EP0149718A2 - Cartouche combustible à charge propulsive - Google Patents

Cartouche combustible à charge propulsive Download PDF

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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
Application number
EP84110926A
Other languages
German (de)
English (en)
Other versions
EP0149718A3 (en
EP0149718B1 (fr
Inventor
Karlheinz Chem.-Ing. Reinelt
Dietmar Dr. Dipl.-Chem. Müller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of EP0149718A2 publication Critical patent/EP0149718A2/fr
Publication of EP0149718A3 publication Critical patent/EP0149718A3/de
Application granted granted Critical
Publication of EP0149718B1 publication Critical patent/EP0149718B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/18Caseless ammunition; Cartridges having combustible cases
    • F42B5/181Caseless ammunition; Cartridges having combustible cases consisting of a combustible casing wall and a metal base; Connectors therefor
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00Compositions or products which are defined by structure or arrangement of component of product
    • C06B45/12Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/025Cartridges, i.e. cases with charge and missile characterised by the dimension of the case or the missile
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/18Caseless ammunition; Cartridges having combustible cases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/26Cartridge cases
    • F42B5/30Cartridge cases of plastics, i.e. the cartridge-case tube is of plastics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/38Separately-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)
EP84110926A 1983-09-21 1984-09-13 Cartouche combustible à charge propulsive Expired - Lifetime EP0149718B1 (fr)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (1)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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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