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Publication numberUS3837057 A
Publication typeGrant
Publication dateSep 24, 1974
Filing dateMar 6, 1972
Priority dateMar 29, 1971
Also published asCA957560A1, DE2212853A1, DE2212853B2
Publication numberUS 3837057 A, US 3837057A, US-A-3837057, US3837057 A, US3837057A
InventorsEngel W
Original AssigneeOerlikon Buehrle Ag
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Method for securing a projectile in a sabot
US 3837057 A
Abstract
A sabot projectile comprising a projectile body having at least one peripheral groove and a sabot incorporating a sabot rear part having a substantially sleeve-shaped extension arranged at its front end. The extension is sub-divided into segments by means of substantially axially extending slots, and such segments possess radially inwardly directed projections or tabs which are pressed into such peripheral groove.
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Description  (OCR text may contain errors)

United States Patent 1 Engel 1451 Sept. 24, 1974 METHOD FOR SECURING A PROJECTILE IN A SABOT [75] Inventor: Walter Engel, Dubendorf,

Switzerland [73] Assignee: Werkzeugmaschinenfabrik Oerlikon-Buhrle AG, Zurich, Switzerland [22] Filed: Mar. 6, 1972 [21] Appl. No.1 231,867

[30] Foreign Application Priority Data Mar. 29, 1971 Switzerland 4557/71 [52] US. Cl. 29/l.2, 29/l.3 [51] Int. Cl B21k 21/06 [58] Field of Search 29/1.2, 1.21, 1.22, 1.23, 29/1.3, 516, 519; 10/86 F [56] References Cited UNITED STATES PATENTS 930,863 8/1909 Kearney 29/l.2 UX 2,349,677 5/1944 Reynolds 29/1.22 2,792,618 5/1957 Walker 29/l.23 3,349,459 10/1967 King et al. 29/l.3 3,349,711 10/1967 Darigo 29/l.23 X

Rusche 29/516 X Engel 29/1.23

Primary Examiner-Andrew R. Juhasz Assistant Examiner-Leon Gilden Attorney, Agent, or Firm-Werner W. Kleeman 5 7 ABSTRACT A sabot projectile comprising a projectile body having at least one peripheral groove and a sabot incorporating a sabot rear part having a substantially sleeveshaped extension arranged at its front end. The extension is sub-divided into segments by means of substantially axially extending slots, and such segments possess radially inwardly directed projections or tabs which are pressed into such peripheral groove.

3 Claims, 5;Drawing Figures 1 1 zen 6 22 9 f 2| I 11 F METHOD FOR SECURING A PROJECTILE IN A SABOT BACKGROUND OF THE INVENTION The present invention relates to a new and improved construction of sabot projectile embodying a projectile body having at least one peripheral groove and with a sabot rear part containing a sleeve-shaped extension arranged at its front end and which is sub-divided by axially extending slots into segments. A further aspect of this development also pertains to a new and improved method of securing a projectile body in a sabot.

With a known sabot projectile of this general type a ring consisting of a number of segments is arranged in a peripheral groove, this ring bearing upon a rear flank of the groove. The ring protrudes outwardly past the diameter of the projectile body and forms the bearing support for a forwardly projecting sleeve formed from a number of segments. A sleeve-shaped projection or extension of the rear part surrounds the aforementioned sleeve. The extension is provided with axially-extending slots and is inwardly flanged at its front end, thereby preventing forward displacement of the sleeve. Upon introducing a cartridge containing such type projectile into the cartridge chamber of an automatic weapon the forces acting at the projectile body are transmitted via the ring, the sleeve and the sleeveshaped projection to the sabot. The rear part preferably consists of an aluminum alloy, for instance Perunal, which characterizes itself on the one hand by lower weight and on the other hand by high mechanical strength, something which is important because of the larger inertia forces acting during firing.

SUMMARY OF THE INVENTION It is a primary object of the present invention to provide a projectile formed of fewer parts and therefore less expensive to manufacture, and by means of which there is ensured for positive separation of the sabot rear part from the projectile body after leaving the weapon bore or barrel.

A further object ofthe present invention relates to an improved sabot projectile having novel means for connecting the projectile body with the sabot.

