EP0425877B1 - Safety means for projectile fuze - Google Patents
Safety means for projectile fuze Download PDFInfo
- Publication number
- EP0425877B1 EP0425877B1 EP90119704A EP90119704A EP0425877B1 EP 0425877 B1 EP0425877 B1 EP 0425877B1 EP 90119704 A EP90119704 A EP 90119704A EP 90119704 A EP90119704 A EP 90119704A EP 0425877 B1 EP0425877 B1 EP 0425877B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotor
- ignition
- delayed
- delay
- fuze
- 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 - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C9/00—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
- F42C9/14—Double fuzes; Multiple fuzes
- F42C9/142—Double fuzes; Multiple fuzes combined time and percussion fuzes in which the timing is caused by combustion
-
- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C9/00—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
- F42C9/02—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by mechanical means
- F42C9/04—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by mechanical means by spring motor
- F42C9/041—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by mechanical means by spring motor the clockwork activating a security device, e.g. for unlocking the firing-pin
Description
Die Erfindung betrifft einen Geschoßzünder mit einer Sicherungseinrichtung aus einem ersten Zündmittel in einem Gehäuse, an dem ein Rotor mit einem zweiten Zündmittel drehbar gelagert ist, welcher über das erste Zündmittel zur Bildung einer Zündkette schwenkbar ist, und miteiner in die Zündkette wahlweise hineinbewegbaren Verzögerungsladung.The invention relates to a projectile fuse with a safety device comprising a first ignition means in a housing on which a rotor is rotatably mounted with a second ignition means which can be pivoted via the first ignition means to form an ignition chain, and with a delay charge which can be moved into the ignition chain.
Eine derartige Sicherungseinrichtung ist in der DE 26 40 782 C3 und in der DE 31 07 110 A1 beschrieben. Weist das Zündmittel eine Zünverzögerung auf, dann arbeitet die Zündkette in jedem Fall mit der Zündverzögerung. Es ist jedenfalls nicht möglich, je nach dem Einsatzfall mit oder ohne Zündverzögerung zu arbeiten.Such a safety device is described in DE 26 40 782 C3 and in DE 31 07 110 A1. If the ignition device has an ignition delay, the ignition chain always works with the ignition delay. In any case, depending on the application, it is not possible to work with or without ignition delay.
Zwei voneinander unabhängige Zündketten vorzusehen, von denen die eine mit Zündverzögerung und die andere ohne Zündverzögerung arbeitet, wäre aufwendig und würde zusätzliche Probleme im Hinblick auf die Detonatorsicherheit bringen. Durch die DE-AS 10 65 758 ist ein Geschoßzünder offenbart, bei dem zwischen einer Zündpille und dem Detonator am Rotor ein Freiraum besteht, der von der Zündpille überbrückbar ist. Eine Verzögerungspille ist über einen Schieber in den Freiraum einschiebbar, wenn eine Zündverzögerung gewünscht wird. Der Aufbau dieses Geschoßzünders erscheint technisch aufwenidg und kompliziert. In der Unterseite des Rotors befindet sich eine Nut, in welcher die Zündpille, die Verzögerungspille und die Übertragungspille übereinander liegend durch getrennte Schieber unter Federkraft verschiebbar sind.Providing two ignition chains that are independent of one another, one of which operates with a delayed ignition and the other without a delayed ignition, would be complex and would cause additional problems in terms of detonator safety. DE-AS 10 65 758 discloses a projectile detonator in which there is a free space between a squib and the detonator on the rotor which can be bridged by the squib. A delay pill can be inserted into the free space via a slide if an ignition delay is desired. The structure of this projectile detonator appears technically complex and complicated. In the underside of the rotor there is a groove in which the squib, the retardation pill and the transmission pill can be moved one above the other by means of separate slides under spring force.
Aufgabe der Erfindung ist es, einen Geschoßzünder mit einer Sicherungseinrichtung der eingangs genannten Art vorzuschlagen, bei dem die gleiche Zündkette wahlweise entweder mit einer Zündverzögerung oder ohne Zündverzögerung betrieben werden kann und bei dem die Zündkette raumsparend durch einfache Bauteile aufgebaut ist, die eine sichere Funktion gewährleisten.The object of the invention is to propose a projectile detonator with a safety device of the type mentioned in the introduction, in which the same ignition chain can be operated either with an ignition delay or without ignition delay and in which the ignition chain is constructed in a space-saving manner by simple components which ensure reliable operation .
