ES8801558A1 - Pieza suplementaria de un proyectil en forma de barra - Google Patents

Pieza suplementaria de un proyectil en forma de barra

Info

Publication number
ES8801558A1
ES8801558A1 ES557528A ES557528A ES8801558A1 ES 8801558 A1 ES8801558 A1 ES 8801558A1 ES 557528 A ES557528 A ES 557528A ES 557528 A ES557528 A ES 557528A ES 8801558 A1 ES8801558 A1 ES 8801558A1
Authority
ES
Spain
Prior art keywords
insert
making
lining
bar
forming
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
Application number
ES557528A
Other languages
English (en)
Other versions
ES557528A0 (es
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 ES8801558A1 publication Critical patent/ES8801558A1/es
Publication of ES557528A0 publication Critical patent/ES557528A0/es
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
    • F42B1/02—Shaped or hollow charges
    • F42B1/032—Shaped or hollow charges characterised by the material of the liner

Abstract

PIEZA SUPLEMENTARIA DE UN PROYECTIL EN FORMA DE BARRA CON CONFORMACION EXPANSIVA. CONSTA DE UN DISCO PLANO (10.1) QUE PRESENTA ALREDEDOR DE SU CENTRO (16) VARIAS ZONAS (12.1, 14) QUE SE EXTIENDEN HACIA EL INTERIOR RADIALMENTE DESDE EL CONTORNO (18); DE UN DISCO PLANO (10.2) QUE SE OBTIENE A PARTIR DE UN DISCO PLANO QUE SE CALIENTA HASTA LA TEMPERATURA DE REBLANDECIMIENTO ANTES DE DARLE LA CONFORMACION DEFINITIVA, DE TAL MANERA QUE LAS ZONAS SOLIDIFICADAS POR PRESION SE LIMITAN EXTERIORMENTE POR EL CONTORNO (18) Y, POR EL INTERIOR, POR LOS LADOS DE UN HEXAGONO DE LADOS IGUALES; Y DE UN DISCO PLANO (10.3) QUE SE OBTIENE A PARTIR DE UN DISCO PLANO CALENTADO HASTA LA TEMPERATURA DE REBLANDECIMIENTO Y MEDIANTE UNA ESTAMPA CON SALIENTES SE LE DA LA CONFORMACION DEFINITIVA.
ES557528A 1985-07-18 1987-05-08 Pieza suplementaria de un proyectil en forma de barra Expired ES8801558A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19853525613 DE3525613A1 (de) 1985-07-18 1985-07-18 Einlage zum belegen einer sprengladung und bilden eines stabfoermigen projektils und verfahren zum herstellen der einlage

Publications (2)

Publication Number Publication Date
ES8801558A1 true ES8801558A1 (es) 1988-02-16
ES557528A0 ES557528A0 (es) 1988-02-16

Family

ID=6276058

Family Applications (2)

Application Number Title Priority Date Filing Date
ES555811A Expired ES8900199A1 (es) 1985-07-18 1986-06-06 Procedimiento de fabricacion de una pieza suplementaria para formar un proyectil en forma de barra con configuracion en forma de casquete esferico hueco para cubrir una carga explosiva.
ES557528A Expired ES8801558A1 (es) 1985-07-18 1987-05-08 Pieza suplementaria de un proyectil en forma de barra

Family Applications Before (1)

Application Number Title Priority Date Filing Date
ES555811A Expired ES8900199A1 (es) 1985-07-18 1986-06-06 Procedimiento de fabricacion de una pieza suplementaria para formar un proyectil en forma de barra con configuracion en forma de casquete esferico hueco para cubrir una carga explosiva.

