EP0318995B1 - Pyrotechnical initiator for projectiles - Google Patents
Pyrotechnical initiator for projectiles Download PDFInfo
- Publication number
- EP0318995B1 EP0318995B1 EP88120077A EP88120077A EP0318995B1 EP 0318995 B1 EP0318995 B1 EP 0318995B1 EP 88120077 A EP88120077 A EP 88120077A EP 88120077 A EP88120077 A EP 88120077A EP 0318995 B1 EP0318995 B1 EP 0318995B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- slider
- delayed
- pyrotechnical
- detonator
- self
- 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
Links
Images
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
- F42C15/184—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 slidable carrier
Definitions
- the invention relates to a pyrotechnic self-dismantling device for projectiles, rockets, bomblets and mines according to the preamble of claim 1.
- a pyrotechnic self-dismantling device for projectiles, missiles, bomblets and mines is known from EP-A-0 256 320. It has an ignition device for a pyrotechnic delay device in a housing.
- the delay device is arranged in a slide which is mounted so that it can move transversely in the housing, this slide being extendable via a lateral opening on the housing via the outer housing contour.
- the delay device consists of an ignition charge, a delay charge and a detonator for igniting an explosive charge.
- the detonator can be triggered by a firing pin that can be actuated when the ammunition strikes.
- a firing needle which is biased by a spring, is mounted in the slide to ignite the deceleration rate. If the delay set is fired outside of the rule, the detonator is inevitably initiated. There is a risk that the explosive charge will be detonated. However, this risk should be excluded.
- the invention is based on the object of proposing a pyrotechnic self-dismantling device in which it is ensured that a delay block ignited outside the rule in safety does not initiate the detonator provided for detonating the explosive charge.
- a firing pin 15 engages securely in a bore 16 of the slide 8.
- a detonator 17 and a sheet 18 with an ignition needle 19 are crimped in the slide 8.
- a delay detonator 25 has: A tube 26 with the sections 27 and 28, an ignition set 29, a delay set 30 and a transmission set 31. 2, the latter lies outside the response range 32 of the detonator 17.
- the tube 26 is slidably mounted in a slide guide 34.
- a ball 35 is mounted in an opening 36 of the slide 8 while the slide 8 is secured.
- the ball 35 is supported on the slide guide 34 and rests on a shoulder 37 of the delay detonator 25.
- the opening 36 is outside the housing 4.
- the slide 8 is provided with a spring 40.
- the slide 8 has a center of gravity 9 at a distance 10 from the main axis 11.
- the bomblet 1 ejected from a swirl projectile also has a corresponding swirl.
- a stabilizing parachute lifts the firing pin 15 out of the bore 16 in a known manner. Then the centrifugal forces generated by the swirl and acting on the slide 8, supported by the spring 40, move the slide 8 into the focus shown in FIG. 3.
- the opening 36 lies outside the jacket 6, the ball 35 is thrown out of the opening 36 and has thus released the delay detonator 25. This strikes against the sheet 18 due to the inertial forces, whereby the firing needle 19 initiates the ignition charge 29.
- the slide 8 initially only transports the delay detonator 25 until the stop 21 hits the stop 20 of the housing 4 in its movement phase. The delay detonator 25 is unlocked.
- the inertial forces act solely on the delay detonator 25 and move it up to the sheet metal 18.
- the transmission set 31 immediately adjacent to the detonator 17 ignites the detonator 17 in accordance with the arrow 44. This then initiates the explosive charge 3 via the transfer charge 2.
- the slide 8 is secured in a known manner.
- the telescopability of the delay detonator allows a relatively large overall length, which is only limited by the run-up section 50 between the firing needle 19 and the primer. In addition, there is also a safety distance, which is defined as the response area 32. Therefore, if the delay detonator 25 is fired in a safe manner outside the rule, it is ensured that the detonator 17 is not initiated due to the spatial separation.
- the hot gases and particles of the transmission set 31 are discharged into relaxation rooms (not shown) of the pyrotechnic igniter 5. Despite the fact that the delay detonator 25 can be telescoped, it is ensured in the focus that the transmission set 31 is in the immediate vicinity of the detonator 17.
- the transmission set 31 penetrates the section 28, the wall 33 and the detonator cup 38.