Erfindungsgemäß ist obige Aufgabe bei einer Sicherungseinrichtung der eingangs genannten Art durch die Merkmale des Patentanspruches 1 gelöst.According to the invention, the above object is achieved in a safety device of the type mentioned at the outset by the features of
Dieser neue Geschoßzünder besitzt Zündmittel, die einfach im Aufbau sind und einzelne, ohne großen technischen Aufwand einsetzbare und austauschbare Eintelteile besitzen. Diese Einzelteile sind leicht herstellbar und montierbar, wodurch insgesamt die Wirtschaftlichkeit in der Lagerhaltung und Produktion erhöht wird. Ist eine Zündung ohne Zündverzögerung vorgesehen, dann ist der Schieber so bewegt, daß in der Scharfstellung des Rotors die Verzögerungsladung außerhalb der Zündkette steht. Ist dagegen eine Zündung mit Zündverzögerung vorgesehen, dann ist der Schieber so bewegt, daß die Verzögerungsladung in der Zündkette steht.This new projectile detonator has ignition means that are simple in construction and have individual, interchangeable parts that can be used and replaced without great technical effort. These individual parts are easy to manufacture and assemble, which increases the overall economy in warehousing and production. If ignition without ignition delay is provided, then the slide is moved so that the delay charge is outside the ignition chain when the rotor is in focus. If, on the other hand, an ignition with ignition delay is provided, the slide is moved so that the delay charge is in the ignition chain.
Vorzugsweise steht in der Sicherstellung des Rotors die Verzögerungsladung weder in dem Freiraum noch über dem Zündmittel.When the rotor is secured, the delay charge is preferably neither in the free space nor above the ignition means.
Aus baulichen Gründen ist der Schieber vorzugsweise am Gehäuse gelagert. Er könnte jedoch auch am Rotor selbst gelagert sein.For structural reasons, the slide is preferably mounted on the housing. However, it could also be mounted on the rotor itself.
Weitere vorteilhafte Ausgestaltungen der Erfindung ergeben sich aus der folgenden Beschreibung eines Ausführungsbeispiels und den Unteransprüchen. In der Zeichnung zeigen:
Figur 1- eine Sicherungseinrichtung in Sicherstellung,
Figur 2- die Sicherungseinrichtung in Scharfstellung ohne Zündverzögerung,
Figur 3- einen Teilschnitt längs der Linie III-III nach
Figur 2, Figur 4- die Sicherungseinrichtung in Scharfstellung mit Zündverzögerung und
Figur 5- einen Teilschnitt längs der Linie V-V nach
Figur 4.
- Figure 1
- a security device in security,
- Figure 2
- the safety device in arming without ignition delay,
- Figure 3
- 3 shows a partial section along the line III-III according to FIG. 2,
- Figure 4
- the safety device in arming with ignition delay and
- Figure 5
- a partial section along the line VV of Figure 4.
In einem Gehäuse (1) ist ein Zündmittel (2), hier ein Zündübertrager, angeordnet. An dem Gehäuse (1) ist an einer Achse (3) ein segmentförmiger Rotor (4) schwenkbar gelagert, der durch eine quer zur Drehachse (3) eingebrachte Ausnehmung (8) U-förmig gestaltet ist. In einem ersten, in Figur 3 obenliegenden Schenkel (4.1) trägt der Rotor (4) in einer zur Drehachse (3) parallelen Bohrung (5.1) ein Anzündstück (5). In dem zweiten und in Figur 3 untenliegenden Schenkel (4.2) ist in einer wiederum parallel zur Rotordrehachse (3) parallelen zweiten Bohrung (6.1) ein Detonator (6) eingesetzt. Die Drehachse (3) des Rotors (4) ist in dem verbleibenden Steg (4.3) der U-Bauform vorgesehen. Zwischen dem Detonator (6) und dem Anzündstück (5) besteht somit ein Freiraum (7), der von der Ausnehmung (8) gebildet ist.An ignition device (2), here an ignition transmitter, is arranged in a housing (1). A segment-shaped rotor (4) is pivotally mounted on the housing (1) on an axis (3) and is U-shaped by a recess (8) made transversely to the axis of rotation (3). The rotor (4) carries an igniter (5) in a bore (5.1) parallel to the axis of rotation (3) in a first leg (4.1) located at the top in FIG. A detonator (6) is inserted in the second leg (4.2) located at the bottom in FIG. 3 in a second bore (6.1), which is again parallel to the rotor axis of rotation (3). The axis of rotation (3) of the rotor (4) is provided in the remaining web (4.3) of the U design. There is a free space (7) between the detonator (6) and the igniter (5), which is formed by the recess (8).
