EP0149718A2 - Cartouche combustible à charge propulsive - Google Patents
Cartouche combustible à charge propulsive Download PDFInfo
- Publication number
- EP0149718A2 EP0149718A2 EP84110926A EP84110926A EP0149718A2 EP 0149718 A2 EP0149718 A2 EP 0149718A2 EP 84110926 A EP84110926 A EP 84110926A EP 84110926 A EP84110926 A EP 84110926A EP 0149718 A2 EP0149718 A2 EP 0149718A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- propellant charge
- propellant
- film
- nitrate
- plastic film
- 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.)
- Granted
Links
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
- F42B5/18—Caseless ammunition; Cartridges having combustible cases
- F42B5/181—Caseless ammunition; Cartridges having combustible cases consisting of a combustible casing wall and a metal base; Connectors therefor
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
- C06B45/12—Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones
-
- 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
- F42B5/025—Cartridges, i.e. cases with charge and missile characterised by the dimension of the case or the missile
-
- 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
- F42B5/18—Caseless ammunition; Cartridges having combustible cases
-
- 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
- F42B5/26—Cartridge cases
- F42B5/30—Cartridge cases of plastics, i.e. the cartridge-case tube is of plastics
-
- 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
- F42B5/38—Separately-loaded propellant charges, e.g. cartridge bags
Definitions
- the invention relates to a propellant charge case according to the preamble of claim 1.
- the invention is based on the object of specifying a propellant charge sleeve which is particularly simple to produce and which therefore greatly simplifies and reduces the cost of laboring propellant charges, in particular also of the cartridge ammunition.
- Fig. 1 shows a schematic representation in a side view of a large-caliber cartridge ammunition 10 with a projectile 12, a sleeve bottom 13 made of metal and a combustible sleeve 11 and a lid made of an elastic material 14.
- the propellant charge sleeve 11 consists of a combustible plastic film 20, which envelops the propellant charge powder, which is not visible in FIG.
- the plastic film 20 is particularly advantageously designed as a shrink film, which shrinks considerably under the influence of heat, thereby compressing the encased propellant powder strongly and in this way ensures excellent mechanical strength of the propellant charge build-up. Compared to a loosely filled powder, this also enables a significantly higher loading density to be achieved, which brings internal ballistic advantages.
- a method known per se in the field of food packaging is used, in that after the
- Propellant powder with the film 20 is sucked air by connecting a vacuum pump. This also causes the film 20 to lie closely against the enveloped propellant charge powder, which results in a structure which is similarly stable as when using a shrink film.
- the propellant charge sleeve 11 is expediently introduced into a mold, on the inner wall of which it is supported during the filling process.
- a higher charge density can be achieved, combined with an improvement in the mechanical stability of the propellant charge build-up.
- Plastic films which are set to a desired burn-off behavior by oxygen carriers are particularly suitable.
- plastic films made of polyethylene, polyurethane, polyisobutylene, polybutadiene and polysulfides are suitable.
- Combined oxygen carriers such as boron / potassium nitrate, zirconium / barium nitrate and mixtures of the metals magnesium, boron and aluminum with the oxidizers mentioned above are also particularly suitable for the propellant charge sleeve.
- the stability of the propellant charge sleeve can be increased further by covering the plastic film 20 with an outer coating 21 'made of polyurethane, as the cross-sectional image of a propellant charge sleeve 11 shown in FIG. 3 shows.
- this is expediently mixed with a mixture of e.g. B. boron potassium nitrate or other aforementioned oxygen carriers.
- the invention also offers further advantages, since the storage stability of the propellant charges can be increased by selecting gas and moisture-tight film materials.
- cartridge ammunition (FIG. 1) is used with the foil 20 according to the invention configured propellant charge sleeve 11.
- the film 20 is in the form of a hose which is fastened on the one hand to the rear of the projectile 12 and on the other hand to the sleeve base 13.
- These fastenings can preferably be brought about by gluing or welding, possibly also by screwing, spraying or by shrink fit of the film. Possibly. can be attached to the lid 14 simultaneously with the attachment of the film 20 to the sleeve bottom 13.