- a spring 12 effects or supports the setting of the delay detonator 25.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
Description
Die Erfindung bezieht sich auf eine pyrotechnische Selbstzerlegungseinrichtung für Geschosse, Rakteten, Bomblets und Minen nach dem Oberbegriff des Anspruches 1.The invention relates to a pyrotechnic self-dismantling device for projectiles, rockets, bomblets and mines according to the preamble of claim 1.
Aus der EP-A-0 256 320 ist eine pyrotechnische Selbstzerlegungseinrichtung für Geschosse, Raketen, Bomblets und Minen bekannt. Sie weist in einem Gehäuse eine Zündeinrichtung für eine pyrotechnische Verzögerungseinrichtung auf. Die Verzögerungseinrichtung ist in einem, in dem Gehäuse quer beweglich gelagerten Schieber angeordnet, wobei dieser Schieber über eine seitliche Öffnung am Gehäuse über die äußere Gehäusekontur ausfahrbar ist. Die Verzögerungseinrichtung besteht aus einem Anzündsatz, einem Verzögerungssatz und einem Detonator zur Zündung einer Sprengladung. Andererseits ist der Detonator durch einen beim Aufschlag der Munition betätigbaren Schlagbolzen auslösbar. In dem Schieber ist eine über eine Feder vorgespannte Zündnadel zur Zündung des Verzögerungssatzes gelagert. Wird außerhalb der Regel der Verzögerungssatz in Sicherstellung gezündet, so wird zwangsläufig der Detonator initiiert. Hierbei besteht die Gefahr, daß auch die Sprengladung gezündet wird. Diese Gefahr sollte jedoch ausgeschlossen werden.A pyrotechnic self-dismantling device for projectiles, missiles, bomblets and mines is known from EP-A-0 256 320. It has an ignition device for a pyrotechnic delay device in a housing. The delay device is arranged in a slide which is mounted so that it can move transversely in the housing, this slide being extendable via a lateral opening on the housing via the outer housing contour. The delay device consists of an ignition charge, a delay charge and a detonator for igniting an explosive charge. On the other hand, the detonator can be triggered by a firing pin that can be actuated when the ammunition strikes. A firing needle, which is biased by a spring, is mounted in the slide to ignite the deceleration rate. If the delay set is fired outside of the rule, the detonator is inevitably initiated. There is a risk that the explosive charge will be detonated. However, this risk should be excluded.
Demgemäß liegt der Erfindung die Aufgabe zugrunde, eine pyrotechnische Selbstzerlegungseinrichtung vorzuschlagen, bei der gewährleistet ist, daß ein außerhalb der Regel in Sicherstellung gezündeter Verzögerungssatz den für die Zündung der Sprengladung vorgesehenen Detonator nicht initiiert.Accordingly, the invention is based on the object of proposing a pyrotechnic self-dismantling device in which it is ensured that a delay block ignited outside the rule in safety does not initiate the detonator provided for detonating the explosive charge.
Diese Aufgabe wird entsprechend den Merkmalen des Anspruches 1 gelöst. Vorteilhafte Weiterbildungen der Erfindung gehen aus den Unteransprüchen hervor.This object is achieved in accordance with the features of claim 1. Advantageous developments of the invention emerge from the subclaims.
Die Vorteile der Erfindung werden anhand zweier in der Zeichnung dargestellten Ausführungsbeispiele erläutert.The advantages of the invention are explained using two exemplary embodiments shown in the drawing.
Es zeigt:
- Fig. 1
- einen Ausschnitt aus einem pyrotechnischen Zünder für ein Bomblet;
- Fig. 2
- einen Schnitt II-II nach Fig. 1;
- Fig. 3
- den Zünder nach Fig. 2 in Scharfstellung;
- Fig. 1
- a section of a pyrotechnic detonator for a bomblet;
- Fig. 2
- a section II-II of FIG. 1;
- Fig. 3
- the igniter of Figure 2 in focus.
Ein Schlagbolzen 15 greift in Sicherstellung in eine Bohrung 16 des Schiebers 8 ein. Ein Detonator 17 und ein Blech 18 mit einer Zündnadel 19 sind im Schieber 8 eingebördelt.A
Ein Verzögerungsdetonator 25 weist auf:
Ein Röhrchen 26 mit den Abschnitten 27 und 28, einen Anzündsatz 29, einen Verzögerungssatz 30 und einen Übertragungssatz 31.
