US3750578A - Expellable cartridge case - Google Patents
- ️Tue Aug 07 1973
US3750578A - Expellable cartridge case - Google Patents
Expellable cartridge case Download PDFInfo
-
Publication number
- US3750578A US3750578A US00215364A US3750578DA US3750578A US 3750578 A US3750578 A US 3750578A US 00215364 A US00215364 A US 00215364A US 3750578D A US3750578D A US 3750578DA US 3750578 A US3750578 A US 3750578A Authority
- US
- United States Prior art keywords
- projectile
- casing
- cartridge
- propellant gases
- weapon Prior art date
- 1972-01-04 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
- 239000003380 propellant Substances 0.000 claims abstract description 44
- 239000007789 gas Substances 0.000 claims abstract description 38
- 239000000203 mixture Substances 0.000 claims abstract description 14
- 238000010304 firing Methods 0.000 claims description 10
- 239000004033 plastic Substances 0.000 claims description 10
- 229920003023 plastic Polymers 0.000 claims description 10
- 229920000098 polyolefin Polymers 0.000 claims description 3
- 238000000926 separation method Methods 0.000 claims description 2
- 239000000700 radioactive tracer Substances 0.000 abstract description 9
- 239000012634 fragment Substances 0.000 abstract description 8
- 229940090045 cartridge Drugs 0.000 description 32
- -1 polypropylene Polymers 0.000 description 11
- 239000000463 material Substances 0.000 description 8
- 239000004743 Polypropylene Substances 0.000 description 7
- 229920001155 polypropylene Polymers 0.000 description 7
- 239000004698 Polyethylene Substances 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 229920000573 polyethylene Polymers 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 229920005989 resin Polymers 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- 239000000020 Nitrocellulose Substances 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 2
- 229920001903 high density polyethylene Polymers 0.000 description 2
- 239000004700 high-density polyethylene Substances 0.000 description 2
- 239000003999 initiator Substances 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 229920001220 nitrocellulos Polymers 0.000 description 2
- 229920001778 nylon Polymers 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 238000009987 spinning Methods 0.000 description 2
- 241000270281 Coluber constrictor Species 0.000 description 1
- 229910000562 Gilding metal Inorganic materials 0.000 description 1
- 229930182556 Polyacetal Natural products 0.000 description 1
- 208000036366 Sensation of pressure Diseases 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- OQZCSNDVOWYALR-UHFFFAOYSA-N flurochloridone Chemical compound FC(F)(F)C1=CC=CC(N2C(C(Cl)C(CCl)C2)=O)=C1 OQZCSNDVOWYALR-UHFFFAOYSA-N 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000002655 kraft paper Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000002985 plastic film Substances 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920001225 polyester resin Polymers 0.000 description 1
- 239000004645 polyester resin Substances 0.000 description 1
- 229920006324 polyoxymethylene Polymers 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 239000002341 toxic gas Substances 0.000 description 1
- CYRMSUTZVYGINF-UHFFFAOYSA-N trichlorofluoromethane Chemical compound FC(Cl)(Cl)Cl CYRMSUTZVYGINF-UHFFFAOYSA-N 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/10—Cartridges, i.e. cases with charge and missile with self-propelled bullet
- F42B5/105—Cartridges, i.e. cases with charge and missile with self-propelled bullet propelled by two propulsive charges, the rearwardly situated one being separated from the rest of the projectile during flight or in the barrel; Projectiles with self-ejecting cartridge cases
-
- 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
- F42B14/061—Sabots for long rod fin stabilised kinetic energy projectiles, i.e. multisegment sabots attached midway on the projectile
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/067—Mounting or locking missiles in cartridge cases
- F42B5/073—Mounting or locking missiles in cartridge cases using an auxiliary locking element
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S102/00—Ammunition and explosives
- Y10S102/703—Flechette
Definitions
- the cartridge has an open ended casing attached by means of U.S. an adapter to the rear of a projectile provided a 102/DiG- 7 tracer composition and an obturating band.
- the casing ⁇ S In. C.
- t t t 1 is closcd at its breech end a ventablg cap and the 0' Search 43, p, adapter at the other end is open so that the propellant 102/931 52 gases can pressurize the breech area and entire gun area behind the obturator band and expel the projec- [56]
- the present invention relates to a novel cartridge suitable for use with large caliber ammunition, wherein the casing is of an open tube design and is expelled from the weapon together with the projectile by means of the gas pressure generated from the propellant act ing against an obturating band located on the projectile.
- Conventional ordnance ammunition consists of a metal casing containing a propellant charge and a projectile forming a single structure or cartridge, which is placed into the breech of a cannon and fired, whereby the projectile is shot from the cannon at a high velocity.
- the cannon is provided with an ejector mechanism for removing the metallic casing after the cartridge has been fired.
- Conventional cartridges of this type are unsuitable for use in military tank cannons since ejection of the metallic casings into the tank would be intolerable due to space limitations within the tank and introduction of toxic gases attending the opening of the breech.
- the metallic cartridge case has been replaced by a non-metallic casing containing highly inflammable nitrocellulose, which is consumed on firing of the propellant charge. It has also been proposed to provide a casing of an organic plastic material, c.g. a glass fiber reinforced polyester resin, having a plurality of structurally weak areas, whereby the pressure of the propellant gases causes the casing to break into small fragments which burn and disintegrate and are blown out of the weapon.
- the use of such consumable or frangible cartridge casings eliminates the need for an ejection mechanism and opening of the breech of the cannon.