- the propellant charge can then be introduced into the propellant charge sleeve 11.
- Bulk powder can expediently be filled in through the opening provided in the case base 13 for the propellant charge lighter, while tube powder is to be filled into the case 11 before the case base 13 is fastened.
- the propellant charge sleeve 11 is then shrunk or evacuated. When evacuating, the opening of the propellant lighter can be used to extract the air.
- the propellant charge sleeve 11 which is completed by shrinking or evacuating, has a highly irregular external shape.
- this proves to be an advantage from the inside ballistic point of view, since this facilitates the combustion of the film 20.
- propellant charge 40 of modular construction, in which propellant charge portions 43 are arranged in portions in a shrink tube 42 separated from one another.
- the propellant charge portions 43 are in turn housed in an outer shell 41, which is also made of plastic film.
- propellant charges 43 arranged in a shell 41 can be used simultaneously or only partially.
- the outer shell 41 is designed to be easy to tear open, so that any number of propellant charges 43 that are not required can be removed.
- the connecting pieces 44 are perforated between the foil casings enveloping the propellant charges 43 and are therefore easily separable.
- the hose pieces 42 enveloping the propellant charges 43 can expediently be provided with different colors and / or an imprint, e.g. B. be marked with a number.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Organic Chemistry (AREA)
- Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3334026A DE3334026A1 (de) | 1983-09-21 | 1983-09-21 | Treibladungshuelse |
DE3334026 | 1983-09-21 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0149718A2 true EP0149718A2 (fr) | 1985-07-31 |
EP0149718A3 EP0149718A3 (en) | 1988-09-07 |
EP0149718B1 EP0149718B1 (fr) | 1990-03-21 |
Family
ID=6209620
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP84110926A Expired - Lifetime EP0149718B1 (fr) | 1983-09-21 | 1984-09-13 | Cartouche combustible à charge propulsive |
Country Status (3)
Country | Link |
---|---|
US (1) | US4709636A (fr) |
EP (1) | EP0149718B1 (fr) |
DE (2) | DE3334026A1 (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3927400A1 (de) * | 1989-08-19 | 1991-02-21 | Rheinmetall Gmbh | Verbrennbare treibladungshuelse |
WO2004015358A1 (fr) | 2002-08-08 | 2004-02-19 | Bofors Defence Ab | Cartouche sans douille complete et son procede de production |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4952341A (en) * | 1979-02-09 | 1990-08-28 | The United States Of America As Represented By The Secretary Of The Army | Mechanical enhancement of the burning rate of solid propellants by means of shrink tubes or spheres |
DE3939295A1 (de) * | 1989-11-28 | 1991-05-29 | Rheinmetall Gmbh | Verfahren und vorrichtung zur herstellung von grosskalibriger munition |
US5048421A (en) * | 1990-08-06 | 1991-09-17 | Olin Corporation | Combustible cartridge case base |
US5138949A (en) * | 1990-09-20 | 1992-08-18 | Olin Corporation | Combustible ammunition cartridge case |
US5323707A (en) * | 1991-08-05 | 1994-06-28 | Hercules Incorporated | Consumable low energy layered propellant casing |
US5237927A (en) * | 1991-10-21 | 1993-08-24 | Olin Corporation | Energetic consumable cartridge case |
DE4342428C2 (de) * | 1993-12-13 | 1999-05-27 | Rheinmetall W & M Gmbh | Geschützmunition mit einer verbrennbaren Treibladungshülse |
US6038978A (en) * | 1998-02-11 | 2000-03-21 | Olin Corporation | Shotshell having a protective barrier layer |