Der Letztere liegt in Sicherstellung nach Fig. 2 außerhalb des Ansprechsbereiches 32 des Detonators 17.A
A
2, the latter lies outside the
Das Röhrchen 26 ist in einer Schieberführung 34 verschiebbar gelagert. Eine Kugel 35 ist in Sicherstellung des Schiebers 8 in einer Öffnung 36 des Schiebers 8 gelagert. Die Kugel 35 ist an der Schieberführung 34 abgestützt und liegt an einer Schulter 37 des Verzögerungsdetonators 25 an. In Scharfstellung des Schiebers 8 ist die Öffnung 36 außerhalb des Gehäuses 4. Der Schieber 8 ist mit einer Feder 40 versehen.The
Der Schieber 8 weist einen Schwerpunkt 9 in einem Abstand 10 von der Hauptachse 11 auf.The
Das aus einem Drallgeschoß ausgestossene Bomblet 1 weist ebenfalls einen entsprechenden Drall auf. Ein Stabilisierungsfallschirm hebt in bekannter Weise den Schlagbolzen 15 aus der Bohrung 16. Danach bewegen die durch den Drall erzeugten, am Schieber 8 wirksamen Zentrifugalkräfte, unterstützt durch die Feder 40, den Schieber 8 in die aus Fig. 3 ersichtliche Scharfstellung. Sobald die Öffnung 36 außerhalb des Mantels 6 liegt, wird die Kugel 35 aus der Öffnung 36 herausgeschleudert und hat damit den Verzögerungsdetonator 25 freigegeben. Dieser schlägt aufgrund der Massenkräfte gegen das Blech 18, wodurch die Zündnadel 19 den Anzündsatz 29 initiiert. Wesentlich ist, daß der Schieber 8 in seiner Bewegungsphase den Verzögerungsdetonator 25 bis zum Aufschlag des Anschlags 21 an dem Anschlag 20 des Gehäuses 4 zunächst nur transportiert. Dabei wird der Verzögerungsdetonator 25 entsichert. Durch den Aufschlag wirken die Massenkräfte allein an dem Verzögerungsdetonator 25 und bewegen diesen bis an das Blech 18. Nach Ablauf der Brennzeit des Verzögerungssatzes 30 zündet der, dem Detonator 17 unmittelbar benachbarte Übertragungssatz 31 den Detonator 17 entsprechend dem Pfeil 44. Dieser initiiert dann die Sprengladung 3 über die Übertragungsladung 2. In Scharfstellung (Fig. 3) ist der Schieber 8 in bekannter Weise gesichert.The bomblet 1 ejected from a swirl projectile also has a corresponding swirl. A stabilizing parachute lifts the
Der beschriebene Funktionsablauf erfolgt nur unter der Voraussetzung, daß das Bomblet 1 auf weichen Untergrund aufschlägt, so daß für den Schlagbolzen 15 kein entsprechender Impuls vorlag.The functional sequence described takes place only on the condition that the bomblet 1 hits soft ground, so that there was no corresponding pulse for the
Die Teleskopierbarkeit des Verzögerungsdetonators erlaubt eine relativ große Baulänge, die nur durch die Anlaufstrecke 50 zwischen der Zündnadel 19 und dem Anzündsatz begrenzt ist. Außerdem liegt in Sicherstellung ein ebenfalls der Sicherheit dienender Abstand vor, der als Ansprechbereich 32 definiert ist. Wird daher außerhalb der Regel der Verzögerungsdetonator 25 in Sicherstellung gezündet, so ist gewährleistet, daß der Detonator 17 aufgrund der räumlichen Trennung nicht initiiert wird.The telescopability of the delay detonator allows a relatively large overall length, which is only limited by the run-up section 50 between the
Die heißen Gase und Partikel des Übertragungssatzes 31 werden in nicht gezeigte Entspannungsräume des pyrotechnischen Zünders 5 abgeleitet.
