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US2811901A - Method and apparatus for sabot removal - Google Patents

Method and apparatus for sabot removal Download PDF

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Publication number
US2811901A
US2811901A US451537A US45153754A US2811901A US 2811901 A US2811901 A US 2811901A US 451537 A US451537 A US 451537A US 45153754 A US45153754 A US 45153754A US 2811901 A US2811901 A US 2811901A
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United States
Prior art keywords
sabot
projectile
remover
gun barrel
gun
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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.)
Expired - Lifetime
Application number
US451537A
Inventor
Irwin R Barr
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.)
Textron Systems Corp
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Aircraft Armaments Inc
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Publication date
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Priority to US451537A priority Critical patent/US2811901A/en
Application granted granted Critical
Publication of US2811901A publication Critical patent/US2811901A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • 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
    • F41A21/46Barrels having means for separating sabots from projectiles

Definitions

  • This invention relates to a method for removing sabots from high velocity projectiles and to a sabot remover to be used in conjunction therewith. While the use of sabots to increase the velocity imparted to projectiles fired from guns is well known, removal of such a sabot from a projectile once it has left the gun barrel presents certain difiiculties which the present invention is designed to overcome. Some of the prior methods have utilized explosive charges to shatter the sabot, or have utilized sabots made of several pieces, or have relied on air resistance to separate the sabot from the missile. Although each of these methods is useful, each has its limitations when applied to a particular type of projectile.
  • the present invention proposes the utilization of centrifugal force developed by the axial rotation of the projectile in conjunction with a device for scoring the surface of the sabot as it leaves the gun barrel, the shock of the scoring operation together with the centrifugal force developed in the sabot acting together to fracture the sabot along the scores and remove the resulting pieces by causing them to fly tangentially outward from the surface of the projectile.
  • Figure 1 is a cross sectional view of a gun barrel equipped with the sabot remover contemplated by this invention, showing a projectile carrying a sabot just prior to its emergence from the gun barrel.
  • Figure 2 is a sectional view taken along line 22 of Figure 1 showing the arrangement of the scoring projections within the remover.
  • Figure 3 is a view of a projectile and sabot after passing through the remover showing the fractures caused by centrifugal force and the scoring operation.
  • Figure 1 shows a sectional view of a gun barrel 1 equipped with a sabot remover 2 of the type herein contemplated.
  • a projectile 3 carrying a sabot 4 is shown just prior to passing through the remover 2.
  • the sabot shown is of the type used for high velocity projectiles having a large mass with relation to cross-sectional area,
  • the forward end of the gun barrel 1, as best seen in Figure 1, is provided with threads 5 which are adapted to engage the interior threads 6 in the rearward end of the remover 2.
  • the remover which is of generally cylindrical shape, comprises a central opening 7 which is in axial alignment with the bore 8 of gun barrel 1.
  • a group of inwardly directed projections 9 extend radially inward from the inner wall of the opening 7 and encom pass within their inner edges 10 a circumference having a somewhat smaller diameter than the outer circumference of the sabot 4.
  • the projections 9, as shown in Figure 2 may be conformed spirally about the axis of the opening 7. If a rifled gun barrel is used, the twist of the projections in the remover should be made the same as that of the rifling to allow the sabot to pass through without disturbing its rate of rotation.
  • One of the advantages of this invention lies in the fact that a smooth bore gun may be used, the needed axial rotation being imparted to the projectile by the spirally conformed projections in the remover simultaneously with the scoring operation. 7
  • the necessary axial rotation may be imparted to the projectile by canting the stabilizing fins 12 with respect to the line of flight of the projectile.
  • the centrifugal force developed in the sabot by the axial rotation will 'then be effective to separate the pieces of the sabot from the projectile, causing the pieces to fly tangentially outward from the surface of the projectile.
  • the projectile 3 may continue its flight with the increased velocity imparted to it by reason of the use of the sabot 4, but free from the sabot and presenting a clean aerodynamic surface and a reduced frontal area to increase its penetrating characteristics.
  • Means for removing a sabot from a projectile fired from a gun comprising a collar carried by the barrel of said gun at the forward end thereof, means forming an opening through said collar in axial alignment with the bore of said gun, scoring means carried within said opening and extending inwardly to a circumference less than the circumference of said barrel, said scoring means being spirally disposed with relation to the axis of said bore to simultaneously score said sabot and impart axial rotation thereto as said sabot passes through said collar.
  • a 'sabot remover adapted to 'fit the end of a gun barrel, 'said remover comprising a plurality of inwardly directed projections extending to lie on a circumference less than that of said gun barrel arranged to score and substantially weaken a sabot carried by a projectile leaving said 'gun barrel, said projections being spirally di-sposed so as to impart axial rotation to said weakened sabot and to develop centrifugal forces sufficient to fracture said sabot into a plurality of fragments and separate said fragments from said projectile.
  • a sabot remover adapted to be carried by the end of -a gun barrel comprising a plurality of inwardly extending projections, the inner edges thereof lying on a circumference concentric with and smaller than the bore of said gun, and means for attaching said remover to said gun barrel.
  • a sabot remover adapted to be carried by the end of a gun barrel comprising a plurality of inwardly extending projections, the inner edges of said projections encompassing a circumference concentric with and smaller than the bore of said gun barrel, said projections each being spirally directed about the longitudinal axis of said gun barrel, and means for attaching said remover to said gun barrel.
  • a sabot remover carried by the muzzle end of a gun barrel comprising a cylindrical collar, a central opening formed in said collar concentric with and axially aligned with the bore of said gun barrel, a plurality of spirally conformed projections extending longitudinally along the inner surface of said opening, said projections extending inwardly to .lie on a circumference less than that of said gun barrel to score and substantially weaken a sabot carried by a projectile fired from said gun barrel so that centrifugal forces-engendered by rotation of said sabot about the axis of flight of said projectile will fracture said sabot, and means for attaching said remover to said gun barrel.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Description

