EP3014213B1 - Détonateur pour grenade de mortier et grenade de mortier pouvant être tirée par un mortier à ergot équipée d'un tel détonateur - Google Patents

Détonateur pour grenade de mortier et grenade de mortier pouvant être tirée par un mortier à ergot équipée d'un tel détonateur Download PDF

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Publication number
EP3014213B1
EP3014213B1 EP14730517.1A EP14730517A EP3014213B1 EP 3014213 B1 EP3014213 B1 EP 3014213B1 EP 14730517 A EP14730517 A EP 14730517A EP 3014213 B1 EP3014213 B1 EP 3014213B1
Authority
EP
European Patent Office
Prior art keywords
mortar
shear
detonator
grenade
detonator carrier
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.)
Active
Application number
EP14730517.1A
Other languages
German (de)
English (en)
Other versions
EP3014213A1 (fr
Inventor
Alexander Paesch
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 Waffe Munition GmbH
Original Assignee
Rheinmetall Waffe Munition GmbH
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Application filed by Rheinmetall Waffe Munition GmbH filed Critical Rheinmetall Waffe Munition GmbH
Publication of EP3014213A1 publication Critical patent/EP3014213A1/fr
Application granted granted Critical
Publication of EP3014213B1 publication Critical patent/EP3014213B1/fr
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/18—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved
    • F42C15/188—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved using a rotatable carrier
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/20—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin
    • F42C15/21—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin using spring action
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/28—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
    • F42C15/30—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids of propellant gases, i.e. derived from propulsive charge or rocket motor

