EP3014213A1 - 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 - Google Patents

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

Info

Publication number
EP3014213A1
EP3014213A1 EP14730517.1A EP14730517A EP3014213A1 EP 3014213 A1 EP3014213 A1 EP 3014213A1 EP 14730517 A EP14730517 A EP 14730517A EP 3014213 A1 EP3014213 A1 EP 3014213A1
Authority
EP
European Patent Office
Prior art keywords
mortar
mortar shell
detonator
shear
pin
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
EP14730517.1A
Other languages
German (de)
English (en)
Other versions
EP3014213B1 (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
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 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
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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 which can be fired from a mortar are known, for example, from the book by lan V. Hogg: “Ammunition for Light Weapons, Mortars and Artillery", L Aufl., 1989, Motorbuch Verlag, Stuttgart, pages 106f and 138f They usually consist of a serving as a driving tube In the interior of the driving tube, a driving piston is supported by a propellant charge on the thrusting surface, the active part igniter being 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
  • 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 is, according to design minimally invasive standards and with sufficient consideration of those fly-k-specific design features, or the functionally unchanged retention thereof, to implement here a second security device in this design.
  • this invention is based on partially bypassing propellant charge gases passing through the bullet-side thrusting surface and guiding it in a controlled manner to the front side of a shearing collar bolt which is preferably now transversely and gas-tightly installed in the firing direction.
  • 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 fired 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 into 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.
  • FIG. 1 shows the longitudinal section of a mortar shell which can be fired from a mortise mortar in the region of its active part igniter, which includes a shear force bolt, shortly before the firing pin arranged in the journal of the mortar strikes the propellant charge igniter of the mortar shell;
  • FIG. 2 shows a view corresponding to FIG. 1, shortly after ignition of the propellant charge of the mortar shell;
  • FIG 3 shows the enlarged view of the present in a transverse bore shear collar pin of the active part of the invention.
  • FIGS. 1 and 2 designates 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 by 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.
  • a propellant charge 6 which is located in a rear end of the grenade axially displaceable driving piston 7.
  • 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 shearing collar pin 14 has on its the first end 13 of the locking pin 12 side facing a guide contour 16, such that in the illustrated in Figures 1 and 3 secured position in which the detonator 9 located on the detonator (not shown) is held outside the alignment of a detonating chain, the second end 17 of the locking pin 12 against the pressure of the spring 1 1 in a first recess 18 (Fig.2) of the Detonatoraniis 9 is positively pressed and prevents pivotal movement of the Detonatoritatis 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. Subsequently, the mode of action of the two safety devices 10 and 20 of the active part igniter 8 when firing the mortar shell 1 according to the invention will be discussed below:
  • the mortar shell 1 is 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 ( Figure 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 locking pin 12 supported on the guide contour 16 with its first end 13 and biased by the spring 11 is pressed out of the first recess 18 of the detonator carrier 9 due to the changing guide contour 16. That is, after ignition of the propellant charge 6 results in the transverse bore 15, a pressure increase sufficient to separate the provided with the guide contour 16 portion 26 of the shear collar pin 14 of the remaining part of the shear collar pin 14 and along the transverse bore 15 in the direction of the outer wall 27th to move the mortar shell 1, so that on the guide contour (16) with its first end 13 supporting locking pin 12 is pushed out of the first recess 18 of the Detonatoritatis 9 due to the changing guide contour 16 and the Detonatoritati 9 is pivotable in its firing position.
  • 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.

Abstract

L'invention concerne un détonateur de charge active (8) destiné à une grenade de mortier (1), notamment une grenade de mortier qui peut être tirée par un mortier de type Fly-K et qui est équipée d'un détonateur de charge active (8) disposé côté fond (fond de percussion). En vue d'obtenir un premier système de sécurité (10) destiné à empêcher une activation inopinée du détonateur de charge active (8) qui soit à la fois simple et économique, l'invention comporte une goupille de blocage (12) qui peut coulisser dans le sens axial à l'aide d'un guidage forcé et qui, dans une position de sécurité d'un porte-détonateur (9) pivotant du détonateur de charge active (8), vient en prise dans un premier évidement (18) du porte-détonateur (9) et qui, lors du tir de la grenade de mortier (1), est tirée hors du premier évidement par les gaz de charge propulsive (25) agissant sur le fond de percussion (2) de la grenade de mortier (1). Le guidage forcé de la goupille de blocage (12) s'effectue par un boulon à cisaillement ou à collerette à cisaillement (14) doté d'un profilé de guidage (16) qui est monté dans un orifice transversal (15).
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 true EP3014213A1 (fr) 2016-05-04
EP3014213B1 EP3014213B1 (fr) 2017-08-09

Family

ID=50943314

Family Applications (1)

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

Family Cites Families (3)

* Cited by examiner, † Cited by third party
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

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2014206771A1 *

Also Published As

Publication number Publication date
WO2014206771A1 (fr) 2014-12-31
ES2646514T3 (es) 2017-12-14
EP3014213B1 (fr) 2017-08-09
DE102013010502A1 (de) 2015-01-08

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