Am Gehäuse (1) ist an einer weiteren Achse (9) ein Träger (10) schwenkbar gelagert. Am einen, in die Ausnehmung (9) ragenden Ende des Trägers (10) ist eine Verzögerungsladung (11) angeordnet, die von einem Verzögerungsstück gebildet ist. Der Träger (10) ist mittels einer Feder (12) belastet. Er ist durch einen Sperrstift (13) in Sicherstellung des Rotors (4) und in Scharfstellung des Rotors (4), wenn ohne Zündverzögerung gearbeitet werden soll, arretiert (vgl. Figur 1, 2).A carrier (10) is pivotably mounted on the housing (1) on a further axis (9). A delay charge (11), which is formed by a delay piece, is arranged at one end of the carrier (10) projecting into the recess (9). The carrier (10) is loaded by means of a spring (12). It is locked by a locking pin (13) in the rotor (4) and in the arming of the rotor (4), if you want to work without ignition delay, locked (see Figure 1, 2).
In Sicherstellung ist der Rotor (4) durch ein Vorsicherungselement (14), das in eine Einbuchtung (15) des Umfangs des Rotors (4) greift, und durch ein Räder-Hemmwerk (16) mit einer abgeplatteten Scheibe (17) blockiert, die in eine zweite Einbuchtung (18) des Umfangs des Rotors (4) greift.In safety, the rotor (4) is blocked by a pre-securing element (14) which engages in an indentation (15) in the circumference of the rotor (4) and by a wheel locking mechanism (16) with a flattened disc (17) engages in a second indentation (18) of the circumference of the rotor (4).
Nach dem Lösen des Vorsicherungselements (14) aus der Einbuchtung (15) und dem Ablauf des Räder-Hemmwerks (16) gibt die abgeplattete Scheibe (17) den Rotor (4) auch an seiner zweiten Einbuchtung (18) frei. Er wird dann unter der Wirkung einer Feder (19) in die Scharfstellung (vgl. Figuren 2 bis 5) gebracht.After the pre-securing element (14) has been released from the indentation (15) and the wheel inhibitor (16) has run off, the flattened disc (17) also releases the rotor (4) at its second indentation (18). It is then brought into focus (see FIGS. 2 to 5) under the action of a spring (19).
Ist ein Zünden ohne Zündverzögerung vorgesehen, dann bleibt der Träger (10) durch den Sperrstift (13) blockiert, so daß die Verzögerungsladung (11) außerhalb des Freiraums (7) steht (vgl. Figur 2, 3). Wird das Anzündstück (5) initiiert, dann zündet es über den Freiraum (7) hinweg den Detonator (6), der seinerseits das Zündmittel (2) zündet.If ignition without delay is provided, the carrier (10) remains blocked by the locking pin (13), so that the delay charge (11) is outside the free space (7) (cf. FIGS. 2, 3). If the igniter (5) is initiated, then it ignites the detonator (6) across the free space (7), which in turn ignites the ignition means (2).
Ist ein Zünden mit Zündverzögerung vorgesehen, dann wird der Sperrstift (13) verschoben, so daß er den Träger (10) freigibt. Dieser verschwenkt dann unter der Kraft der Feder (12) so, daß die Verzögerungsladung (11) in dem Freiraum (7) steht (vgl. Figur 4, 5). Nach dem Initiieren des Anzündstücks (5) wird die Verzögerungsladung (11) angezündet. Dieses zündet nach ihrer Verzögerungszeit den Detonator (6), der dann seinerseits das Zündmittel (2) zündet.If ignition with delay is provided, the locking pin (13) is moved so that it releases the carrier (10). This then pivots under the force of the spring (12) so that the deceleration charge (11) is in the free space (7) (see FIGS. 4, 5). After initiating the igniter (5), the delay charge (11) is ignited. After its delay time, this ignites the detonator (6), which in turn ignites the ignition means (2).