Still a further significant object of the present invention relates to sabot projectiles which are less complicated in design and more economical to manufacture.

A further significant object of the present invention relates to a novel method of securing a projectile body to a sabot in a reliable and economical fashion with a minimum of components for providing the connection.

Now, in order to implement these and still further objects of the invention, which will become more readily apparent as the description proceeds, the inventive sabot projectile is manifested by the features that the segments of the sleeve-shaped extension of the sabot rear part embody radially inwardly directed tabs or dogs which engage in the aforementioned peripheral groove.

The method aspects of this development for attaching a projectile body with a sabot having a sleeveshaped extension into which is inserted the projectile body and by deformation of such sleeve-shaped extension the projectile body is secured to the sabot rear part, is manifested by the features that material is pressed from the sleeveshaped extension into the peripheral groove of the projectile body, this material forming tabs or dogs which enter into the peripheral groove of the projectile body to thereby establish the aforementioned connection.

BRIEF DESCRIPTION OF THE DRAWINGS The invention will be better understood and objects other than those set forth above, will become apparent when consideration is given to the following detailed description thereof. Such description makes reference to the annexed drawings wherein:

FIG. 1 is a longitudinal sectional a sabot projectile designed according to the teachings of the present invention, and taken substantially along the line II of FIG. 2;

FIG. 2 is a cross-sectional view of the sabot projectile of FIG. 1, taken substantially along the line IIII thereof;

FIG. 3 illustrates in cross-section view the projectile body located at the rear portion of the sabot but prior to its attachment therewith;

FIG. 4 is a cross-sectional view, similar to the showing of FIG. 3 but illustrating the projectile body after its attachment with the rear portion of the sabot; and

FIG. 5 is a front view of the punch used for securing the projectile body at the sabot rear part, and seen looking in the direction of the arrow A of FIG. 1.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Describing now the drawings, the projectile or core body 1 illustrated in FIG. 1 is preferably formed from a heavy metal, has an essentially cylindrical configuration and possesses an ogive 2. The rear portion of the projectile body 1 bears by means ofa forwardly widening conical surface 3 upon a similarly constructed bore surface 4 of a sabot rear part 5. The projectile body 1 is provided at its rear portion with two peripheral or circumferential grooves 7. The flanks of the peripheral grooves 7 constitute parts of conical surfaces. The rear conical surface 8 opens towards the rear and the front conical surface 9 towards the front. The aperture angle or angle of opening of the rear conical surface 8 is greater than that of the front surface 9 and only slightly less than The sabot rear part 5 possesses a sleeve-shaped extension or projection 6 into which protrudes the rear part of the projectile or core body 1. This sabot rear part 5 is preferably formed from an aluminum alloy, for instance Perunal. Sabot rear part 5 possesses a ringshaped groove 11 machined at the region of a central bore 10 and an externally cut peripheral groove 12. The flanks of groove 12 are located at intersecting cone surfaces. A rear groove flank 13 is intersected by a further rearwardly extending and forwardly opening conical surface 14, the diameter of the line of intersection of both surfaces 13 and 14 being less than the outside diameter of the rear end 15 of the sabot rear part 5. Furthermore, the conical surface 14 intersects a forwardly opening conical surface 16 which intersects the jacket surface of the sabot rear part end 15, as shown.

Now from the end face six axially extending slots 17 arranged at'regular angular intervals extend into the extension 6 of the sabot rear part 5 up to the location of a plane 18 which is perpendicular to the projectile axis, so that extension 6 is subdivided into six segments 32. Plane 18 is disposed rearwardly of the peripheral grooves 7 of the projectile body 1 and contains the cutting line or point of intersection of the flanks of the groove 12 and the plane of symmetry of the groove 11. The segments 32 of the sabot rear part 5 are provided at the outside with conical blind bores or boreholes 19 having flat or planar base surfaces 190. At these planar base surfaces, which are disposed perpendicular to the radially directed axis of the blind boreholes 19, there are impressed two recesses 21 by means of a punch 35 having a substantially square or quadratic crosssection. The recesses 21 are thus located at thin-wall zones of the sabot rear part 5. The material displaced by the punch forms tabs or dogs or projections 22 which protrude ,into the peripheral grooves 7 of the v projectile body 1.