- such cartridge cases are relatively fragile and the nitrocellulose is easily degraded by water and oils with the result that the cartridge, after firing, occasionally leaves fragments and smoldering residue, which constitute a serious hazard as it can ignite subsequent rounds.
- a further object of the invention is to provide a cartridge, wherein a high velocity, fin-stabilized projectile mounting an obturator is attached to an open tube casing containing a suitable propellant, and wherein the casing is attached at its forward open end to the rear of the projectile by means of a device adapted to be disconnected therefrom by a pyrotechnic charge situated in the projectile and ignited by the propellant burn.
- the novel cartridge comprises a. a projectile
- a ventable closure for the breech end of said casing i.e. one which burns away or vents to permit the propellant gases to pressurize the breech area;
- the invention is particularly directed to a cartridge of the foregoing design, wherein the projectile is a fin stabilized, high velocity (eg 5000 ft./sec. or more) missile and the open tube casing is relatively long due to its content of a large amount of propellant needed to provide the high pressures ⁇ c.g. 60,000 psi or higher) required for propelling the high velocity projectile.
- high velocity eg 5000 ft./sec. or more
- the open tube casing is relatively long due to its content of a large amount of propellant needed to provide the high pressures ⁇ c.g. 60,000 psi or higher
- the complete removal of such long, noncombustible cartridge casings associated with high velocity, finstabilized projectiles presents an especially difficult problem which is satisfactorily overcome by the present invention.
- the projectile is provided with a pyrotechnic composition, which is adapted to be ignited by the propellant burn and thereby sever the attaching means from the projectile.
- the drawing illustrates a longitudinal sectional view of an expellable cartridge of this invention.
- I52 mm. cartridge comprising an open ended cylindrical casing I0 approximately 63 cm. long, fabricated of high density polyethylene or other suitable material and not combustible under the firing conditions.
- Casing I0 contains a propellant charge ll for generating the desired pressure.
- the breech end of casing 10 is closed by cap 12 having a cup 13 containing an initiator (not shown) for a booster charge of black powder etc. contained in a plastic bag (not shown) for igniting the main propellant charge.
- the base cap I2 is attached to casing I0 with an epoxy resin or other suitable adhesive and is composed of conventional combustible material which is consumed under the firing conditions and thus allows the propellant gases to pressurize the breech area of the gun.
- casing The forward end of casing is attached to a rigid, wheel-like adapter 14 of high density polypropylene having a hub 15 joined by four equally spaced, radial spoke members 16 to a flat rim 17, which is peripherally joined to casing 10, e.g. by adhesive bonding, riv ets, etc.
- Hub 15 is provided with screw threads 18 for attachment to threaded cavity l9 in the rear of tungsten steel projectile 20, and a hole 21 for passage of propellant flash to a tracer charge (not shown) contained in cavity 19.
- Projectile has four equally spaced, full caliber fins 22, which fit into sealed slots in the forward end of casing 10. (Subcaliber fins can also be used, obviating the need for slots in the casing).
- Four full caliber steel sabot blocks 23, as quadrantal sections, are removably mounted on the low caliber cylindrical body of projectile 20 by means of buttress threads or the like, which prevent sliding movement but permit release of said blocks by centrifugal force generated by the spinning projectile.
- Four quadrantal sabot blocks 24 of polypropylene are placed around steel sabot blocks 23 and are held in place by a tight fitting annular obturating band of polypropylene.
- the obturating band 25 is engraved with grooves, which cause the obturator band to break into pieces by spin and thrust forces on exiting from the gun muzzle.
- ignition of propellant 11 by initiator l3 and the black powder booster charge causes generation of gas pressure and combustion of cap l2, thereby venting gases to pressurize the breech area of the gun.
- the gases penetrate between the casing 10 and the gun wall, and also pass through the open forward end of casing 10 and open adapter 14, thereby exerting pres sure against the projectile-sabot-obturator assembly.
- This pressure causes obturating band 25 to slide forward along the inclined surface of sabot blocks 24 and thus expand and wedge against the gun barrel wall, thereby sealing the gases behind the projectile-sabotobturator assembly and propelling the projectile and attached adapter and easing through the gun barrel and engraving the rifling of the bun barrel to provide projectile spin.
- Obturating band 25 is provided with a tongue extension 27, which overlaps casing 10 for a sufficient distance so as to maintain such overlapping and gas seal function even when the front end of obtu rating band 25 reaches the rear edge 26 of steel sabot 23, which stops its forward travel. Further, the hot combustion gases pass through hole 2] in hub 15 of adapter wheel 14 to cavity 19, thereby igniting the tracer charge in cavity 19 for marking the path of the projectile 20. The heat from the burning tracer charge melts and destroys screw threads l8 in such a manner that adapter [4 and casing 10 remain attached to the projectile in the gun barrel but are separated from the projectile on exiting from the weapon.
- the casing N] on exit ruptures explosively into shreds and fragments, which together with the adapter 14 separate from the projectile essentially in the cone of tire region in front of the weapon along with debris from the obturating band 25 and sabot elements 23 and 24, which are separated from the spinning projectile by centrifugal force, as noted above.
- an obturating band is required to seal and confine the propellant gases behind the projectile.
- the obturating band can be made of materials conventionally used for such purpose, preferably a tough flexible organic plas tic material, e.g. polyethylene polypropylene and nylon, although a soft malleable metal e.g. copper, gilding metal etc. can be employed.
- the obturator can be installed in any suitable manner, e.g. as a fixed annu lar ring on a cylindrical projectile slug or shell of sub stantially full caliber size.
