)

Abstract

This invention relates to a noise attenuation device and in particular a device which provides an increased performance in the range of a mortar system.
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.

Description

    FIELD OF THE INVENTION
  • This invention relates to a noise attenuation device and in particular a 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 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 a frustroconical portion, has a cone angle α° 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 height 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 munition'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 81 mm standard mortar barrel in combination with an 81 mm 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.
    DETAILED 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 α° 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 (11)

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 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.
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 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 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
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.
10. A system according to claim 9, wherein the reduction of propellant is in the range of 5 to 20%wt.
EP16275159.8A 2016-10-28 2016-10-28 Noise attenuation device Ceased EP3315892A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
EP16275159.8A EP3315892A1 (en) 2016-10-28 2016-10-28 Noise attenuation device
US16/345,567 US10670363B2 (en) 2016-10-28 2017-10-05 Noise attenuation device
PT177846722T PT3532794T (en) 2016-10-28 2017-10-05 Noise attenuation device
PCT/GB2017/053013 WO2018078320A1 (en) 2016-10-28 2017-10-05 Noise attenuation device
LTEP17784672.2T LT3532794T (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
EP16275159.8A EP3315892A1 (en) 2016-10-28 2016-10-28 Noise attenuation device

Publications (1)

Publication Number Publication Date
EP3315892A1 true EP3315892A1 (en) 2018-05-02

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ID=57249759

Family Applications (1)

Application Number Title Priority Date Filing Date
EP16275159.8A Ceased EP3315892A1 (en) 2016-10-28 2016-10-28 Noise attenuation device

Country Status (2)

Country Link
EP (1) EP3315892A1 (en)
PT (1) PT3532794T (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL6804528A (en) * 1967-04-01 1968-10-02
US6308608B1 (en) * 1998-08-30 2001-10-30 Moshe Eisenman Dust suppression
EP1956335A2 (en) * 2007-02-08 2008-08-13 Honeywell International Inc. Velocity measurement using manetoresistive sensors

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL6804528A (en) * 1967-04-01 1968-10-02
US6308608B1 (en) * 1998-08-30 2001-10-30 Moshe Eisenman Dust suppression
EP1956335A2 (en) * 2007-02-08 2008-08-13 Honeywell International Inc. Velocity measurement using manetoresistive sensors

Also Published As

Publication number Publication date
PT3532794T (en) 2021-02-02

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