US3927618A - Sabot projectile - Google Patents
Sabot projectile Download PDFInfo
- Publication number
- US3927618A US3927618A US416208A US41620873A US3927618A US 3927618 A US3927618 A US 3927618A US 416208 A US416208 A US 416208A US 41620873 A US41620873 A US 41620873A US 3927618 A US3927618 A US 3927618A
- Authority
- US
- United States
- Prior art keywords
- sabot
- projectile
- rear part
- sleeve
- shaped 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.)
- Expired - Lifetime
Links
- 230000002093 peripheral effect Effects 0.000 claims abstract description 19
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 241000282472 Canis lupus familiaris Species 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 229910001385 heavy metal Inorganic materials 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 239000012815 thermoplastic material Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/06—Sub-calibre projectiles having sabots; Sabots therefor
- F42B14/064—Sabots enclosing the rear end of a kinetic energy projectile, i.e. having a closed disk shaped obturator base and petals extending forward from said base
Definitions
- 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 sleeveshaped extension arranged at its front end and which is sub-divided by axially extending slots into segments.
- 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 fonns 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.
- 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.
- a further object of the 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.
- the inventive sabot projectile is generally manifested by the features that the segments of the sleeve-shaped extension of the sabot rear part embody radially inwardly directed projections or dogs which engage in the aforementioned peripheral groove.
- a sabot projectile comprising a sabot rear part and a sleeveshaped extension connected via a reference rupture location with the sabot rear part, said sleeve-shaped extension being subdivided into segments by slots uniformly distributed about the periphery of the extension.
- Each segment is provided at its outside surface with a blindhole bore having a base or bottom surface by means of which a thin-walled zone is formed at each segment. and a punched-out or stamped recess is pro- 2 vided at the base surface of each segment. Opposite each such recess there is formed a radially inwardly directed projection.
- a projectile body is mounted at the sabot rear part, said projectile body having a pe ripheral groove at its rear part which extends into the sleeve-shaped extension and into which groove there extends the aforesaid projections.
- the projectile or core body I illustrated in FIG. I is preferably formed from a heavy metal, has an essentially cylindrical configura' tion and possesses an ogive 2.
- the rear portion of the projectile body 1 bears by means of a forwardly widening conical surface 3 upon a similarly constructed bore surface 4 of a sabot rear part 5.
- the projectile body I 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 I.
- This sabot rear part5 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 I6 which intersects the jacket surface of the sabot rear part end 15, as shown.
- 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 I l.
- 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.
- 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 232 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 I6 of the sabot rear part 5 forms a ring 25 of substantially tongue-shaped cross-section.
- the jacket 23 also engages with the blind boreholes l9 and the recesses 21 of the sabot rear part 5.
- radially directed grooves 26 are cut from the outside up to the location of webs 3
- the grooves 26 extend rearwardly up to the height of the groove l2 of the sabot rear part 5.
- 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 1, 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 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.
- 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.
- the projectile body 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 s in.
- 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 part 5, 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.
- detachment of the segments 32 with the projections or tabs 22 from the projectile or core body I is aided by the inclination of the 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.
- a sabot projectile comprising a sabot rear part having a substantially sleeve-shaped extension, said sleeve-shaped extension being subdivided into a plurality of segments by slots uniformly distributed about the periphery of the sleeve-shaped extension, each segment being provided at its outside surface with a blindhole bore having a base surface by means of which there is formed a thin-walled zone at each segment, and a stamped recess provided at the base surface of each segment wherein opposite each such recess there is formed a radially inwardly directed projection, a projectile body mounted at the sabot rear part, said projectile body having a peripheral groove at its rear portion which extends into the sleeve-shaped extension, said radially inwardly directed projections engaging with said peripheral groove of said projectile body.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
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.