- the obtura tor band can be installed in a non-fixed manner directly on the projectile shell, etc. or on sabot elements attached to the projectile, the sabot-obturator-projectile assembly design being such that the propellant gases will move the obturating band forward up an inclined plane, as illustrated in the drawing, sufficiently to expand and prevent the escape of gases past the projectile and also to engage the rifling of the weapon and thus impart sufficient spin to the projectile to remove the obturator and sabot elements by centrifugal force.
- the cartridge casing is desirably made of a flexible organic plastic, including a thermoplastic or thermosetting resin, preferably having an elongation of at least about 400 percent, and especially about 500 l000 percent, such as for example high density polyethylene and polypropylene.
- a thermoplastic or thermosetting resin preferably having an elongation of at least about 400 percent, and especially about 500 l000 percent, such as for example high density polyethylene and polypropylene.
- Highly malleable metals possessing similar elongation, e.g. tin and aluminum are also suitable.
- organic plastics generally provide advantages in cost and ease of fabrication of the casing and are hence preferred. Casings fabricated of relatively rigid or brittle plastic, such as polyacetal resin, tend to fracture under such high gun pressures and explosive shock and leave fragments behind, whereas a flexible casing of polyethylene travels through the gun barrel essentially intact.
- the obturating band and sabots can be made of materials conventionally used for the purpose, e.g. high density polypropylene and polyethylene, similar to that employed in the casing.
- the base cap of the cartridge casing can be of a combustible type, e.g. a conventional molded nitrocellulose-Kraft fiber-resin mixture; or it may be an organic plastic or metal plate containing holes through which the propellant gases can be vented so that the pressure thereof is not applied against the base cap but rather is applied to the breech area to expel the cartridge.
- the holes are covered with a suitable material, e.g. thin plastic sheet, which will fail before the closure cap on firing of the propellant.
- the adapter for attaching the casing to the projectile can be varied so long as it permits passage of the propellant gases out of the casing to press against the obturating band.
- the adapter can be a circular type frame, eg a wheel, peripherally attached to the casing and connected by strong radial spokes or equivalent structure to a hub, which is fastened to the rear of the projectile by screw threads, bolt, or other suitable locking means capable of being melted, burned or otherwise destroyed by the hot propellant gases, or by a tracer or similar composition contained in the projectile ignited by the hot propellant gases.
- the adapter hub is attached, cg.
- the hub has a hole through which the propellant gases can pass to initiate the tracer composition, which melts or otherwise destroys the means of attachment, such that the attachment remains intact while the round is in the gun barrel but is severed after the projectile-casing assembly leaves the muzzle, whereby the projectile is separated from the adapter and spent casing debris in the area near the front of the weapon and no residue, fragments, etc., are left in the weapon.
- the adapter can be made of organic plastic material, e.g. polyolefine such as polyethylene and polypropylene and nylon.
- An expellable cartidgc comprising in combination:
- a fin-stabilized projectile having a low caliber cylindrical shell
- an open ended flexible cylindrical casing contain ing a charge for propelling said projectile
- annular obturating band slidably mounted on said sabot elements and holding the sabot elements together, said obturating band being adapted to be forced forward slidably over the inclined surface of said sabot elements by the propellant gases and thereby to expand and engage the gun rifling and seal the gases behind the projectile; and wherein said obturating band and sabot elements on muzzle exit are removed from the projectile by centrifugal force of projectile spin;
- a cartridge according to claim I wherein the projectile is provided with a pyrotechnic composition adapted to be ignited by the propellant gases and cause separation of said attaching means from said projectile.
- a cartridge according to claim 2, wherein the easing is fabricated of an organic plastic having an elongation greater than about 400 percent and the ventable closure is a cap which is consumed in the firing of the propellant.
- said means for attaching the front end of the casing to the rear of the projectile comprises a circular frame, a hub, and spokes connecting the frame to the hub, and wherein:
- said frame is peripherally attached to said casing
- said projectile has a cavity containing the pyrotechnic composition
- said hub is attached to said cavity by a locking means and has a hole permitting propellant gases to pass from said casing to said cavity to ignite the pyrotechnic composition and eliminate said locking means.
- a cartridge according to claim 4, wherein said attaching means is fabricated of a polyolefine.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Novel cartridge, suitable for use with high velocity anti-tank projectiles, possesses an open tube casing adapted to be expelled from the weapon along with the projectile and separated therefrom on muzzle exit, thereby eliminating dangerous residues in the weapon without significantly affecting projectile ballistics. The cartridge has an open ended casing attached by means of an adapter to the rear of a projectile provided with a tracer composition and an obturating band. The casing is closed at its breech end by a ventable cap and the adapter at the other end is open so that the propellant gases can pressurize the breech area and entire gun area behind the obturator band and expel the projectile. The adapter also permits the propellant gases to ignite the tracer composition so as to burn and sever the attachment to the projectile. The attachment remains intact while the cartridge is in the gun barrel but is severed after it leaves the muzzle, whereby the projectile is separated from the adapter and spent casing debris in the area near the front of the weapon and no residue, fragments, etc. are left behind in the weapon.