Definitions

  • the invention relates to the active partial igniter of a mortar shell. Furthermore, the invention relates to a mortar from a mortar (also known as Spigot mortar or Fly-K mortar), provided with such an active part igniter mortar shell.
  • the starting point of the invention is the provision of a spark ignition powder gas-initiated fuze fuse for a mechanically acting bottom detonator, for example a fly-k mortar shell.
  • Mortar shells that can be fired from a mortar are, for example, from the book of lan V. Hogg: “Ammunition for Light Weapons Mortar and Artillery", 1. Aufl. 1989, Motorbuch Verlag, Stuttgart, page 106f. and 138f , known. They usually consist of a serving as a driving tube hollow tail part, which is bounded by an impact side effective body side. In the interior of the propellant tube, a propellant piston is supported by a propellant charge on the impact plate. The active part igniter is often designed as a bottom igniter.
  • such mortar shells as a safety device often displaceable by the firing acceleration securing bolt. This first engages in a recess of a pivotable Detonatoranis of the projectile fuse and keeps it in its secure position, so that the detonator is held outside the alignment of a detonating chain, through which the effective charge is ignited.
  • the locking pin is axially displaced against the pressure of an elastic return element (spring) and the Detonatorthere released so that this (for example, by a preloaded torsion spring) pivoted to its firing position and the detonator in alignment with a puncture needle is brought.
  • spring elastic return element
  • an active partial igniter for a grenade comprising a detonator carrier which can be pivoted from a secured position to an ignition position, the detonator carrier being in operative connection with a first securing device which, when used as intended, extends in the direction of the longitudinal axis of the corresponding grenade, Includes a spring loaded locking pin.
  • the invention has for its object to disclose an active partial igniter for a mortar shell, in particular for a mortar mortar fireable from a mortar with bottom side (bottom side) arranged Wirkteilzünder containing a security system to prevent inadvertent activation of the active charge, whose operation is essentially independent of the Mortar Grenade launch acceleration is. Furthermore, it is intended to disclose a mortar shell which can be fired from a mortise and mortar, provided with such an active particle igniter.
  • this invention draws back to passing proportionately expanding propellant gases in a breech through the bullet-side impact bottom and controlled to the front of a preferably now transversely and gas-tight slip-mounted in the weft Scherkragenbolzen.
  • the active partial igniter comprises a detonator carrier which can be pivoted from a secured position into an ignition position and which is operatively connected to a first securing device which, when used as intended, extends in the longitudinal direction of the corresponding mortar shell.
  • a first securing device which, when used as intended, extends in the longitudinal direction of the corresponding mortar shell.
  • the shear pin is arranged within a transverse bore and has on its the first end of the locking pin side facing a guide contour, such that in the secured position of the Detonatorehrs the second end of the locking pin is pressed against the pressure of the spring in a recess of the Detonator obviouslys and prevents a pivoting movement of the Detonator obviouslys in its ignition position.
  • the transverse bore has a connection bore through which the propellant charge gases can pass into the transverse bore when the mortar shell is launched and cause an increase in pressure sufficient to separate the part of the shear bolt provided with the guide contour from the remaining part of the shear bolt and along the transverse bore move in the direction of the outer wall of the mortar shell, so that the resting on the guide contour with its first end locking pin is pushed out of the first recess of the Detonatorriads due to the changing guide contour and the Detonator whatsoever is pivotable in its firing position.
  • the invention therefore proposes not to use the external air flow for actuating the safety device of the active part igniter, but the propellant charge gases acting on the bottom of the mortar shell at the firing point.
  • shear pin is designed as a shearing collar pin.
  • the active part igniter comprises in addition to the first safety device dependent on the mortar shell launching second safety device having an axially displaceable safety pin which engages in the rest position of the mortar shell by means of a return element in a second recess of the detonator igniter, and which is pressed upon reaching a predetermined launch acceleration by the inertial forces against the pressure of the return element of the second recess.
  • a mortar shell of the invention which can be fired from a mortise mortiser, with a live igniter designed as a bottom igniter, it is proposed that the shearbolt be arranged within a transverse bore located in the bottom of the mortar shell, which is connected to the propellant tube via the connecting bore arranged axially in the thrust plate.
  • the active partial igniter comprises an igniter housing, which can be inserted into the mortar shell, and in which both the transverse bore with shear pins and the locking pin are located.
  • a mortar shell which can be fired from a mortise mortar, although only the mortar shell is shown in the region of its collision surface designated 2.
  • the mortar shell 1 has at the rear as at the same time serving as a driving tube 3 hollow tail part, wherein the driving tube 3 is bounded at the top (in the weft direction) by the impact bottom 2.
  • Inside the 4 of the driving tube 3 is the front part of the pin 5 of a mortise not shown.
  • firing pin 30 is inserted.
  • the mortar shell 1 comprises an effective partial igniter 8 designed as a bottom igniter with a detonator carrier 9 which can be pivoted from a secured position into an ignition position.
  • This detonator carrier 9 is in operative connection with a first securing device 10 according to the invention of the active part igniter 8.
  • the first securing device 10 comprises a locking pin 12 which extends in the direction of the longitudinal axis 100 of the mortar shell 1 and is loaded by a spring 11 against the weft direction.
  • the locking pin 12 is supported at its first end 13 on a shearing collar bolt 14 (cf. Figure 3 ).
  • the shear collar bolt 14 is disposed within a transverse bore 15 in the buttock 2 of the mortar shell 1 and is positioned in the transverse bore 15 with respect to its axial degree of freedom by the shear collar 31 of the shear collar bolt 14.
  • the shear collar bolt 14 has on its the first end 13 of the locking pin 12 side facing a guide contour 16, such that in the in the Fig.1 and 3 illustrated secured position in which the detonator located on the Detonatorarba 9 (not shown) is held outside the alignment of a firing chain, the second end 17 of the locking pin 12 against the pressure of the spring 11 in a first recess 18 (FIG. Fig.2 ) of the Detonator obviouslys 9 is positively pressed and prevents pivotal movement of the Detonator obviouslys 9 in its ignition position.
  • the transverse bore 15 is connected via a in the joint bottom 2 axially arranged connecting bore 19 with the driving tube 3.
  • a second securing device 20 which acts as a function of the firing acceleration of the mortar shell 1. This consists essentially of a engaging in a second recess 21 of the Detonator relies 9 securing bolt 22 which is acted upon by an elastic return element 23.
  • the mortar shell 1 is located on the pin 5 of the mortar (charged state of the mortar). If the firing pin 30 strikes the propellant charge igniter 24 by actuation of a corresponding firing device (not shown), the propellant charge 6 is ignited and the propellant piston 7 is moved by the propellant charge gases 25 with high force and velocity to the rear end of the mortar shell 1 ( Fig.2 ). In this case, the driving piston 7 acts on the pin 5 of the mortar, so that the mortar shell 1 is thrown into the air.
  • the Detonatorarba 9 means a torsion spring, not shown, is now pivoted to its ignition position and thus the detonator with a tapping needle, not shown, a Zündkette aligned.
  • the active partial igniter according to the invention can not only be used in conjunction with mortar shells that can be fired from mortise mortars, but it can also be used for active partial igniters of mortar shells connected to tubular mortars. However, such a use is also a prerequisite that a part of the propellant charge gas formed during the firing of the mortar shell on a corresponding shear pin of the active part igniter act.
  • the invention is also not limited to the use of a shear pin. Also so-called shear collar bolts can be used alternatively for this purpose.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Golf Clubs (AREA)