Im Falle der gewünschten Zündverzögerung kann die Verzögerungsladung (11) in die Zündkette vor, während oder nach der Verschwenkung des Rotors (4) von der Sicherstellung in die Scharfstellung eingeschwenkt werden.In the event of the desired ignition delay, the delay charge (11) can be pivoted into the ignition chain before, during or after the pivoting of the rotor (4) from the securing position to the arming position.
Beim beschriebenen Ausführungsbeispiel steht die Verzögerungsladung (11) vor ihrem Verschwenken außerhalb des Freiraums (7) und nicht über dem Zündmittel (2). Bei einem anderen Ausführungsbeispiel kann die Verzögerungsladung (11) vor dem Verschwenken über dem Zündmittel (2) stehen. Der in Scharfstellung stehende Rotor (4) schwenkt dann das Anzündstück (5) und den Detonator (6) über bzw. unter die Verzögerungsladung (11). Ist in diesem Fall eine Zündung ohne Zündverzögerung gewünscht, dann wird der Träger (10) so bewegt, daß die Verzögerungseinrichtung (11) aus der Zündkette geht. Dies kann vor, während oder nach dem Übergang des Rotors (4) von der Sicherstellung in die Scharfstellung erfolgen. Die Verzögerungsladung (11) befindet sich regelmäßig in einer durch die beiden Schenkel (4.1,4.2) des Rotors (4) geschützten Position.In the exemplary embodiment described, the delay charge (11) stands before it is pivoted outside the free space (7) and not above the ignition means (2). In another exemplary embodiment, the delay charge (11) can be positioned above the ignition means (2) before pivoting. The rotor (4) in focus then swings the igniter (5) and the detonator (6) above or below the delay charge (11). If an ignition without ignition delay is desired in this case, then the carrier (10) is moved so that the delay device (11) goes out of the ignition chain. This can be done before, during or after the transition of the rotor (4) from securing to arming. The delay charge (11) is regularly in a position protected by the two legs (4.1, 4.2) of the rotor (4).
Claims (3)
- A projectile fuze having a safety device consisting of a first detonating agent (2) in the fuze housing (1), on which a rotor (14) having a second detonating agent (5) is mounted rotatably, which is swivellable over the first detonating agent (2) in the fuze housing for the formation of a detonation chain, and having a delayed-action charge (11) which is optionally movable into the detonation chain, characterised in that the rotor (4) is shaped in a U-shaped manner by a recess (8) introduced transversely to its axis of rotation (3) and in its first limb (4.1) in a first bore (5.1) parallel to the axis of rotation (3) accommodates a firing piece (5) and in its second limb (4.2) in a second bore (6.1) equiaxially to the first bore (5.1) accommodates a detonator (6), whilst the pivot (3) is provided in the cross-piece (4.3), and in that in the recess (8) there engages a carrier (10) for the delayed-action charge (11), which is protected by the first and second limb (4.1, 4.2) of the rotor (4) and can optionally be swivelled into its armed position in such a way that the firing piece (5), the delayed-action charge (11), the detonator (6) and the first detonating agent (2) lying on the same axis in the fuze housing (1) form a continuous detonation chain.
- A projectile fuze according to claim 1, characterised in that the carrier (10) for the delayed-action charge (11) is acted upon by a spring (12) and is releasable by means of a locking pin (13) for the swivel movement by way of the axis (9) inserted in the fuze housing (1).