Description
United States Patent Blajda Aug. 7, 1973 i 1 EXPELLABLE CA TR CASE Primary Examiner-Robert F. Stahl [75] Inventor: Raymond S. Blajda, Parsippany, NJ. Harry saragov'tz Edward Kelly e a. [73] Assignee: The United States of America as [57] ABSTRACT "Presented P) the Santa" the Novel cartridge, suitable for use with high velocity anti- Army, Washington tank projectiles, possesses an open tube casing adapted to be expelled from the weapon along with the projecl Flledi J 4, 1972 tile and separated therefrom on muzzle exit, thereby [2l] Appl. No.: 215,364 eliminating dangerous residues in the weapon without significantly affecting pro ectile ballistics. The cartridge has an open ended casing attached by means of U.S. an adapter to the rear of a projectile provided a 102/DiG- 7 tracer composition and an obturating band. The casing {S In. C. t t t 1 is closcd at its breech end a ventablg cap and the 0' Search 43, p, adapter at the other end is open so that the propellant 102/931 52 gases can pressurize the breech area and entire gun area behind the obturator band and expel the projec- [56] Rekrences cued tile .tTl: apaptcr also pe zrnits the proiellant ggses to 1gn1 e e racer compos1 101'] so as o urn an sever UNITED STATES PATENTS the attachment to the projectile. The attachment re- 3'609'904 10/197 scfmlon 02/43 P mains intact while the cartrid e is in the un barrel but 2 389 846 ll/l945 F 102/93 8 8 1 7/1966 a g 02/93 is severed after it leaves the muzzle, whereby the projectile is separated from the adapter and spent casing 16581108 4/1972 Larson 102/43 P 3,527.13? M970 Scanlon u '02, P debris 1n the area near the front of the weapon and no 3,620J67 11 1971 Romeret al. 102 93 residue fragments, are left behind the p 6 Claims, 1 Drawing Figure EXPELLABLF. CARTRIDGE CASE The invention described herein may be manufactured, used and licensed by or for the Government for governmental purposes without the payment to me of any royalty thereon.
BACKGROUND OF THE INVENTION The present invention relates to a novel cartridge suitable for use with large caliber ammunition, wherein the casing is of an open tube design and is expelled from the weapon together with the projectile by means of the gas pressure generated from the propellant act ing against an obturating band located on the projectile.
Conventional ordnance ammunition consists of a metal casing containing a propellant charge and a projectile forming a single structure or cartridge, which is placed into the breech of a cannon and fired, whereby the projectile is shot from the cannon at a high velocity. Usually the cannon is provided with an ejector mechanism for removing the metallic casing after the cartridge has been fired. Conventional cartridges of this type are unsuitable for use in military tank cannons since ejection of the metallic casings into the tank would be intolerable due to space limitations within the tank and introduction of toxic gases attending the opening of the breech.
Much effort and expense have been applied to overcome this problem. Thus, the metallic cartridge case has been replaced by a non-metallic casing containing highly inflammable nitrocellulose, which is consumed on firing of the propellant charge. It has also been pro posed to provide a casing of an organic plastic material, c.g. a glass fiber reinforced polyester resin, having a plurality of structurally weak areas, whereby the pressure of the propellant gases causes the casing to break into small fragments which burn and disintegrate and are blown out of the weapon. The use of such consumable or frangible cartridge casings eliminates the need for an ejection mechanism and opening of the breech of the cannon. However, such cartridge cases are relatively fragile and the nitrocellulose is easily degraded by water and oils with the result that the cartridge, after firing, occasionally leaves fragments and smoldering residue, which constitute a serious hazard as it can ignite subsequent rounds.
It is therefore a principal object of this invention to provide a novel cartridge, wherein a projectile carrying an obturator is attached to an open tube casing containing a propellant charge, which will be completely expelled from the gun barrel in conjunction with the projectile when the cartridge is fired, and separated therefrom on muzzle exit.
A further object of the invention is to provide a cartridge, wherein a high velocity, fin-stabilized projectile mounting an obturator is attached to an open tube casing containing a suitable propellant, and wherein the casing is attached at its forward open end to the rear of the projectile by means of a device adapted to be disconnected therefrom by a pyrotechnic charge situated in the projectile and ignited by the propellant burn.
Other objects and advantages of the present invention will appear or be obvious from the following detailed description in conjunction with the accompanying drawing.
SUMMARY OF THE INVENTION The aforesaid difficulties of the prior art are obviated and the objects of the invention are achieved by the novel cartridge which possesses an open tube cartridge casing adapted to be expelled from the gun barrel along with the projectile and to be separated therefrom after expulsion so as not materially to affect the ballistic properties of the projectile. Thus. after firing of the cartridge, no dangerous smoldering or other residues are left in the gun barrel and the need for means for removing a used casing from the fun breech is eliminated.
In general, the novel cartridge comprises a. a projectile;
b. a propellant charge for propelling the projectile;
c. an open ended non-combustible cylindrical car tridge casing containing the propellant charge;
d. a ventable closure for the breech end of said casing, i.e. one which burns away or vents to permit the propellant gases to pressurize the breech area;
e. an obturator attached to the projectile to seal the gases so as to propel the projectile; and
f. means for attaching the forward end of the casing to the rear of the projectile, said means permitting passage of propellant gases from the casing to the obturator and being adapted to separate from the projectile by the action of the propellant gases after leaving the gun barrel, whereby said means and easing follow the projectile in the gun barrel and separate from the projectile when it leaves the weapon without significantly affecting the ballistic properties of the projectile.
The invention is particularly directed to a cartridge of the foregoing design, wherein the projectile is a fin stabilized, high velocity (eg 5000 ft./sec. or more) missile and the open tube casing is relatively long due to its content of a large amount of propellant needed to provide the high pressures {c.g. 60,000 psi or higher) required for propelling the high velocity projectile. The complete removal of such long, noncombustible cartridge casings associated with high velocity, finstabilized projectiles presents an especially difficult problem which is satisfactorily overcome by the present invention.