Description
D United States Patent 1 1 1111 Engel Dec. 23, 1975 SABOT PROJECTILE 3,000,316 9/1961 Dunlap et al. 102/93 3.055.268 9/l962 Rosenthal [02/93 X [75] Inventor Engel Dubendorf 3,359,905 l2/l967 Engel 1. 102/93 Switzerland 3,447.466 6/1969 Engel .1 102/93 73 I 3.496,869 2/1970 Engel [02/93 1 Asslgnee g i fzxfi fi r'fg gg 3,551,972 1/1971 Engel 102/93 9 9 Switzerland Primary Exam1nerStephen C. Bentley Flledi 1973 Assistant ExaminerC. T. Jordan [2]] AppL 416,208 Attorney, Agent, or Firm-Werner W. Kleeman [62] Related US. Application Data [57] ABSTRACT gg g fgs-i March 1972 A sabot projectile comprising a projectile body having at least one peripheral groove and a sabot incorporat- [52] US. Cl. 102/93 ing a Sabot rear Pan having a Substantially sleeve 51 1111. 13/16 Shaped extension arranged from The [58] Field 61 Search 102/93 Sic) is subdivided into Segments by means of Substa" tially axially extending slots, and such segments pos- [56] References Cited sess radially inwardly directed projections or tabs UNITED STATES PATENTS which are pressed into such peripheral groove 2,994,274 7/1961 Dunlap 102/93 5 Claims 2 Drawing Figures 27 f r i ll l l 1 y i i i It 1- I i i 233-16, 26
,a- M: i 23 Q 7 6 j 9 l7 9...; 1 r 8 M" i; M 23652 in 2/ l 12 US. Patent Dec. 23, 1975 3,927,618
Fig.1 X 50 Fig.2
SABOT PROJECTILE CROSS-REFERENCE TO RELATED CASE:
This is a divisional application of my copending, commonly assigned US. application Ser. No. 231,867, filed Mar. 6, 1972 now US. Pat. No. 3,837,057.
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 sleeveshaped extension arranged at its front end and which is sub-divided by axially extending slots into segments.
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 fonns 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 of the 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.
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 generally manifested by the features that the segments of the sleeve-shaped extension of the sabot rear part embody radially inwardly directed projections or dogs which engage in the aforementioned peripheral groove.
In its more specific aspects there is disclosed a sabot projectile comprising a sabot rear part and a sleeveshaped extension connected via a reference rupture location with the sabot rear part, said sleeve-shaped extension being subdivided into segments by slots uniformly distributed about the periphery of the extension. Each segment is provided at its outside surface with a blindhole bore having a base or bottom surface by means of which a thin-walled zone is formed at each segment. and a punched-out or stamped recess is pro- 2 vided at the base surface of each segment. Opposite each such recess there is formed a radially inwardly directed projection. A projectile body is mounted at the sabot rear part, said projectile body having a pe ripheral groove at its rear part which extends into the sleeve-shaped extension and into which groove there extends the aforesaid projections.
BRIEF DESCRIPTION OF THE DRAWING DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Describing now the drawing, the projectile or core body I illustrated in FIG. I is preferably formed from a heavy metal, has an essentially cylindrical configura' tion and possesses an ogive 2. The rear portion of the projectile body 1 bears by means of a forwardly widening conical surface 3 upon a similarly constructed bore surface 4 of a sabot rear part 5. The projectile body I 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 I. This sabot rear part5 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 I6 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 I l. 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. 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 having a substantially square or quadratic crosssection. The recesses 21 are thus located at thin-wall zones of the sabot rear part 5 which are bounded by thicker rein forcement locations or portions. The material displaced by the punch forms projections or tabs 22 which protrude into the peripheral grooves 7 of the projectile body 1.
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 232 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 I6 of the sabot rear part 5 forms a ring 25 of substantially tongue-shaped cross-section. The jacket 23 also engages with 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 3| at the jacket 23. The grooves 26 extend rearwardly up to the height of the groove l2 of the sabot rear part 5. 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 1, 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 projectile and is as follows: When a cartridge delivered to the breech-block of an automatic weapon comes to a sudden stop at the 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 projections, dogs or tabs 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 projectile body 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 s in.
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 300 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 bearing against the wall of the gun bore are forwardly displaced by the jacket 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 part 5, 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 projections or tabs 22 from the projectile or core body I is aided by the inclination of the 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.