Trotz der Teleskopierbarkeit des Verzögerungsdetonators 25 ist in Scharfstellung gewährleistet, daß der Übertragungssatz 31 in unmittelbarer Nachbarschaft des Detonators 17 steht. Der Übertragungssatz 31 durchschlägt den Abschnitt 28, die Wand 33 und den Detonatorbecher 38.The hot gases and particles of the transmission set 31 are discharged into relaxation rooms (not shown) of the
Despite the fact that the
Bei einem Bomblet ohne Drall bewirkt bzw. unterstützt eine Feder 12 die Scharfstellung des Verzögerungsdetonators 25.In the case of a bomblet without swirl, a
Claims (5)
- A pyrotechnical self-destruction mechanism for projectiles, rockets, bomblets (1) and mines, which has in a housing (4) an ignition device for a pyrotechnical delayed-action mechanism (25), consisting of a firing composition (29) and a delayed-action composition (30), a detonator (17) for the detonation of an explosive charge (3) and a firing pin (15) for the detonator (17), in which respect the detonator (17) is arranged in a transversely movable slider (8) and the housing (4) has a lateral aperture (7) for the slider (8; 68) which can be run out beyond the outer housing contour (jacket 6) and which contains the delayed-action mechanism (25; 60), the delayed-action mechanism (25) is displaceably mounted so as to be longitudinally movable in the slider (8), is secured by way of a safety device (34-37) in the slider (8) and is unlocked only in the armed position of the slider (8), in which respect the slider (8) has a stationary firing needle (19) for igniting the displaceable delayed-action mechanism (25).
- A pyrotechnical self-destruction fuze according to claim 1, characterised in that the safety device of the delayed-action mechanism (25) is a ball safety device, in which respect the ball (35) in the safe position of the slider (8) is mounted in an aperture (36) of the slider (8) between a shoulder (37) of the delayed-action mechanism (25) and a slider guide (34) of the housing (4), in which respect the aperture (36) lies close to the jacket (6).
- A pyrotechnical self-destruction fuze according to claim 1, characterised in that a transmission composition (31), a delayed-action composition (30) and a detonation firing composition (29) are arranged in a tube (26), in which respect the transmission composition (31) in the safe position lies outside the response region (33) of the detonator (17).
- A pyrotechnical self-destruction fuze according to claim 1, characterised in that the slider (8; 68) is secured in a form-locking manner by spring force (40) or by centrifugal forces in known "per se" manner in the safe position by a striker pin (15) mounted in the main axis of the fuse and the slider (8; 68) after the unlocking thereof is movable out of the safe position into the armed setting (72).
- A pyrotechnical self-destruction fuze according to claim 1, characterised in that in the armed position of the slider (8) the stops (20, 21) butt against one another.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3740967 | 1987-12-03 | ||
DE19873740967 DE3740967A1 (en) | 1987-12-03 | 1987-12-03 | PYROTECHNICAL IGNITION FOR BULLETS |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0318995A2 EP0318995A2 (en) | 1989-06-07 |
EP0318995A3 EP0318995A3 (en) | 1990-04-18 |
EP0318995B1 true EP0318995B1 (en) | 1994-05-18 |
Family
ID=6341802
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP88120077A Expired - Lifetime EP0318995B1 (en) | 1987-12-03 | 1988-12-01 | Pyrotechnical initiator for projectiles |
Country Status (3)
Country | Link |
---|---|
US (1) | US4901643A (en) |
EP (1) | EP0318995B1 (en) |
DE (2) | DE3740967A1 (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3912671A1 (en) * | 1989-04-18 | 1990-10-25 | Diehl Gmbh & Co | IGNITION OF A BOMBLET |
DE3925235A1 (en) * | 1989-07-29 | 1991-01-31 | Rheinmetall Gmbh | BOMBLETZUENDER |