In a particular embodiment the projectile is provided with a pyrotechnic composition, which is adapted to be ignited by the propellant burn and thereby sever the attaching means from the projectile.
DETAILED DESCRIPTION OF THE INVENTION The drawing illustrates a longitudinal sectional view of an expellable cartridge of this invention.
Referring to the drawing, there is shown I52 mm. cartridge comprising an open ended cylindrical casing I0 approximately 63 cm. long, fabricated of high density polyethylene or other suitable material and not combustible under the firing conditions. Casing I0 contains a propellant charge ll for generating the desired pressure. The breech end of casing 10 is closed by
cap12 having a
cup13 containing an initiator (not shown) for a booster charge of black powder etc. contained in a plastic bag (not shown) for igniting the main propellant charge. The base cap I2 is attached to casing I0 with an epoxy resin or other suitable adhesive and is composed of conventional combustible material which is consumed under the firing conditions and thus allows the propellant gases to pressurize the breech area of the gun. The forward end of casing is attached to a rigid, wheel-
like adapter14 of high density polypropylene having a
hub15 joined by four equally spaced, radial spoke members 16 to a flat rim 17, which is peripherally joined to casing 10, e.g. by adhesive bonding, riv ets, etc.
Hub15 is provided with
screw threads18 for attachment to threaded cavity l9 in the rear of
tungsten steel projectile20, and a
hole21 for passage of propellant flash to a tracer charge (not shown) contained in
cavity19.
Projectile has four equally spaced,
full caliber fins22, which fit into sealed slots in the forward end of casing 10. (Subcaliber fins can also be used, obviating the need for slots in the casing). Four full caliber steel sabot blocks 23, as quadrantal sections, are removably mounted on the low caliber cylindrical body of
projectile20 by means of buttress threads or the like, which prevent sliding movement but permit release of said blocks by centrifugal force generated by the spinning projectile. Four
quadrantal sabot blocks24 of polypropylene are placed around
steel sabot blocks23 and are held in place by a tight fitting annular obturating band of polypropylene. The obturating
band25 is engraved with grooves, which cause the obturator band to break into pieces by spin and thrust forces on exiting from the gun muzzle.
In operation, ignition of propellant 11 by initiator l3 and the black powder booster charge causes generation of gas pressure and combustion of cap l2, thereby venting gases to pressurize the breech area of the gun. The gases penetrate between the casing 10 and the gun wall, and also pass through the open forward end of casing 10 and
open adapter14, thereby exerting pres sure against the projectile-sabot-obturator assembly. This pressure causes obturating
band25 to slide forward along the inclined surface of
sabot blocks24 and thus expand and wedge against the gun barrel wall, thereby sealing the gases behind the projectile-sabotobturator assembly and propelling the projectile and attached adapter and easing through the gun barrel and engraving the rifling of the bun barrel to provide projectile spin. Obturating
band25 is provided with a
tongue extension27, which overlaps casing 10 for a sufficient distance so as to maintain such overlapping and gas seal function even when the front end of
obtu rating band25 reaches the
rear edge26 of
steel sabot23, which stops its forward travel. Further, the hot combustion gases pass through hole 2] in
hub15 of
adapter wheel14 to
cavity19, thereby igniting the tracer charge in
cavity19 for marking the path of the
projectile20. The heat from the burning tracer charge melts and destroys screw threads l8 in such a manner that adapter [4 and casing 10 remain attached to the projectile in the gun barrel but are separated from the projectile on exiting from the weapon. Due to the enormous internal gas pressures, the casing N] on exit ruptures explosively into shreds and fragments, which together with the
adapter14 separate from the projectile essentially in the cone of tire region in front of the weapon along with debris from the obturating
band25 and
sabot elements23 and 24, which are separated from the spinning projectile by centrifugal force, as noted above.
Inspection of the breech after firing of the novel cartridge showed no evidence of residue or fragments so that the weapon could be safely and repeatedly reloaded and fired with automatic reloading mechanism (not shown) using the aforesaid ammunition without the need to open the breech for any reason.
Due to the open tube design of the casing used in the novel expellable cartridge of the present invention, an obturating band is required to seal and confine the propellant gases behind the projectile. The obturating band can be made of materials conventionally used for such purpose, preferably a tough flexible organic plas tic material, e.g. polyethylene polypropylene and nylon, although a soft malleable metal e.g. copper, gilding metal etc. can be employed. Further, the obturator can be installed in any suitable manner, e.g. as a fixed annu lar ring on a cylindrical projectile slug or shell of sub stantially full caliber size. Advantageously, the obtura tor band can be installed in a non-fixed manner directly on the projectile shell, etc. or on sabot elements attached to the projectile, the sabot-obturator-projectile assembly design being such that the propellant gases will move the obturating band forward up an inclined plane, as illustrated in the drawing, sufficiently to expand and prevent the escape of gases past the projectile and also to engage the rifling of the weapon and thus impart sufficient spin to the projectile to remove the obturator and sabot elements by centrifugal force.
With high velocity fin-stabilized projectiles of the type illustrated above, pressures of the order of 60,000 80,000 psi are usually developed in the gun. Such projectiles depend essentially on fins for flight stability, but are usually imparted a low spin (e.g. 30 rps) sufficient to prevent yaw, etc. as well as to remove sabot el ements and obturator band by centrifugal force. In con trast, spin-stabilized projectiles require a much higher order of spin (e.g. 1000 rps and higher) and relatively low pressures (e.g. 30,000 psi) to achieve gyroscopic flight stability.