What is claimed is:
l. A sabot projectile comprising a sabot rear part having a substantially sleeve-shaped extension, said sleeve-shaped extension being subdivided into a plurality of segments by slots uniformly distributed about the periphery of the sleeve-shaped extension, each segment being provided at its outside surface with a blindhole bore having a base surface by means of which there is formed a thin-walled zone at each segment, and a stamped recess provided at the base surface of each segment wherein opposite each such recess there is formed a radially inwardly directed projection, a projectile body mounted at the sabot rear part, said projectile body having a peripheral groove at its rear portion which extends into the sleeve-shaped extension, said radially inwardly directed projections engaging with said peripheral groove of said projectile body.
4. The sabot projectile as defined in claim 1, wherein the sleeve-shaped extension is connected with the sabot rear part by means of a reference rupture location which possesses an external groove, an inner groove arranged opposite said external groove.
5. The sabot projectile as defined in claim 1, wherein said projections are angularly spaced about the peripheral groove.
Claims (5)
1. A sabot projectile comprising a sabot rear part having a substantially sleeve-shaped extension, said sleeve-shaped extension being subdivided into a plurality of segments by slots uniformly distributed about the periphery of the sleeve-shaped extension, each segment being provided at its outside surface with a blindhole bore having a base surface by means of which there is formed a thin-walled zone at each segment, and a stamped recess provided at the base surface of each segment wherein opposite each such recess there is formed a radially inwardly directed projection, a projectile body mounted at the sabot rear part, said projectile body having a peripheral groove at its rear portion which extends into the sleeve-shaped extension, said radially inwardly directed projections engaging with said peripheral groove of said projectile body.
2. The sabot projectile as defined in claim 1, wherein the base surface of each blindhole bore is substantially flat.
3. The sabot projectile as defined in claim 1, wherein the peripheral groove incorporates flank means forming portions of conical surfaces, said conical surfaces defining a front conical surface and a rear conical surface, the angle of opening of the front conical surface being smaller than the angle of opening of the rear conical surface.
4. The sabot projectile as defined in claim 1, wherein the sleeve-shaped extension is connected with the sabot rear part by means of a reference rupture location which possesses an external groove, an inner groove arranged opposite said external groove.
5. The sabot projectile as defined in claim 1, wherein said projections are angularly spaced about the peripheral groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US416208A US3927618A (en) | 1971-03-29 | 1973-11-15 | Sabot projectile |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH455771A CH536481A (en) | 1971-03-29 | 1971-03-29 | Sabot bullet and process for its manufacture |
| US416208A US3927618A (en) | 1971-03-29 | 1973-11-15 | Sabot projectile |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3927618A true US3927618A (en) | 1975-12-23 |
Family
ID=25695750
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US416208A Expired - Lifetime US3927618A (en) | 1971-03-29 | 1973-11-15 | Sabot projectile |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3927618A (en) |
Cited By (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4142467A (en) * | 1976-07-09 | 1979-03-06 | Dynamit Nobel Aktiengesellschaft | Projectile with sabot |
| DE2919807A1 (en) * | 1978-05-30 | 1979-12-06 | Oerlikon Buehrle Ag | SPIRAL STABILIZED DRIVING LEVEL FLOOR TO OVERCOME HETEROGENIC RESISTANCE |