Nov. 5, 1957 1. R. BARR 2,311,901
METHOD AND APPARATUS FOR SABOT REMOVAL Filed Aug. '25. 1954 I INVENTOR.
2,811,901 Ice Patented Nov. 5, 1957 METHOD AND APPARATUS FOR SABOT REMOVAL Application August 23, 1954, Serial No. 451,537
Claims. (Cl. 89--14) This invention relates to a method for removing sabots from high velocity projectiles and to a sabot remover to be used in conjunction therewith. While the use of sabots to increase the velocity imparted to projectiles fired from guns is well known, removal of such a sabot from a projectile once it has left the gun barrel presents certain difiiculties which the present invention is designed to overcome. Some of the prior methods have utilized explosive charges to shatter the sabot, or have utilized sabots made of several pieces, or have relied on air resistance to separate the sabot from the missile. Although each of these methods is useful, each has its limitations when applied to a particular type of projectile.
The present invention proposes the utilization of centrifugal force developed by the axial rotation of the projectile in conjunction with a device for scoring the surface of the sabot as it leaves the gun barrel, the shock of the scoring operation together with the centrifugal force developed in the sabot acting together to fracture the sabot along the scores and remove the resulting pieces by causing them to fly tangentially outward from the surface of the projectile.
It is the object of this invention, therefore, to provide a method for removing a sabot from a projectile by utilizing the velocity of the projectile and the centrifugal force developed by its axial rotation to fracture the sabot and separate it from the projectile.
It is another object of this invention to provide a device for fracturing a sabot to effect its removal from a projectile after leaving the barrel of the gun from which it is fired.
It is a further object of this invention to provide a device for simultaneously scoring the surface of a sabot carried by a projectile and imparting axial rotation thereto to effect removal of the sabot from the projectile by fracturing the sabot and causing the resulting pieces to separate from the projectile.
These and further objects of this invention will become apparent from the following description taken in conjunction with the drawing and appended claims.
In the drawing:
Figure 1 is a cross sectional view of a gun barrel equipped with the sabot remover contemplated by this invention, showing a projectile carrying a sabot just prior to its emergence from the gun barrel.
Figure 2 is a sectional view taken along line 22 of Figure 1 showing the arrangement of the scoring projections within the remover.
Figure 3 is a view of a projectile and sabot after passing through the remover showing the fractures caused by centrifugal force and the scoring operation.
Figure 1 shows a sectional view of a gun barrel 1 equipped with a sabot remover 2 of the type herein contemplated. A projectile 3 carrying a sabot 4 is shown just prior to passing through the remover 2. .The sabot shown is of the type used for high velocity projectiles having a large mass with relation to cross-sectional area,
the method of this invention being particularly suited for use with such projectiles and sabots, but it is to be understood that any conventional type of sabot may, by proper utilization of the method of this invention, be removed from its associated projectile.
The forward end of the gun barrel 1, as best seen in Figure 1, is provided with threads 5 which are adapted to engage the interior threads 6 in the rearward end of the remover 2. The remover, which is of generally cylindrical shape, comprises a central opening 7 which is in axial alignment with the bore 8 of gun barrel 1. A group of inwardly directed projections 9 extend radially inward from the inner wall of the opening 7 and encom pass within their inner edges 10 a circumference having a somewhat smaller diameter than the outer circumference of the sabot 4.
The projections 9, as shown in Figure 2, may be conformed spirally about the axis of the opening 7. If a rifled gun barrel is used, the twist of the projections in the remover should be made the same as that of the rifling to allow the sabot to pass through without disturbing its rate of rotation. One of the advantages of this invention, however, lies in the fact that a smooth bore gun may be used, the needed axial rotation being imparted to the projectile by the spirally conformed projections in the remover simultaneously with the scoring operation. 7
If it is desired to utilize a smooth bore gun in conjunction with a remover having straight projections instead of the spiral form shown in the drawing, the necessary axial rotation may be imparted to the projectile by canting the stabilizing fins 12 with respect to the line of flight of the projectile.
In operation, when a projectile carrying a sabot i-s fired from a gun equipped with the remover of this invention, the sabot is deeply scored in passing through the remover. Because of the velocity imparted to the projec tile and the sabot in the gun barrel prior to entering the remover, considerable shock is sustained by the sabot upon entry into the remover, the shock of the scoring operation and the centrifugal force developed by the axial rotation combining to fracture the sabot along the scores in a manner similar to the cracks 11 shown in Figure 3. The centrifugal force developed in the sabot by the axial rotation will 'then be effective to separate the pieces of the sabot from the projectile, causing the pieces to fly tangentially outward from the surface of the projectile. Thus, the projectile 3 may continue its flight with the increased velocity imparted to it by reason of the use of the sabot 4, but free from the sabot and presenting a clean aerodynamic surface and a reduced frontal area to increase its penetrating characteristics.
Each of the forms of the present invention herein disclosed provides an effective and simple method for removing a sabot from a projectile, making it unnecessary to use split sabots or explosive charges to effect a removal. The remover may be adapted for use with guns of all sizes and projectiles and sabots of various types,
and is particularly suited for use with plastic and other non-metallic sabots, and sabots made of the light weight metals, although its use is not limited thereto.
It is to be understood that this invention is not restricted to the exact form depicted, and that modifications and changes may be made without departing from the scope of the invention.
I claim:
1. Means for removing a sabot from a projectile fired from a gun comprising a collar carried by the barrel of said gun at the forward end thereof, means forming an opening through said collar in axial alignment with the bore of said gun, scoring means carried within said opening and extending inwardly to a circumference less than the circumference of said barrel, said scoring means being spirally disposed with relation to the axis of said bore to simultaneously score said sabot and impart axial rotation thereto as said sabot passes through said collar.
2. A 'sabot remover adapted to 'fit the end of a gun barrel, 'said remover comprising a plurality of inwardly directed projections extending to lie on a circumference less than that of said gun barrel arranged to score and substantially weaken a sabot carried by a projectile leaving said 'gun barrel, said projections being spirally di-sposed so as to impart axial rotation to said weakened sabot and to develop centrifugal forces sufficient to fracture said sabot into a plurality of fragments and separate said fragments from said projectile.
3. A sabot remover adapted to be carried by the end of -a gun barrel comprising a plurality of inwardly extending projections, the inner edges thereof lying on a circumference concentric with and smaller than the bore of said gun, and means for attaching said remover to said gun barrel.
4. A sabot remover adapted to be carried by the end of a gun barrel comprising a plurality of inwardly extending projections, the inner edges of said projections encompassing a circumference concentric with and smaller than the bore of said gun barrel, said projections each being spirally directed about the longitudinal axis of said gun barrel, and means for attaching said remover to said gun barrel.
5. A sabot remover carried by the muzzle end of a gun barrel comprising a cylindrical collar, a central opening formed in said collar concentric with and axially aligned with the bore of said gun barrel, a plurality of spirally conformed projections extending longitudinally along the inner surface of said opening, said projections extending inwardly to .lie on a circumference less than that of said gun barrel to score and substantially weaken a sabot carried by a projectile fired from said gun barrel so that centrifugal forces-engendered by rotation of said sabot about the axis of flight of said projectile will fracture said sabot, and means for attaching said remover to said gun barrel.
References Cited in the file of this patent UNITED STATES PATENTS 478,020 Pollard June 28, 1892 569,190 Gathmann Oct. 13, 1896 868,938 Pufi Oct. 22, 1907 2,115,028 Logan Apr. 26, 1938
US451537A 1954-08-23 1954-08-23 Method and apparatus for sabot removal Expired - Lifetime US2811901A (en)