Particularly for use with such high velocity projectiles the cartridge casing is desirably made of a flexible organic plastic, including a thermoplastic or thermosetting resin, preferably having an elongation of at least about 400 percent, and especially about 500 l000 percent, such as for example high density polyethylene and polypropylene. Highly malleable metals possessing similar elongation, e.g. tin and aluminum, are also suitable. However, organic plastics generally provide advantages in cost and ease of fabrication of the casing and are hence preferred. Casings fabricated of relatively rigid or brittle plastic, such as polyacetal resin, tend to fracture under such high gun pressures and explosive shock and leave fragments behind, whereas a flexible casing of polyethylene travels through the gun barrel essentially intact.
The obturating band and sabots can be made of materials conventionally used for the purpose, e.g. high density polypropylene and polyethylene, similar to that employed in the casing.
The base cap of the cartridge casing can be of a combustible type, e.g. a conventional molded nitrocellulose-Kraft fiber-resin mixture; or it may be an organic plastic or metal plate containing holes through which the propellant gases can be vented so that the pressure thereof is not applied against the base cap but rather is applied to the breech area to expel the cartridge. To contain and protect the propellant charge in the casing prior to firing, the holes are covered with a suitable material, e.g. thin plastic sheet, which will fail before the closure cap on firing of the propellant.
The design of the adapter for attaching the casing to the projectile can be varied so long as it permits passage of the propellant gases out of the casing to press against the obturating band. Thus, the adapter can be a circular type frame, eg a wheel, peripherally attached to the casing and connected by strong radial spokes or equivalent structure to a hub, which is fastened to the rear of the projectile by screw threads, bolt, or other suitable locking means capable of being melted, burned or otherwise destroyed by the hot propellant gases, or by a tracer or similar composition contained in the projectile ignited by the hot propellant gases. In a preferred embodiment the adapter hub is attached, cg. by screw threads to a cavity, which is lo cated in the rear end of the projectile and contains a tracer composition. The hub has a hole through which the propellant gases can pass to initiate the tracer composition, which melts or otherwise destroys the means of attachment, such that the attachment remains intact while the round is in the gun barrel but is severed after the projectile-casing assembly leaves the muzzle, whereby the projectile is separated from the adapter and spent casing debris in the area near the front of the weapon and no residue, fragments, etc., are left in the weapon. The adapter can be made of organic plastic material, e.g. polyolefine such as polyethylene and polypropylene and nylon.
I wish it to be understood that I do not desire to be limited to the exact method and detail of construction described for obvious modification will occur to persons skilled in the art.
What is claimed is:
1. An expellable cartidgc comprising in combination:
a. a fin-stabilized projectile having a low caliber cylindrical shell;
b. sabot elements removably mounted on said projectile shell;
c. an open ended flexible cylindrical casing contain ing a charge for propelling said projectile;
d. a veritable closure for the breech end of said casing permitting the propellant gases to pressurize the breech area;
e. an annular obturating band slidably mounted on said sabot elements and holding the sabot elements together, said obturating band being adapted to be forced forward slidably over the inclined surface of said sabot elements by the propellant gases and thereby to expand and engage the gun rifling and seal the gases behind the projectile; and wherein said obturating band and sabot elements on muzzle exit are removed from the projectile by centrifugal force of projectile spin;
f. means for attaching the front end of said casing to the rear of said projectile, said means permitting passage of propellant gases from the casing to the obturator band and being adapted to separate from the projectile by the action of the propellant gases on muzzle exit, whereby said casing and means follow the projectile in the weapon but are separated from said projectile on muzzle exit without materially affecting the ballistic properties of the projectile.
2. A cartridge according to claim I, wherein the projectile is provided with a pyrotechnic composition adapted to be ignited by the propellant gases and cause separation of said attaching means from said projectile.
3. A cartridge according to claim 2, wherein the easing is fabricated of an organic plastic having an elongation greater than about 400 percent and the ventable closure is a cap which is consumed in the firing of the propellant.
4. A cartridge according to claim 3, wherein said means for attaching the front end of the casing to the rear of the projectile comprises a circular frame, a hub, and spokes connecting the frame to the hub, and wherein:
said frame is peripherally attached to said casing;
said projectile has a cavity containing the pyrotechnic composition; and
said hub is attached to said cavity by a locking means and has a hole permitting propellant gases to pass from said casing to said cavity to ignite the pyrotechnic composition and eliminate said locking means. i
5. A cartridge according to claim 4, wherein said attaching means is fabricated of a polyolefine.
6. A cartridge according to claim 4, wherein said locking means consists of a screw.
Claims (6)
1. An expellable cartridge comprising in combination: a. a fin-stabilized projectile having a low caliber cylindrical shell; b. sabot elements removably mounted on said projectile shell; c. an open ended flexible cylindrical casing containing a charge for propelling said projectile; d. a ventable closure for the breech end of said casing permitting the propellant gases to pressurize the breech area; e. an annular obturating band slidably mounted on said sabot elements and holding the sabot elements together, said obturating band being adapted to be forced forward slidably over the inclined surface of said sabot elements by the propellant gases and thereby to expand and engage the gun rifling and seal the gases behind the projectile; and wherein said obturating band and sabot elements on muzzle exit are removed from the projectile by centrifugal force of projectile spin; f. means for attaching the front end of said casing to the rear of said projectile, said means permitting passage of propellant gases from the casing to the obturator band and being adapted to separate from the projectile by the action of the propellant gases on muzzle exit, whereby said casing and means follow the projectile in the weapon but are separated from said projectile on muzzle exit without materially affecting the ballistic properties of the projectile.