In consideration of the above it will be recognized that the projectile body 1 is secured to the sabot rear part 5 by carrying out by the following working operations of the method: initially the projectile body 1 is inserted into the sabot rear part 5 in the manner depicted on FIG. 3. As previously discussed each segment 32 of the sabot rear part 5 possesses at the outside or outer surface a conical blindhole bore 19 with flat bottom or base surface 19a, thus providing a thin-walled zone 20 at such segment 32. Thereafter, in each flat bottom or base surface 19a, which is disposed perpendicular to the radially directed axis of the blindhole bore 19, there are punched-in two recesses ordepressions 21 by means of the respective associated punch 35 or other suitable tool equipped with two projections 34, as best seen by referring to FIGS. 3 and 5. These projections 34 of the punch 35 have a quadratic or square crosssection. The material displaced by the projections 34 of the punch 35, at the peripheral grooves 7 of the projectile body 1, form the inwardly extending projections or tabs 22, as best recognized by referring to FIGS. 2 and 4.

The cylindrical part la of the projectile or core body 1 which is not inserted into the extension 6 of the sabot rear part 5 is enclosed by a jacket 23 which extends up to a point forward of the rear end of the ogive 2. Jacket 23 is preferably formed, as by injection molding, from a thermoplastic material designated as nylon 6.6, and is a material known'in the art. The front portion 23a of the jacket 23 is cylindrical, whereas the rear portion 23b has the form of a truncated cone which tapers slightly from the rear towards the front. The diameter of the front edge of the truncated cone portion 23b is greater than the diameter of the cylindrical jacket portion 23a so that the rear part of the jacket 23 forms a collar-shaped widened portion 24 of such jacket. This widened portion 24 forms the guide or driving band, which upon passing through the gun or weapon bore, transmits spin or rotational movement to the jacket 23. The rearmost portion of the jacket 23 contacting the surfaces 14 and 16 of the sabot rear part 5 forms a ring 25 of substantially tongue-shaped cross-section. The jacket 23 also engageswith the blind boreholes l9 and the recesses 21 of the sabot rear part 5. As clearly evident from the drawing radially directed grooves 26 are cut from the outside up to the location of webs 31 at the jacket 23. The grooves 26 extend rearwardly up to the height of the groove 12 of-the sabot rear part5. The plane of symmetry of the grooves 26 coincide with those of the slots 17 of the sabot rear part 5.

A hood member 27 formed of plastic and extending forwardly of the jacket 23 is constructed in the form of a hollow body which is tapered or conically formed at its front. part and widens rearwardly to the diameter of the jacket 23. Hood member 27 terminates forwardly of the ogive or tip 2 of the projectile body I, encloses the ogive and is spaced therefrom, and is connected with the jacket 23 in such a way that an inwardly projecting flange 28 which bounds such hood member towards the rear engages with a groove 29 cut throughout the entire periphery of the jacket 23. The hood member 27 is sealed at its front end by a thin cover member 30 extending transversely with respect to the lengthwise axis of the hood member 27 and formed integral with the remaining part of the hood member 27. The circular-shaped junction location 30a of this cover member 30 forms an intended rupture location.

The mode of functioning should be apparent from the described construction of the inventive sabot pro- I jectile and is as follows: When a cartridge delivered to the breech-block of an automatic weapon comes to a sudden stop atthe cartridge chamber at the end of the loading operation, then the projectile or core body 1, owing to its forwardly directed inertia, comes to rest with its rear groove flanks 8 defining support or bearing locations via the tabs or projections 22 at the sabot rear part 5.

At the beginning of the movement of the projectile, following ignition of the propellent charge, the lands of the gun bore not illustrated in the drawing, cut into the driving or guide band 24 so that the jacket 23 is placed into rotation or spin. At the same time the rear part of the driving band 24 disposed at the height of the conical surface 14 of the sabot rear part 5 is subjected to deformation in radial direction. Under the action of the force brought about by this deformation and exerted by the conical surface 14 upon the jacket 23 there is produced a frictional force by means of which there is transmitted the spin of the jacket 23 to the sabot rear part 5. During acceleration of the projectile the projectilebody 1 is pressed against the support formed by the support surface 4 of the sabot rear part 5 and owing to the thus engaging frictional force is likewise placed into spin.