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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2968984A (en) * 1955-03-09 1961-01-24 Olin Mathieson Explosively actuated stud with a front guiding means with a tapered flange
US2984836A (en) * 1955-06-24 1961-05-23 Novotech Anstalt Firing tool with ammunition, more particularly for use as a pin driving tool
US2985074A (en) * 1958-03-28 1961-05-23 Musser C Walton Fluted flash hider
US3033116A (en) * 1958-05-20 1962-05-08 John L Critcher Ammunition
US3120185A (en) * 1962-05-25 1964-02-04 Henry S Lipinski Separate loading ammunition ramming assist
US3141412A (en) * 1961-05-18 1964-07-21 Elroy C Roehrdanz Sabots
US3148472A (en) * 1962-06-11 1964-09-15 Edward N Hegge Subcaliber projectile and sabot for high velocity firearms
US3212208A (en) * 1964-09-25 1965-10-19 Mario A Persechino Augmentor and sabot stripper for hypervelocity light gas gun
US3392472A (en) * 1967-06-30 1968-07-16 Army Usa Sabot remover with helically arranged ridges
US3430572A (en) * 1966-11-22 1969-03-04 Avco Corp Disintegrating sabot
US3490329A (en) * 1967-10-20 1970-01-20 Hilti Ag Bolt for explosive actuated bolt setter
US3951039A (en) * 1969-06-26 1976-04-20 Oy Tampella Ab Firearm with muzzle and smooth-bore barrel for firing finned projectiles
US4301737A (en) * 1979-10-04 1981-11-24 The United States Of America As Represented By The Secretary Of The Army Multi-purpose kinetic energy projectile
US4656919A (en) * 1985-01-08 1987-04-14 The United States Of America As Represented By The Secretary Of The Air Force Sabot/gun gas diverter
US4815682A (en) * 1987-07-20 1989-03-28 Pacific Armatechnica Corporation Fin-stabilized subcaliber projectile and method of spin tuning
US5452535A (en) * 1993-06-04 1995-09-26 Impromark, Inc. Shotgun shell wad/shot cup retarding device
RU2153140C1 (en) * 1999-06-07 2000-07-20 Открытое акционерное общество "Тульский оружейный завод" Muzzle attachment
US6128846A (en) * 1998-06-08 2000-10-10 Inpromark, Inc. Length shotgun choke tube
US10502515B2 (en) * 2017-01-17 2019-12-10 Raytheon Company Launch piston brake