2. A cartridge according to claim 1, wherein the projectile is provided with a pyrotechnic composition adapted to be ignited by the propellant gases and cause separation of said attaching means from said projectile.
3. A cartridge according to claim 2, wherein the casing is fabricated of an organic plastic having an elongation greater than about 400 percent and the ventable closure is a cap which is consumed in the firing of the propellant.
4. A cartridge according to claim 3, wherein said means for attaching the front end of the casing to the rear of the projectile comprises a circular frame, a hub, and spokes connecting the frame to the hub, and wherein: said frame is peripherally attached to said casing; said projectile has a cavity containing the pyrotechnic composition; and said hub is attached to said cavity by a locking means and has a hole permitting propellant gases to pass from said casing to said cavity to ignite the pyrotechnic composition and eliminate said locking means.
5. A cartridge according to claim 4, wherein said attaching means is fabricated of a polyolefine.
6. A cartridge according to claim 4, wherein said locking means consists of a screw.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US21536472A | 1972-01-04 | 1972-01-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3750578A true US3750578A (en) | 1973-08-07 |
Family
ID=22802695
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00215364A Expired - Lifetime US3750578A (en) | 1972-01-04 | 1972-01-04 | Expellable cartridge case |
Country Status (1)
Country | Link |
---|---|
US (1) | US3750578A (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3978792A (en) * | 1975-04-25 | 1976-09-07 | The United States Of America As Represented By The Secretary Of The Army | Projectile-to-cartridge case attachment |
FR2526153A1 (en) * | 1980-06-11 | 1983-11-04 | Saint Louis Inst | Sub-calibre projectile with propelling ring - comprising outer deformable plastics cylinder and inner metal cone |
US4517899A (en) * | 1978-08-08 | 1985-05-21 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Sabot projectile |
US4671181A (en) * | 1972-07-12 | 1987-06-09 | Rheinmetall Gmbh | Anti-tank shell |
EP0281462A1 (en) * | 1987-03-05 | 1988-09-07 | GIAT Industries | Ammunition, in particular for ordnance, comprising a projectile and a case |
US4815682A (en) * | 1987-07-20 | 1989-03-28 | Pacific Armatechnica Corporation | Fin-stabilized subcaliber projectile and method of spin tuning |
US5297492A (en) * | 1993-02-26 | 1994-03-29 | Buc Steven M | Armor piercing fin-stabilized discarding sabot tracer projectile |
DE4323209A1 (en) * | 1993-07-12 | 1995-01-26 | Brenneke Wilhelm Kg | Boost plate for discarding sabot projectiles, in particular for fin-stabilised projectiles having fins which are extended to the rear |
US20050242230A1 (en) * | 2002-06-28 | 2005-11-03 | Marc Vallier | Adapter device for projectile fired from a launching tube |
US20060123684A1 (en) * | 2001-03-13 | 2006-06-15 | Bunney Robert F | Apparatus |
US20090308274A1 (en) * | 2008-06-11 | 2009-12-17 | Lockheed Martin Corporation | Integrated Pusher Plate for a Canister- or Gun-Launched Projectile and System Incorporating Same |
US20120175457A1 (en) * | 2009-09-25 | 2012-07-12 | John William Hunter | Vehicle for launching from a gas gun |
US9567107B2 (en) | 2009-09-25 | 2017-02-14 | Quicklaunch, Inc. | Gas gun launcher |
US10113846B2 (en) | 2016-07-07 | 2018-10-30 | General Dynamics Ordnance and Tactical Systems-Canada, Inc. | Systems and methods for reducing munition sensitivity |
US10427804B1 (en) | 2016-04-29 | 2019-10-01 | Quicklaunch, Inc. | Orbital mechanics of impulsive launch |
US11267588B2 (en) | 2016-04-29 | 2022-03-08 | Quicklaunch, Inc. | Orbital mechanics of impulsive launch |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2389846A (en) * | 1941-08-26 | 1945-11-27 | George R Ericson | High velocity projectile |
US3262391A (en) * | 1964-10-12 | 1966-07-26 | Budd Co | Subcaliber projectile and sabot |
US3527137A (en) * | 1967-11-29 | 1970-09-08 | Remington Arms Co Inc | Expendable case ammunition |
US3609904A (en) * | 1969-05-07 | 1971-10-05 | Remington Arms Co Inc | Extractable plastic cartridge |
US3620167A (en) * | 1968-05-31 | 1971-11-16 | Rheinmetall Gmbh | Drive cage for wing-stabilized lowcaliber shells |
US3658008A (en) * | 1970-04-17 | 1972-04-25 | Dow Corning | Integrated round with combustible cartridge |
-
1972
- 1972-01-04 US US00215364A patent/US3750578A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2389846A (en) * | 1941-08-26 | 1945-11-27 | George R Ericson | High velocity projectile |
US3262391A (en) * | 1964-10-12 | 1966-07-26 | Budd Co | Subcaliber projectile and sabot |
US3527137A (en) * | 1967-11-29 | 1970-09-08 | Remington Arms Co Inc | Expendable case ammunition |