- A projectile fuze according to claims 1 and 2, characterised in that the carrier (10) for the delayed-action charge (11) is swivellable in the same direction as the rotor (4) into the end position which corresponds to the armed position.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3935180 | 1989-10-23 | ||
DE3935180A DE3935180A1 (en) | 1989-10-23 | 1989-10-23 | PROTECTIVE DEVICE FOR A FLOOR IGNITION |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0425877A2 EP0425877A2 (en) | 1991-05-08 |
EP0425877A3 EP0425877A3 (en) | 1991-08-28 |
EP0425877B1 true EP0425877B1 (en) | 1993-08-11 |
Family
ID=6391973
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP90119704A Expired - Lifetime EP0425877B1 (en) | 1989-10-23 | 1990-10-15 | Safety means for projectile fuze |
Country Status (4)
Country | Link |
---|---|
US (1) | US5063847A (en) |
EP (1) | EP0425877B1 (en) |
CA (1) | CA2027837A1 (en) |
DE (2) | DE3935180A1 (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2724451B1 (en) * | 1994-09-14 | 1997-01-17 | Matra Marconi Space France | PYROTECHNIC CHAIN SAFETY EQUIPMENT |
AT406910B (en) * | 1995-09-07 | 2000-10-25 | Dynamit Nobel Graz Gmbh | Safety apparatus for ignition apparatuses for pyrotechnic charges |
USH1603H (en) * | 1995-11-07 | 1996-11-05 | The United States Of America As Represented By The Secretary Of The Navy | Flare with safe-and-arm ignition system |
DE10000177A1 (en) * | 2000-01-05 | 2001-07-12 | Junghans Feinwerktechnik Gmbh | Ignition device, in particular for a mortar grenade |
HRPK20000068B1 (en) | 2000-02-08 | 2003-02-28 | Janković Ratko | Arming mean in the warhead fuze with the safety mean having the possibility of the explosive train timing regulation |
US6679174B1 (en) | 2002-09-26 | 2004-01-20 | The United States Of America As Represented By The Secretary Of The Navy | Flare igniter with a slurry groove |
US6634301B1 (en) | 2002-09-26 | 2003-10-21 | The United States Of America As Represented By The Secretary Of The Navy | Enclosed ignition flare igniter |
US6588343B1 (en) | 2002-09-26 | 2003-07-08 | The United States Of America As Represented By The Secretary Of The Navy | Igniter system for a flare |
US8037826B2 (en) * | 2006-06-01 | 2011-10-18 | Dse, Inc. | Mechanical self destruct for runaway escapements |
DE102006046811A1 (en) * | 2006-10-02 | 2008-04-03 | Junghans Microtec Gmbh | Projectile fuze has pyrotechnic force element mechanically blocking safety and arming unit until elapse of set time obtained by subtracting predetermined time from time of flight and unlocking arming unit after elapse of set time |
DE102007054777B3 (en) * | 2007-11-16 | 2009-08-13 | Junghans Microtec Gmbh | Safety device for an igniter |
DE102008053990B4 (en) * | 2008-10-30 | 2010-07-22 | Junghans Microtec Gmbh | Igniter for a projectile |
RU2500977C2 (en) * | 2012-03-15 | 2013-12-10 | Шепеленко Виталий Борисович | Remote action ammunition |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1655591A (en) * | 1928-01-10 | Combination fuse | ||
US1775660A (en) * | 1928-07-12 | 1930-09-16 | Alfred F Teitscheid | Combination fuse for projectiles |
DE1065758B (en) * | 1956-04-11 | |||
CH381573A (en) * | 1963-06-14 | 1964-08-31 | Mefina Sa | Hand grenade |
CH464015A (en) * | 1967-10-05 | 1968-10-15 | Mefina Sa | Rocket for rotating projectile |
DE2640782C3 (en) * | 1976-09-10 | 1979-09-06 | Gebrueder Junghans Gmbh, 7230 Schramberg | Safety device on detonators |
DE3107110C2 (en) * | 1981-02-26 | 1984-03-29 | Gebrüder Junghans GmbH, 7230 Schramberg | Safety device for detonators of twist projectiles |
-
1989
- 1989-10-23 DE DE3935180A patent/DE3935180A1/en active Granted
-
1990
- 1990-10-12 US US07/596,502 patent/US5063847A/en not_active Expired - Fee Related
- 1990-10-15 EP EP90119704A patent/EP0425877B1/en not_active Expired - Lifetime
- 1990-10-15 DE DE9090119704T patent/DE59002298D1/en not_active Expired - Fee Related
- 1990-10-17 CA CA002027837A patent/CA2027837A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
US5063847A (en) | 1991-11-12 |
EP0425877A2 (en) | 1991-05-08 |
DE3935180A1 (en) | 1991-04-25 |
EP0425877A3 (en) | 1991-08-28 |
DE3935180C2 (en) | 1991-09-05 |
DE59002298D1 (en) | 1993-09-16 |
CA2027837A1 (en) | 1991-04-24 |
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