EP2339285A3 - Granate und Granatabschussvorrichtung - Google Patents

Granate und Granatabschussvorrichtung Download PDF

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Publication number
EP2339285A3
EP2339285A3 EP10015602.5A EP10015602A EP2339285A3 EP 2339285 A3 EP2339285 A3 EP 2339285A3 EP 10015602 A EP10015602 A EP 10015602A EP 2339285 A3 EP2339285 A3 EP 2339285A3
Authority
EP
European Patent Office
Prior art keywords
grenade
flow cross
tube
section
open
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
EP10015602.5A
Other languages
English (en)
French (fr)
Other versions
EP2339285A2 (de
EP2339285B8 (de
EP2339285B1 (de
Inventor
Helmut Hammer
Axel Pfersmann
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.)
Diehl Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence GmbH and Co KG
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 Diehl BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Publication of EP2339285A2 publication Critical patent/EP2339285A2/de
Publication of EP2339285A3 publication Critical patent/EP2339285A3/de
Application granted granted Critical
Publication of EP2339285B1 publication Critical patent/EP2339285B1/de
Publication of EP2339285B8 publication Critical patent/EP2339285B8/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A1/00—Missile propulsion characterised by the use of explosive or combustible propellant charges
    • F41A1/08—Recoilless guns, i.e. guns having propulsion means producing no recoil
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/04—Stabilising arrangements using fixed fins
    • F42B10/06—Tail fins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control
    • F42B15/04—Arrangements thereon for guidance or control using wire, e.g. for guiding ground-to-ground rockets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
    • F42B30/08—Ordnance projectiles or missiles, e.g. shells
    • F42B30/10—Mortar projectiles
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00—Details of fuzes
    • F42C19/08—Primers; Detonators
    • F42C19/0823—Primers or igniters for the initiation or the propellant charge in a cartridged ammunition
    • F42C19/0826—Primers or igniters for the initiation or the propellant charge in a cartridged ammunition comprising an elongated perforated tube, i.e. flame tube, for the transmission of the initial energy to the propellant charge, e.g. used for artillery shells and kinetic energy penetrators

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)

Abstract

Die vorliegende Erfindung betrifft eine rohrverschießbare Granate (1) zum rückstoßfreien Abschuss aus einem beidseitig offenen Rohr (2) ohne Strömungsquerschnittsverengungen. Die Granate umfasst einen Granatengrundkörper (10), welcher zumindest eine Sprengladung (11) umgibt, und eine Strömungsquerschnittsverringerungseinrichtung (12) zur Verringerung des Strömungsquerschnitts des Rohres (2), welche in Bezug auf den Granatengrundkörper (10) in entgegengesetzter Richtung zur Abschussrichtung (X) angeordnet ist. Dabei ist die Strömungsquerschnittsverringerungseinrichtung (12) über eine Verbindungseinrichtung (13) mit dem Granatengrundkörper (10) von diesem beabstandet und abschussstabil verbunden. Die vorliegende Erfindung betrifft ferner eine Granatabschussvorrichtung mit einer solchen Granate (1), wobei die Granatabschussvorrichtung ein beidseitig offenes Rohr (2) ohne Strömungsquerschnittsverengungen aufweist.
Die Strömungsquerschnittsverringerungseinrichtung (12) umfasst einen hohlzylinderförmigen Ring (12a), der über einen oder mehreren Stege (12b) mit der Verbindungseinrichtung (13) verbunden ist.
EP10015602.5A 2009-12-22 2010-12-14 Granate und Granatabschussvorrichtung Active EP2339285B8 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102009060658A DE102009060658B4 (de) 2009-12-22 2009-12-22 Granate und Granatabschussvorrichtung

Publications (4)

Publication Number Publication Date
EP2339285A2 EP2339285A2 (de) 2011-06-29
EP2339285A3 true EP2339285A3 (de) 2014-05-07
EP2339285B1 EP2339285B1 (de) 2017-03-29
EP2339285B8 EP2339285B8 (de) 2017-05-31

Family

ID=43447739

Family Applications (1)

Application Number Title Priority Date Filing Date
EP10015602.5A Active EP2339285B8 (de) 2009-12-22 2010-12-14 Granate und Granatabschussvorrichtung

Country Status (4)

Country Link
US (1) US9488422B2 (de)
EP (1) EP2339285B8 (de)
DE (1) DE102009060658B4 (de)
IL (1) IL210095A (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8967046B2 (en) * 2012-11-30 2015-03-03 Alliant Techsystems Inc. Gas generators, launch tubes including gas generators and related systems and methods
TR201907451T4 (tr) * 2013-11-27 2019-06-21 Security Devices Int Inc Bir mermi.

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BE465985A (de) *
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FR1362182A (fr) * 1963-06-27 1964-05-29 Tampella Oy Ab Procédé et dispositif de stabilisation de la trajectoire de projectiles et de fusées
US4452124A (en) * 1983-03-10 1984-06-05 Ford Aerospace & Communications Corporation Stabilizing tab for missile launcher
DE68907257T2 (de) * 1988-04-14 1993-12-16 Aerospatiale Lagerungs- und Abschusseinheit für eine Drahtlenkrakete.
DE4414737C1 (de) * 1994-04-27 1996-01-04 Daimler Benz Aerospace Ag Vorrichtung zur Fernsteuerung von Flugkörpern oder Torpedos
EP2226607A2 (de) * 2009-03-03 2010-09-08 Diehl BGT Defence GmbH & Co.KG Verfahren zum Zünden eines Gefechtskopfs einer Granate und Fahrzeug

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE465985A (de) *
US2671401A (en) * 1950-01-16 1954-03-09 Abramson Hugo Shaft projectile
FR1362182A (fr) * 1963-06-27 1964-05-29 Tampella Oy Ab Procédé et dispositif de stabilisation de la trajectoire de projectiles et de fusées
US4452124A (en) * 1983-03-10 1984-06-05 Ford Aerospace & Communications Corporation Stabilizing tab for missile launcher
DE68907257T2 (de) * 1988-04-14 1993-12-16 Aerospatiale Lagerungs- und Abschusseinheit für eine Drahtlenkrakete.
DE4414737C1 (de) * 1994-04-27 1996-01-04 Daimler Benz Aerospace Ag Vorrichtung zur Fernsteuerung von Flugkörpern oder Torpedos
EP2226607A2 (de) * 2009-03-03 2010-09-08 Diehl BGT Defence GmbH & Co.KG Verfahren zum Zünden eines Gefechtskopfs einer Granate und Fahrzeug

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Also Published As

Publication number Publication date
EP2339285A2 (de) 2011-06-29
EP2339285B8 (de) 2017-05-31
DE102009060658A1 (de) 2011-06-30
EP2339285B1 (de) 2017-03-29
DE102009060658B4 (de) 2012-11-15
IL210095A (en) 2013-12-31
US20110162247A1 (en) 2011-07-07
US9488422B2 (en) 2016-11-08
IL210095A0 (en) 2011-03-31

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