DE4303128C2 (en) * | 1993-02-04 | 1995-10-12 | Rheinmetall Ind Gmbh | Projectile device for projectiles, missiles, bomblets and mines with a pyrotechnic self-dismantling device |
AT403410B (en) * | 1994-01-31 | 1998-02-25 | Oregon Ets Patentverwertung | IGNITION FOR A GRENADE |
DE9419261U1 (en) * | 1994-12-01 | 1996-04-04 | Junghans Gmbh Geb | Impact detonator for ammunition |
FR2737293B1 (en) * | 1995-07-27 | 1997-10-17 | Giat Ind Sa | SYSTEM FOR GENERATING THE EXPLOSIVE LOAD OF A SUBMUNITION ON BOARD IN A CARRIER |
DE19726951C2 (en) * | 1997-06-25 | 1999-12-16 | Rheinmetall W & M Gmbh | Detonator for a swirl projectile with a self-dismantling unit arranged in the locking bolt for the detonator carrier |
ES2174661B1 (en) * | 1999-02-22 | 2004-08-16 | Instalaza, S.A. | IMPROVEMENTS INTRODUCED IN SELF-DESTRUCTIVE ELECTRONIC SPOOLS. |
DE19919001A1 (en) * | 1999-04-27 | 2000-11-09 | Junghans Gmbh Geb | Pyrotechnic self-dismantling for ammunition |
DE19930045C2 (en) * | 1999-06-30 | 2002-07-18 | Rheinmetall W & M Gmbh | Securing element in particular for detonators which are fired without only a very small swirl |
DE102012006429B4 (en) * | 2012-03-30 | 2013-11-07 | Diehl Bgt Defence Gmbh & Co. Kg | Device for igniting a pyrotechnic active mass |
EP3076122B1 (en) * | 2015-04-01 | 2018-10-24 | Inauen-Schätti AG | System for triggering of avalanches |
CN109654961B (en) * | 2018-12-10 | 2021-10-01 | 中国航天科工集团八五一一研究所 | Safe ignition device capable of effectively preventing chamber from being blocked |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB529505A (en) * | 1938-02-17 | 1940-11-22 | Bofors Ab | Percussion fuzes for aerial bombs |
GB624135A (en) * | 1945-02-02 | 1949-05-27 | Controles Ind Et | Improvements in and relating to detonating devices for rocket projectiles |
US3025795A (en) * | 1958-02-12 | 1962-03-20 | Thiokol Chemical Corp | Time delay fuse element |
CH456403A (en) * | 1966-07-28 | 1968-07-31 | Tamerlan Ets | Percussion fuze for projectile |
CH448812A (en) * | 1967-03-10 | 1967-12-15 | Fibora Ag | Mine detonator with detonator fuse |
US4030418A (en) * | 1975-10-30 | 1977-06-21 | The United States Of America As Represented By The Secretary Of The Army | Gravity deployed mine with combined upper clearing charge firing and delayed main charge initiation |
US4029016A (en) * | 1976-06-29 | 1977-06-14 | The United States Of America As Represented By The Secretary Of The Army | Plural mode fuze |
DE3333312A1 (en) * | 1983-09-15 | 1985-04-04 | Rheinmetall GmbH, 4000 Düsseldorf | IGNITION FOR A SUBFLOOR |
CA1225542A (en) * | 1984-12-03 | 1987-08-18 | Gilles M. Berube | Firing pin and safety and arming mechanism for a penetrating warhead |
DE3539279A1 (en) * | 1985-11-06 | 1987-05-07 | Diehl Gmbh & Co | Detonator for a parachute-stabilised or strip-stabilised submunition |
FR2592475B1 (en) * | 1985-12-27 | 1989-11-03 | Lacroix E Tous Artifices | PYROTECHNICALLY ACTUATED LOAD AND AMMUNITION INCORPORATING THE SAME. |
DE8614108U1 (en) * | 1986-05-24 | 1987-09-24 | Diehl Gmbh & Co, 8500 Nuernberg, De | |
DE3624713C2 (en) * | 1986-07-22 | 1995-09-07 | Diehl Gmbh & Co | Impact detonator with self-dismantling device for a bomblet |
IL82066A (en) * | 1987-03-31 | 1992-03-29 | Israel State | Fuse for sub-munition warhead |
-
1987
- 1987-12-03 DE DE19873740967 patent/DE3740967A1/en not_active Withdrawn
-
1988
- 1988-11-29 US US07/277,275 patent/US4901643A/en not_active Expired - Fee Related
- 1988-12-01 DE DE3889636T patent/DE3889636D1/en not_active Expired - Fee Related
- 1988-12-01 EP EP88120077A patent/EP0318995B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0318995A2 (en) | 1989-06-07 |
EP0318995A3 (en) | 1990-04-18 |
DE3740967A1 (en) | 1989-06-15 |
US4901643A (en) | 1990-02-20 |
DE3889636D1 (en) | 1994-06-23 |
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