EP0129679A1 - Proximity fuze arrangement for missiles - Google Patents
Proximity fuze arrangement for missiles Download PDFInfo
- Publication number
- EP0129679A1 EP0129679A1 EP84105153A EP84105153A EP0129679A1 EP 0129679 A1 EP0129679 A1 EP 0129679A1 EP 84105153 A EP84105153 A EP 84105153A EP 84105153 A EP84105153 A EP 84105153A EP 0129679 A1 EP0129679 A1 EP 0129679A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- fuse
- distance
- ignition device
- housing
- projectile
- 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
Links
- 239000002775 capsule Substances 0.000 claims abstract description 7
- 238000010304 firing Methods 0.000 claims abstract description 4
- 239000003792 electrolyte Substances 0.000 claims description 11
- 238000011156 evaluation Methods 0.000 claims 1
- 238000007789 sealing Methods 0.000 description 2
- 230000004913 activation Effects 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Images
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
- F42C15/28—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
- F42C15/31—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids generated by the combustion of a pyrotechnic or explosive charge within the fuze
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C1/00—Impact fuzes, i.e. fuzes actuated only by ammunition impact
- F42C1/14—Impact fuzes, i.e. fuzes actuated only by ammunition impact operating at a predetermined distance from ground or target by means of a protruding member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C13/00—Proximity fuzes; Fuzes for remote detonation
-
- 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
Definitions
- the invention relates to a distance ignition device for a projectile, which contains a head fuse with essential igniter parts.
- Projectile detonators with an electronic or optronic distance function, as well as other essential functions, in particular safety functions, are known in practice. They are built as integrated igniter units and are e.g. offered as a mine launcher, artillery missile or rocket missile fuse at a high purchase price, due to the expensive electronic part. Much cheaper detonators, e.g. mechanical igniters, but do not have a distance function. An economical alternative product for use with or without a spacing function is therefore missing, in particular for the field of application with blasting distances between 2 to 12 m.
- the invention solves the problem of providing head igniters, which have essential igniter functions, with a spacing function in a simple and inexpensive manner.
- a head igniter having impact and delay functions is inserted into a distance igniter by plugging in an adapter, e.g. can be converted in the field, which means that it can be used economically, in that the expensive electronics are only used when required, or saved when used without a distance function.
- the adapter can be kept short and light, so that the ballistics of the projectile are practically unchanged.
- an adapter 20 which is provided as a distance ignition device, is placed on and attached to the head igniter 11.
- An adapter housing 21 contains, from top to bottom, a distance sensor 22 with associated electronic circuit board 23, an electrolyte battery with contact pin 24, electrode stack 25 and electrolyte housing 26 as an electrical current source for supplying the distance ignition device with the required electrical energy, an electrical primer, or here an electrical one Gas pressure capsule 27, and means for attaching the adapter housing 21 to the igniter 11.
- the functions of handling, transport and a certain safety against falling for the adapter 20 as an individual part are ensured by the electrode housing 26 being held stationary only by being placed on the head igniter. But even in this position, a predetermined breaking point 36 must first penetrate through the action of force to activate the battery, which also ensures load security.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
- Connection Of Batteries Or Terminals (AREA)
- Selective Calling Equipment (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
- Primary Cells (AREA)
Abstract
Description
Die Erfindung bezieht sich auf eine Abstandszündeinrichtung für ein Geschoss, das einen Kopfzünder mit wesentlichen Zünderteilen enthält.The invention relates to a distance ignition device for a projectile, which contains a head fuse with essential igniter parts.
Aus der Praxis sind Geschosszünder mit elektronischer oder optronischer Abstandsfunktion, sowie anderen wesentlichen Funktionen, insbesondere Sicherheitsfunktionen, bekannt. Sie sind als integrierte Zündereinheiten aufgebaut und werden z.B. als Minenwerfer-, Artillerlegeschoss- oder Raketengeschosszünder zu einem hohen Kaufpreis angeboten, bedingt durch den teuren elektronischen Teil. Wesentlich preisgünstigere Zünder, z.B. mechanische Kopfzünder, weisen jedoch keine Abstandsfunktion auf. Insbesondere für das Anwendungsgebiet mit Sprengabständen zwischen 2 bis 12m fehlt daher ein wirtschaftliches Alternativprodukt für den Einsatz mit oder ohne Abstandsfunktion.Projectile detonators with an electronic or optronic distance function, as well as other essential functions, in particular safety functions, are known in practice. They are built as integrated igniter units and are e.g. offered as a mine launcher, artillery missile or rocket missile fuse at a high purchase price, due to the expensive electronic part. Much cheaper detonators, e.g. mechanical igniters, but do not have a distance function. An economical alternative product for use with or without a spacing function is therefore missing, in particular for the field of application with blasting distances between 2 to 12 m.