Claims (4)

  1. Détonateur de partie active pour une grenade de mortier, possédant les caractéristiques suivantes :
    a) le détonateur de partie active (8) comprend un porte-détonateur (9) qui peut être pivoté d'une position de sûreté dans une position d'allumage ;
    b) le porte-détonateur (9) se trouve en liaison fonctionnelle avec un premier dispositif de sécurité (10) qui, s'il est utilisé conformément à l'usage pour lequel il a été conçu, comporte une goupille de verrouillage (12) chargée par un ressort (11), laquelle s'étend dans la direction de l'axe longitudinal (100) de la grenade de mortier (1) correspondante et s'appuie avec sa première extrémité (13) contre un goujon à cisaillement (14) ;
    c) le goujon à cisaillement (14) est disposé à l'intérieur d'un trou transversal (15) et possède, sur son côté faisant face à la première extrémité (13) de la goupille de verrouillage (12), un profil de guidage (16) de telle sorte que dans la position de sûreté du porte-détonateur (9), la deuxième extrémité (17) de la goupille de verrouillage (12) est poussée en s'opposant à la pression du ressort (11) dans une première cavité (18) du porte-détonateur (9) et empêche un mouvement de pivotement du porte-détonateur (9) dans sa position d'allumage ;
    d) le trou transversal (15) possède un trou de liaison (19) par le biais duquel les gaz de charge propulsive lors du tir de la grenade de mortier (6) correspondante peuvent parvenir dans le trou transversal et y provoquer une augmentation de la pression, laquelle est suffisante pour séparer la partie (26) du goujon à cisaillement (14) pourvue du profil de guidage (16) de la partie restante du goujon à cisaillement (14) et la déplacer le long du trou transversal (15) en direction de la paroi extérieure (27) de la grenade de mortier (1), de sorte que la goupille de verrouillage (12) qui s'appuie avec sa première extrémité (13) sur le profil de guidage (16), du fait de la modification du profil de guidage (16), est repoussée hors de la première cavité (18) du porte-détonateur (9) et le porte-détonateur (9) peut pivoter dans sa position d'allumage.
  2. Détonateur de partie active selon la revendication 1, caractérisé en ce que le goujon à cisaillement (14) est un goujon à collerette à cisaillement.
  3. Détonateur de partie active selon la revendication 1 ou 2, caractérisé en ce que le porte-détonateur (9), en plus du premier dispositif de sécurité (10), se trouve en liaison fonctionnelle avec un deuxième dispositif de sécurité (20) qui comporte un goujon de blocage (22) coulissant dans le sens axial, lequel vient en prise dans une deuxième cavité (21) du porte-détonateur (9) dans la position de repos de la grenade de mortier (1) au moyen d'un élément de rappel (23) et qui, lorsqu'une accélération de tir prédéfinie est atteinte, est repoussé par les forces d'inertie hors de la deuxième cavité (21) en s'opposant à la pression de l'élément de rappel (23).
  4. Grenade de mortier (1) pouvant être tirée depuis un mortier à tourillons, comprenant une partie d'empennage creuse faisant office de tube propulseur (3), le tube propulseur (3) étant délimité du côté avant par un fond d'impact (2) auquel se rattachent, à l'intérieur (4) du tube propulseur (3), une charge propulsive (6) qui s'étend dans le sens axial et, à celle-ci, un piston propulseur (7) qui peut coulisser dans le sens axial vers l'extrémité du côté arrière de la grenade de mortier (1), caractérisée en ce que la grenade de mortier (1) comporte un détonateur de charge active (8) selon l'une des revendications 1 à 3 réalisé sous la forme d'un détonateur de fond, le goujon à cisaillement ou à collerette à cisaillement (14) étant disposé à l'intérieur d'un trou transversal (15) qui se trouve dans le fond d'impact (2) de la grenade de mortier (1), lequel est relié au tube propulseur (3) par le biais du trou de liaison (19) disposé dans le sens axial dans le fond d'impact (2).
EP14730517.1A 2013-06-25 2014-06-13 Détonateur pour grenade de mortier et grenade de mortier pouvant être tirée par un mortier à ergot équipée d'un tel détonateur Active EP3014213B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE201310010502 DE102013010502A1 (de) 2013-06-25 2013-06-25 Wirkteilzünder für eine Mörsergranate und aus einem Zapfenmörser verschießbare Mörsergranate mit einem derartigen Wirkteilzünder
PCT/EP2014/062355 WO2014206771A1 (fr) 2013-06-25 2014-06-13 Détonateur de charge active pour grenade de mortier et grenade de mortier équipée d'un tel détonateur de charge active pouvant être tirée par un mortier de type fly-k