DE10347372A1 (de) * | 2003-10-11 | 2005-06-09 | Rheinmetall Waffe Munition Gmbh | Geschützmunition |
US8387537B2 (en) * | 2005-01-28 | 2013-03-05 | Thundercharge Corp. | Consumable cartridge for muzzle loading firearms |
US20080093418A1 (en) * | 2005-06-22 | 2008-04-24 | Weihs Timothy P | Multifunctional Reactive Composite Structures Fabricated From Reactive Composite Materials |
SE0502239L (sv) * | 2005-10-11 | 2006-08-15 | Bae Systems Bofors Ab | Sätt att framställa drivladdningar av kornat drivämne, företrädesvis kornat krut, samt i enlighet med nämnda sätt framställda drivladdningar |
US20120260814A1 (en) | 2008-04-25 | 2012-10-18 | Alliant Techsystems Inc. | Advanced Muzzle Loader Ammunition |
US7726245B2 (en) * | 2008-04-25 | 2010-06-01 | Alliant Techsystems Inc. | Muzzleloader ammunition |
US20120318123A1 (en) | 2011-06-14 | 2012-12-20 | Alliant Techsystems Inc. | Muzzle Loader Powder Increment using Celluloid Combustible Container |
FR3050521B1 (fr) * | 2016-04-26 | 2018-03-30 | Nexter Munitions | Sac de poudre propulsive, charge propulsive d'artillerie incorporant un tel sac et procede de fabrication |
GB2555616B (en) | 2016-11-04 | 2021-10-06 | Bae Systems Plc | Modular charge container |
GB2555618B (en) * | 2016-11-04 | 2021-12-29 | Bae Systems Plc | Munition charge container |
USD849874S1 (en) * | 2018-01-21 | 2019-05-28 | Vista Outdoor Operations Llc | Muzzleloader propellant cartridge |
RU2718578C1 (ru) * | 2019-05-07 | 2020-04-08 | Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации | Артиллерийский патрон |
CN114907177B (zh) * | 2022-04-18 | 2023-07-28 | 南京理工大学 | 一种具有高临界可控压强的电控固体推进剂及其制备方法 |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2424900A1 (de) * | 1973-05-25 | 1974-12-12 | Raufoss Ammunisjonsfabrikker | Brennbare huelsen und verfahren zu deren herstellung |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2083665A (en) * | 1933-10-06 | 1937-06-15 | Washington Inst Of Technology | Ammunition and ordnance device |
BE546573A (fr) * | 1955-04-30 | |||
US3095813A (en) * | 1961-07-05 | 1963-07-02 | Henry S Lipinski | Propellant container, plastic impregnated glass |
US3397637A (en) * | 1967-02-08 | 1968-08-20 | Army Usa | Combustible and consumable cartridge cases |
US3696748A (en) * | 1969-12-29 | 1972-10-10 | Us Army | Means for improving burnout of consumable cartridge cases |
US3718089A (en) * | 1970-03-23 | 1973-02-27 | Us Army | Caseless,linkless,telescoped ammunition |
US3703868A (en) * | 1970-07-07 | 1972-11-28 | Hercules Inc | Protective surface covering having heat and moisture resistant properties for caseless ammunition |
-
1983
- 1983-09-21 DE DE3334026A patent/DE3334026A1/de not_active Withdrawn
-
1984
- 1984-09-13 EP EP84110926A patent/EP0149718B1/fr not_active Expired - Lifetime
- 1984-09-13 DE DE8484110926T patent/DE3481724D1/de not_active Expired - Fee Related
- 1984-09-21 US US06/653,675 patent/US4709636A/en not_active Expired - Fee Related
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2424900A1 (de) * | 1973-05-25 | 1974-12-12 | Raufoss Ammunisjonsfabrikker | Brennbare huelsen und verfahren zu deren herstellung |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3927400A1 (de) * | 1989-08-19 | 1991-02-21 | Rheinmetall Gmbh | Verbrennbare treibladungshuelse |
WO2004015358A1 (fr) | 2002-08-08 | 2004-02-19 | Bofors Defence Ab | Cartouche sans douille complete et son procede de production |
Also Published As
Publication number | Publication date |
---|---|
DE3481724D1 (de) | 1990-04-26 |
EP0149718A3 (en) | 1988-09-07 |
DE3334026A1 (de) | 1985-04-04 |
US4709636A (en) | 1987-12-01 |
EP0149718B1 (fr) | 1990-03-21 |
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