| JPS62210398A (en) * | 1986-03-07 | 1987-09-16 | ウエルクツオイクマシイネンフアブリ−ク・エ−リコン−ビユ−レ・アクチエンゲゼルシヤフト | Coupling structure of discarding sabot sheath and discarding sabot tail section of discarding sabot projectile |
| US4719860A (en) * | 1987-01-28 | 1988-01-19 | Honeywell Inc. | Armor-penetrating ammunition assembly with molded protective cap |
| US4750425A (en) * | 1986-03-21 | 1988-06-14 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Sabot projectile with a sabot tail to which an attachment sleeve is fastened through a reference fracture location |
| US4773331A (en) * | 1981-08-13 | 1988-09-27 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Connection arrangement between a sabot jacket and the sabot rear portion of a sabot projectile |
| US4776280A (en) * | 1987-04-30 | 1988-10-11 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Sabot projectile containing a sabot rear portion having reference fracture locations |
| EP0275685A3 (en) * | 1986-12-24 | 1988-12-28 | Royal Ordnance Plc | Discarding sabots |
| US4920889A (en) * | 1987-07-23 | 1990-05-01 | Rheinmetall Gmbh | Fin stabilized, subcaliber propelling cage sobot projectile |
| CH675769A5 (en) * | 1988-06-15 | 1990-10-31 | Oerlikon Buehrle Ag | Sectored head on detachable sabot - shatters with retainer ring having breakage grooves immediately after release on firing |
| US5016538A (en) * | 1987-03-30 | 1991-05-21 | Olin Corporation | Sabot bullet |
| WO1991013313A1 (en) * | 1990-02-27 | 1991-09-05 | Olin Corporation | Sabot bullet |
| US5052305A (en) * | 1989-10-26 | 1991-10-01 | L'etat Francais Represente Par Le Delegue Ministeriel Pour L'armement | Subcaliber projectile including a core, a sabot and a sleeve |
| US5175389A (en) * | 1992-01-07 | 1992-12-29 | Federal-Hoffman, Inc. D/B/A Federal Cartridge Co. | Frontally guided sabot bullet |
| US5175394A (en) * | 1987-03-30 | 1992-12-29 | Olin Corporation | Sabot bullet |
| US5481980A (en) * | 1993-05-27 | 1996-01-09 | Oerlikon-Contraves Pyrotec Ag | Releasable sabot for a subcaliber projectile |
| EP0999426A1 (en) * | 1998-11-06 | 2000-05-10 | Oerlikon Contraves Pyrotec AG | Sabot for sub-caliber projectile |
| US20130312631A1 (en) * | 2010-09-16 | 2013-11-28 | Rheinmetall Waffe Munition Gmbh | Projectile having a discardable sabot |
| US9188417B2 (en) * | 2013-08-01 | 2015-11-17 | Raytheon Company | Separable sabot for launching payload |
| US9488455B1 (en) * | 2015-01-22 | 2016-11-08 | Consolidated Nuclear Security, LLC | Sabot assembly |
| US20190162512A1 (en) * | 2017-11-24 | 2019-05-30 | Nexter Munitions | Projectile |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2994274A (en) * | 1944-06-30 | 1961-08-01 | Henry F Dunlap | Projectile |
| US3000316A (en) * | 1944-07-10 | 1961-09-19 | Henry F Dunlap | Projectile |
| US3055268A (en) * | 1960-12-08 | 1962-09-25 | Rosenthal Henry | Discarding obturator and rotator for projectiles |
| US3359905A (en) * | 1965-04-01 | 1967-12-26 | Oerlikon Buehrle Holding Ag | Sabot projectile |
| US3447466A (en) * | 1967-09-05 | 1969-06-03 | Oerlikon Buhrie Holding Ltd | Sabot projectile with core guiding means |
| US3496869A (en) * | 1967-07-28 | 1970-02-24 | Oerlikon Buehrle Holding Ag | Sabot projectile |
| US3551972A (en) * | 1967-07-24 | 1971-01-05 | Oerlikon Buehrle Holding Ag | Method of manufactring a sabot |
-
1973
- 1973-11-15 US US416208A patent/US3927618A/en not_active Expired - Lifetime
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2994274A (en) * | 1944-06-30 | 1961-08-01 | Henry F Dunlap | Projectile |
| US3000316A (en) * | 1944-07-10 | 1961-09-19 | Henry F Dunlap | Projectile |
| US3055268A (en) * | 1960-12-08 | 1962-09-25 | Rosenthal Henry | Discarding obturator and rotator for projectiles |
| US3359905A (en) * | 1965-04-01 | 1967-12-26 | Oerlikon Buehrle Holding Ag | Sabot projectile |
| US3551972A (en) * | 1967-07-24 | 1971-01-05 | Oerlikon Buehrle Holding Ag | Method of manufactring a sabot |