US3620167A (en) * | 1968-05-31 | 1971-11-16 | Rheinmetall Gmbh | Drive cage for wing-stabilized lowcaliber shells |
US3609904A (en) * | 1969-05-07 | 1971-10-05 | Remington Arms Co Inc | Extractable plastic cartridge |
US3658008A (en) * | 1970-04-17 | 1972-04-25 | Dow Corning | Integrated round with combustible cartridge |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4671181A (en) * | 1972-07-12 | 1987-06-09 | Rheinmetall Gmbh | Anti-tank shell |
US3978792A (en) * | 1975-04-25 | 1976-09-07 | The United States Of America As Represented By The Secretary Of The Army | Projectile-to-cartridge case attachment |
US4517899A (en) * | 1978-08-08 | 1985-05-21 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Sabot projectile |
FR2526153A1 (en) * | 1980-06-11 | 1983-11-04 | Saint Louis Inst | Sub-calibre projectile with propelling ring - comprising outer deformable plastics cylinder and inner metal cone |
EP0281462A1 (en) * | 1987-03-05 | 1988-09-07 | GIAT Industries | Ammunition, in particular for ordnance, comprising a projectile and a case |
FR2611889A1 (en) * | 1987-03-05 | 1988-09-09 | France Etat Armement | AMMUNITION IN PARTICULAR FOR ARTILLERY COMPRISING A PROJECTILE AND A SLEEVE |
US4815682A (en) * | 1987-07-20 | 1989-03-28 | Pacific Armatechnica Corporation | Fin-stabilized subcaliber projectile and method of spin tuning |
US5297492A (en) * | 1993-02-26 | 1994-03-29 | Buc Steven M | Armor piercing fin-stabilized discarding sabot tracer projectile |
DE4323209A1 (en) * | 1993-07-12 | 1995-01-26 | Brenneke Wilhelm Kg | Boost plate for discarding sabot projectiles, in particular for fin-stabilised projectiles having fins which are extended to the rear |
US20060123684A1 (en) * | 2001-03-13 | 2006-06-15 | Bunney Robert F | Apparatus |
US7036419B2 (en) * | 2002-06-28 | 2006-05-02 | Mbda | Adapter device for projectile fired from a launching tube |
US20050242230A1 (en) * | 2002-06-28 | 2005-11-03 | Marc Vallier | Adapter device for projectile fired from a launching tube |
US20090308274A1 (en) * | 2008-06-11 | 2009-12-17 | Lockheed Martin Corporation | Integrated Pusher Plate for a Canister- or Gun-Launched Projectile and System Incorporating Same |
US20120175457A1 (en) * | 2009-09-25 | 2012-07-12 | John William Hunter | Vehicle for launching from a gas gun |
US8536502B2 (en) * | 2009-09-25 | 2013-09-17 | Quicklaunch, Inc. | Vehicle for launching from a gas gun |
US8664576B2 (en) * | 2009-09-25 | 2014-03-04 | Quicklaunch, Inc. | Vehicle for launching from a gas gun |
US8979033B2 (en) | 2009-09-25 | 2015-03-17 | Quicklaunch, Inc. | Gas gun launcher |
US9567107B2 (en) | 2009-09-25 | 2017-02-14 | Quicklaunch, Inc. | Gas gun launcher |
US9567108B2 (en) | 2009-09-25 | 2017-02-14 | Quicklaunch, Inc. | Gas gun launcher |
US10427804B1 (en) | 2016-04-29 | 2019-10-01 | Quicklaunch, Inc. | Orbital mechanics of impulsive launch |
US11267588B2 (en) | 2016-04-29 | 2022-03-08 | Quicklaunch, Inc. | Orbital mechanics of impulsive launch |
US10113846B2 (en) | 2016-07-07 | 2018-10-30 | General Dynamics Ordnance and Tactical Systems-Canada, Inc. | Systems and methods for reducing munition sensitivity |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3750578A (en) | 1973-08-07 | Expellable cartridge case |
US7322295B1 (en) | 2008-01-29 | Cartridge munition, particularly one of medium caliber |
US8573127B2 (en) | 2013-11-05 | Pressure-relief system for gun fired cannon cartridges |
US3485170A (en) | 1969-12-23 | Expendable case ammunition |
ES2701415T3 (en) | 2019-02-22 | Pressure relief system for cartridge ammunition |
US7004074B2 (en) | 2006-02-28 | Controlled fluid energy delivery burst cartridge |
US3696749A (en) | 1972-10-10 | Expendable case with vented base cap |
US4823699A (en) | 1989-04-25 | Back-actuated forward ignition ammunition and method |
US1416827A (en) | 1922-05-23 | Ordnance |
US3724376A (en) | 1973-04-03 | Expendable case shotshell |
US1470591A (en) | 1923-10-16 | Gun and ammunition therefor |
US3952657A (en) | 1976-04-27 | Rifle cartridge |
US3547030A (en) | 1970-12-15 | Rocket and cartridge case therefor |
US3759184A (en) | 1973-09-18 | Self-obturating, expellable cartridge case |
US3326084A (en) | 1967-06-20 | Light gas cartridge |
US20020178960A1 (en) | 2002-12-05 | Generation non-lethal and lethal projectiles for arms |
US3741122A (en) | 1973-06-26 | Expendable shotshell |
US3507220A (en) | 1970-04-21 | Ammunition round |
US4858533A (en) | 1989-08-22 | Cased telescoped ammunition round for a fin stabilized projectile |
USH403H (en) | 1988-01-05 | Gun launched kinetic energy penetrator |
US3670651A (en) | 1972-06-20 | Ammunition round |
US5063852A (en) | 1991-11-12 | Forward full caliber control tube for a cased telescoped ammunition round |
US6988450B1 (en) | 2006-01-24 | Anti-personnel ammunition |
US3978793A (en) | 1976-09-07 | Muzzle-expellable cartridge |
US4497239A (en) | 1985-02-05 | Muzzle ejecting sabot cartridge firearm system |