Publications (2)

Publication Number Publication Date
EP3014213A1 EP3014213A1 (fr) 2016-05-04
EP3014213B1 true EP3014213B1 (fr) 2017-08-09

Family

ID=50943314

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Application Number Title Priority Date Filing Date
EP14730517.1A Active EP3014213B1 (fr) 2013-06-25 2014-06-13 Détonateur pour grenade de mortier et grenade de mortier pouvant être tirée par un mortier à ergot équipée d'un tel détonateur

Country Status (4)

Country Link
EP (1) EP3014213B1 (fr)
DE (1) DE102013010502A1 (fr)
ES (1) ES2646514T3 (fr)
WO (1) WO2014206771A1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105241300B (zh) * 2015-10-10 2017-01-11 湖北三江航天红林探控有限公司 切断式锁定装置
FR3046457B1 (fr) 2015-12-30 2018-02-16 Cathyor Engineering SA Equipement d'armement et projectile specialement adapte pour un tel equipement d'armement
CN105758268B (zh) * 2016-03-03 2017-06-13 湖北三江航天红林探控有限公司 一种具有自锁功能的引信安保机构及引信
CN114485295A (zh) * 2022-01-06 2022-05-13 南京理工大学 一种剪切面可回缩的引信剪切销刚性保险机构

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Publication number Priority date Publication date Assignee Title
BE530432A (fr) *
GB9714947D0 (en) 1997-07-16 2003-01-29 Royal Ordnance Plc A fuze
DE19930045C2 (de) * 1999-06-30 2002-07-18 Rheinmetall W & M Gmbh Sicherungselement insbesondere für Zünder, die ohne nur mit sehr geringem Drall verschossen werden

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* Cited by examiner, † Cited by third party
Title
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Also Published As

Publication number Publication date
WO2014206771A1 (fr) 2014-12-31
ES2646514T3 (es) 2017-12-14
EP3014213A1 (fr) 2016-05-04
DE102013010502A1 (de) 2015-01-08

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