| US3496869A (en) * | 1967-07-28 | 1970-02-24 | Oerlikon Buehrle Holding Ag | Sabot projectile |
| US3447466A (en) * | 1967-09-05 | 1969-06-03 | Oerlikon Buhrie Holding Ltd | Sabot projectile with core guiding means |
Cited By (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4142467A (en) * | 1976-07-09 | 1979-03-06 | Dynamit Nobel Aktiengesellschaft | Projectile with sabot |
| DE2919807A1 (en) * | 1978-05-30 | 1979-12-06 | Oerlikon Buehrle Ag | SPIRAL STABILIZED DRIVING LEVEL FLOOR TO OVERCOME HETEROGENIC RESISTANCE |
| US4437409A (en) | 1978-05-30 | 1984-03-20 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Spin-stabilized sabot projectile for overcoming a heterogeneous resistance |
| US4846072A (en) * | 1981-08-13 | 1989-07-11 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Connection arrangement between a sabot jacket and the rear portion of a sabot projectile |
| US4773331A (en) * | 1981-08-13 | 1988-09-27 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Connection arrangement between a sabot jacket and the sabot rear portion of a sabot projectile |
| JPS62210398A (en) * | 1986-03-07 | 1987-09-16 | ウエルクツオイクマシイネンフアブリ−ク・エ−リコン−ビユ−レ・アクチエンゲゼルシヤフト | Coupling structure of discarding sabot sheath and discarding sabot tail section of discarding sabot projectile |
| US4750425A (en) * | 1986-03-21 | 1988-06-14 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Sabot projectile with a sabot tail to which an attachment sleeve is fastened through a reference fracture location |
| EP0275685A3 (en) * | 1986-12-24 | 1988-12-28 | Royal Ordnance Plc | Discarding sabots |
| US4719860A (en) * | 1987-01-28 | 1988-01-19 | Honeywell Inc. | Armor-penetrating ammunition assembly with molded protective cap |
| US5016538A (en) * | 1987-03-30 | 1991-05-21 | Olin Corporation | Sabot bullet |
| US5175394A (en) * | 1987-03-30 | 1992-12-29 | Olin Corporation | Sabot bullet |
| US4776280A (en) * | 1987-04-30 | 1988-10-11 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Sabot projectile containing a sabot rear portion having reference fracture locations |
| US4920889A (en) * | 1987-07-23 | 1990-05-01 | Rheinmetall Gmbh | Fin stabilized, subcaliber propelling cage sobot projectile |
| CH675769A5 (en) * | 1988-06-15 | 1990-10-31 | Oerlikon Buehrle Ag | Sectored head on detachable sabot - shatters with retainer ring having breakage grooves immediately after release on firing |
| US5052305A (en) * | 1989-10-26 | 1991-10-01 | L'etat Francais Represente Par Le Delegue Ministeriel Pour L'armement | Subcaliber projectile including a core, a sabot and a sleeve |
| WO1991013313A1 (en) * | 1990-02-27 | 1991-09-05 | Olin Corporation | Sabot bullet |
| US5103736A (en) * | 1990-02-27 | 1992-04-14 | Olin Corporation | Sabot bullet |
| US5175389A (en) * | 1992-01-07 | 1992-12-29 | Federal-Hoffman, Inc. D/B/A Federal Cartridge Co. | Frontally guided sabot bullet |
| US5481980A (en) * | 1993-05-27 | 1996-01-09 | Oerlikon-Contraves Pyrotec Ag | Releasable sabot for a subcaliber projectile |
| EP0999426A1 (en) * | 1998-11-06 | 2000-05-10 | Oerlikon Contraves Pyrotec AG | Sabot for sub-caliber projectile |
| US6324986B1 (en) | 1998-11-06 | 2001-12-04 | Oerlikon Contraves Ag | Cartridge-case base for a sub-caliber projectile |
| US20130312631A1 (en) * | 2010-09-16 | 2013-11-28 | Rheinmetall Waffe Munition Gmbh | Projectile having a discardable sabot |
| US9528806B2 (en) * | 2010-09-16 | 2016-12-27 | Rwm Schweiz Ag | Projectile having a discardable sabot |
| US9188417B2 (en) * | 2013-08-01 | 2015-11-17 | Raytheon Company | Separable sabot for launching payload |
| US9488455B1 (en) * | 2015-01-22 | 2016-11-08 | Consolidated Nuclear Security, LLC | Sabot assembly |
| US20190162512A1 (en) * | 2017-11-24 | 2019-05-30 | Nexter Munitions | Projectile |
| US10520290B2 (en) * | 2017-11-24 | 2019-12-31 | Nexter Munitions | Projectile |
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