Country Status (6)

Country Link
US (1) US4714019A (es)
EP (1) EP0215183B1 (es)
JP (1) JPS6219700A (es)
DE (2) DE3525613A1 (es)
ES (2) ES8900199A1 (es)
NO (1) NO161402C (es)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3628622C1 (de) * 1986-08-22 1996-08-08 Fraunhofer Ges Forschung Vorrichtung zur Erzeugung sprenggeformter Projektile
DE3830527A1 (de) * 1988-09-08 1990-03-22 Diehl Gmbh & Co Projektilbildende einlage fuer hohlladungen und verfahren zum herstellen der einlage
US5365852A (en) * 1989-01-09 1994-11-22 Aerojet-General Corporation Method and apparatus for providing an explosively formed penetrator having fins
SE502461C2 (sv) * 1991-07-01 1995-10-23 Bofors Ab Sätt vid projektilbildande explosiva laddningar
FR2681677B1 (fr) * 1991-09-20 1995-01-27 Thomson Brandt Armements Charge explosive avec revetement a proprietes mecaniques reparties.
DE4213318C2 (de) * 1992-04-23 2000-04-13 Rheinmetall W & M Gmbh Verfahren zur Herstellen einer Ladungseinlage
EP0707560A4 (en) * 1993-05-04 1998-01-07 Alliant Techsystems Inc IMPROVED PROPULSIVE SYSTEM
US5892172A (en) * 1997-04-22 1999-04-06 Alliant Techsystems Inc. Propellant system
US6505559B1 (en) * 2000-09-14 2003-01-14 Owen Oil Tools, Inc. Well bore cutting and perforating devices and methods of manufacture
DE102005044320B4 (de) 2005-09-16 2010-11-11 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Ladung mit einer im wesentlichen zylindrischen Sprengstoffanordnung
WO2014196277A1 (ja) 2013-06-04 2014-12-11 日産自動車株式会社 セパレータの歪みを除去する成形方法およびセパレータの歪みを除去する成形装置

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3765177A (en) * 1959-12-30 1973-10-16 Thiokol Chemical Corp Rocket motor with blast tube and case bonded propellant
US3722421A (en) * 1962-04-04 1973-03-27 Us Army Solid bipropellant
US3429264A (en) * 1965-12-01 1969-02-25 Nitrochemie Gmbh Solid rocket propellants
FR1603394A (es) * 1968-10-15 1971-04-13
US3745199A (en) * 1968-12-23 1973-07-10 Us Army Method of making an improved case-bonded end-burning propellant grain with restricted stress-relief ports
FR2234465A1 (en) * 1973-06-19 1975-01-17 Poudres & Explosifs Ste Nale Cylindrical rocket propellant charge blocks - with central branched and eccentric axially directed channels
FR2429990B1 (fr) * 1978-06-27 1985-11-15 Saint Louis Inst Charge explosive plate
FR2487966B1 (fr) * 1980-08-01 1986-07-11 Serat Perfectionnements aux revetements pour charges explosives formees
JPS5747789A (en) * 1980-09-01 1982-03-18 Nippon Oils & Fats Co Ltd Sheet-like gunpowder, manufacture and use
FR2512539B1 (fr) * 1981-09-04 1986-01-24 Saint Louis Inst Charge creuse
DE3317352C2 (de) * 1983-05-13 1985-03-07 Diehl GmbH & Co, 8500 Nürnberg Einlage für eine projektilbildende Ladung
US4594945A (en) * 1984-11-28 1986-06-17 General Dynamics, Pomona Division Thermal protection for propellant grains

Also Published As

Publication number Publication date
EP0215183A1 (de) 1987-03-25
US4714019A (en) 1987-12-22
EP0215183B1 (de) 1989-02-15
ES8900199A1 (es) 1989-04-01
NO861438L (no) 1987-01-19
ES555811A0 (es) 1989-04-01
DE3525613A1 (de) 1987-01-22
DE3662119D1 (en) 1989-03-23
JPH042878B2 (es) 1992-01-21
NO161402C (no) 1989-08-09
JPS6219700A (ja) 1987-01-28
ES557528A0 (es) 1988-02-16
NO161402B (no) 1989-05-02

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