By virtue of the pressure head acting during firing upon the cover member 30 of the hood member 27 within the weapon barrel such cover member is separated along the intended fracture or rupture line 30a from the hood member 27 and thrown rearwardly, so that now the pressure also acts at the inside of the hood member 27. With increasing spinning speed the hood member 27 is destructed or torn apart by the centrifugal forces acting on it so that the fractured pieces hearing against the wall of the gun bore are forwardly displaced by thejacket 23. After the projectile has left the gun bore the jacket 23, under the action of the centrifugal force, disintegrates into outwardly moving segments, disintegration or break-up of the jacket occurring along the intended rupture locations formed by the grooves 26 bounded by the webs 31. The segments detach from the rearmost part 25 of the jacket 23 anchored at the sabot rear part 5. Thereafter, the segments 32 of the extension 6 of the sabot rear part5, and

which segments are bounded by the slots 17, are outwardly rocked or pivoted by the centrifugal forces at their intended rupture locations located at the groove 11 and the transverse plane 18, and torn away along such intended rupture locations. In this regard detachment of the segments 32 with the tabs or projections 22 from the projectile or core body 1 is aided by the inclination ofthe flanks 8 and 9 of its grooves 7. The projectile body 1 now is completely free and moves independently of the rear part 5 forwardly thereof, since there acts upon the projectile body 1 a smaller air resistance than at the rear part 5.

While there is shown and described present preferred embodiments of the invention, it is to be distinctly understood that the invention is not limited thereto but may be otherwise variously embodied and practiced within the scope of the following claims.

I claim:

1. A method for attaching a projectile body as a substantially sleeve-shaped extension of a sabot rear part, which is divided into segments comprising the steps of:

thin-wall zones;

c. inserting the projectile body into the sleeve-shaped extension of the sabot rear part; and

d. displacing material out of the thin-wall zones into the peripheral groove of the projectile body inserted into the sleeve-shaped extension of the sabot rear part, and forming recesses at the bottom surfaces of the blindhole bore, said recesses being formed by deforming the flat bottom surfaces of the blindhole bores with respect to the peripheral groove of the projectile body, to thereby secure the projectile body in said sleeve-shaped extension of the sabot rear part.

2. The method as defined in claim 1 wherein said projectile body includes a plurality of spaced peripheral grooves, and said blindhole bores with flat bottom surfaces are formed in the sabot rear part in sufficient numbers to provide, after deformation, securing tabs which extend into each of said projectile peripheral grooves.

3. The method as defined in claim 1, including the step of forming said recesses with their associated displaced material so as to be substantially uniformly distributed about the periphery of the sleeve-shaped extension of the sabot rear part.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US930863 *Dec 9, 1907Aug 10, 1909Thomas Albert KearneyProcess for banding projectiles.
US2349677 *Oct 31, 1939May 23, 1944Ira J McculloughMethod of making projectiles
US2792618 *Nov 23, 1953May 21, 1957Woodrow A WalkerMethod of construction of dual jacket partition bullets
US3349459 *Dec 30, 1965Oct 31, 1967Fed Cartridge CorpMethod of making plastic tubes
US3349711 *Dec 7, 1964Oct 31, 1967Remington Arms Co IncProcess of forming jacketed projectiles
US3453831 *Jan 25, 1968Jul 8, 1969Rusche FredricMethod of forming and driving thin wall pipe pile and boot
US3551972 *Oct 11, 1968Jan 5, 1971Oerlikon Buehrle Holding AgMethod of manufactring a sabot
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US4351094 *Jul 23, 1979Sep 28, 1982Werkzeugmaschinenfabrik Oerlikon-Buhrle AgMethod of manufacturing a sabot projectile and sabot projectile produced thereby
US4419796 *Sep 24, 1981Dec 13, 1983Honeywell Inc.Method of making spin stabilized discarding sabot projectile
US4982669 *Feb 3, 1989Jan 8, 1991Rheinmetall GmbhSubcaliber discarding sabot projectile
Classifications
U.S. Classification86/52
International ClassificationF42B14/06, F42B14/00
Cooperative ClassificationF42B14/064
European ClassificationF42B14/06D