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US478020A (en) * 1892-06-28 Cartridge
US569190A (en) * 1896-10-13 High-explosive projectile and gun for throwing same
US868938A (en) * 1907-07-25 1907-10-22 Carl Puff Barrel for portable firearms and cannon with deepened grooves.
US2115028A (en) * 1934-05-23 1938-04-26 Logan Orwell Projectile and gun

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US478020A (en) * 1892-06-28 Cartridge
US569190A (en) * 1896-10-13 High-explosive projectile and gun for throwing same
US868938A (en) * 1907-07-25 1907-10-22 Carl Puff Barrel for portable firearms and cannon with deepened grooves.
US2115028A (en) * 1934-05-23 1938-04-26 Logan Orwell Projectile and gun

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2968984A (en) * 1955-03-09 1961-01-24 Olin Mathieson Explosively actuated stud with a front guiding means with a tapered flange
US2984836A (en) * 1955-06-24 1961-05-23 Novotech Anstalt Firing tool with ammunition, more particularly for use as a pin driving tool
US2985074A (en) * 1958-03-28 1961-05-23 Musser C Walton Fluted flash hider
US3033116A (en) * 1958-05-20 1962-05-08 John L Critcher Ammunition
US3141412A (en) * 1961-05-18 1964-07-21 Elroy C Roehrdanz Sabots
US3120185A (en) * 1962-05-25 1964-02-04 Henry S Lipinski Separate loading ammunition ramming assist
US3148472A (en) * 1962-06-11 1964-09-15 Edward N Hegge Subcaliber projectile and sabot for high velocity firearms
US3212208A (en) * 1964-09-25 1965-10-19 Mario A Persechino Augmentor and sabot stripper for hypervelocity light gas gun
US3430572A (en) * 1966-11-22 1969-03-04 Avco Corp Disintegrating sabot
US3392472A (en) * 1967-06-30 1968-07-16 Army Usa Sabot remover with helically arranged ridges
US3490329A (en) * 1967-10-20 1970-01-20 Hilti Ag Bolt for explosive actuated bolt setter
US3951039A (en) * 1969-06-26 1976-04-20 Oy Tampella Ab Firearm with muzzle and smooth-bore barrel for firing finned projectiles
US4301737A (en) * 1979-10-04 1981-11-24 The United States Of America As Represented By The Secretary Of The Army Multi-purpose kinetic energy projectile
US4656919A (en) * 1985-01-08 1987-04-14 The United States Of America As Represented By The Secretary Of The Air Force Sabot/gun gas diverter
US4815682A (en) * 1987-07-20 1989-03-28 Pacific Armatechnica Corporation Fin-stabilized subcaliber projectile and method of spin tuning
US5452535A (en) * 1993-06-04 1995-09-26 Impromark, Inc. Shotgun shell wad/shot cup retarding device
US6128846A (en) * 1998-06-08 2000-10-10 Inpromark, Inc. Length shotgun choke tube
RU2153140C1 (en) * 1999-06-07 2000-07-20 Открытое акционерное общество "Тульский оружейный завод" Muzzle attachment
US10502515B2 (en) * 2017-01-17 2019-12-10 Raytheon Company Launch piston brake

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