Die Erfindung, wie sie in den Ansprüchen gekennzeichnet ist, löst die Aufgabe, auf einfache und preisgünstige Weise Kopfzünder, welche wesentliche Zünderfunktionen aufweisen, mit Abstandsfunktion zu versehen.The invention, as characterized in the claims, solves the problem of providing head igniters, which have essential igniter functions, with a spacing function in a simple and inexpensive manner.
Die durch die Erfindung erreichten Vorteile sind im wesentlichen darin zu sehen, dass ein Aufschlags- und Verzögerungsfunktionen aufweisender Kopfzünder in einen Abstandszünder durch Aufstecken eines Adapters z.B. im Felde umgewandelt werden kann, wodurch ein wirtschaftlicher Einsatz gegeben ist, indem die teure Elektronik nur bei Bedarf verwertet, bzw. beim Einsatz ohne Abstandsfunktion eingespart wird. Ferner kann der Adapter kurz und leicht gehalten werden, sodass die Ballistik des Geschosses praktisch nicht verändert wird.The advantages achieved by the invention are essentially to be seen in the fact that a head igniter having impact and delay functions is inserted into a distance igniter by plugging in an adapter, e.g. can be converted in the field, which means that it can be used economically, in that the expensive electronics are only used when required, or saved when used without a distance function. Furthermore, the adapter can be kept short and light, so that the ballistics of the projectile are practically unchanged.
Im folgenden wird die Erfindung anhand einer Zeichnung, welche ein Ausführungsbeispiel darstellt, erläutert:
- In einem
Geschosskörper 10 ist einKopfzünder 11 mit Momentan- (Aufschlag) und Verzögerungsfunktionen, umstellbar durch dieSchaltvorrichtung 12, eingeschraubt.In der Spitze desKopfzünders 11 Ist einBetätigungsknopf 13 angeordnet, der zum Verschieben einesZündstiftes 14 dient. Solche Kopfzünder sind bekannt und werden hier deshalb nicht näher erläutert.
- A
detonator 11 with momentary (impact) and delay functions, which can be changed by theswitching device 12, is screwed into aprojectile body 10. Anactuation button 13 is arranged in the tip of thedetonator 11 and is used to move anignition pin 14. Such igniters are known and are therefore not explained in detail here.
Erfindungsgemäss auf den Kopfzünder 11 aufgesetzt und daran befestigt ist ein Adapter 20, der als Abstandszündeinrichtung vorgesehen ist. Ein Adaptergehäuse 21 enthält von oben nach unten einen Abstandssensor 22 mit zugehöriger elektronischer Schaltungsplatte 23, eine Elektrolytbatterie mit Kontaktstift 24, Elektrodenstapel 25 und Elektrolytgehäuse 26 als elektrische Stromquelle zur Versorgung der Abstandszündeinrichtung mit der benötigten elektrischen Energie, eine elektrische Zündkapsel, bzw. hier eine elektrische Gasdruckkapsel 27, und Mittel zur Befestigung des Adaptergehäuses 21 auf dem Kopfzünder 11. Diese Mittel bestehen hier in der Verwendung von drei gleichmässig am Umfang des Kopfzünders 11 angeordneten Stiften 28, welche mit entsprechendenAusnehmungeπ 29 im Adaptergehäuse 21 einen Bajonettverschluss bilden, derart, dass eine ringförmige Tragfläche 30 des Adaptergehäuses 21 satt an der Ogive des Kopfzünders 11 anliegt. Ein Teil 31, der das Elektrolytgehäuse 26 und die Gasdruckkapsel 27 enthält, ist im Adaptergehäuse 21, durch eine nutförmige Ausnehmung 32, in welche ein im Adaptergehäuse 21 befestigter Stift 33 hineinragt, axial verschiebbar angeordnet. Eine weitere ringförmige Tragfläche 35 am Teil 31 unterstützt den festen Sitz zwischen Adapter 20 und Kopfzünder 11.According to the invention, an
Die Wirkungsweise der beschriebenen Abstandszündeinrichtung ist folgende:
- Ist ein Bedarf für einen Abstandszünder z.B. im Feld gegeben, so wird ein
Adapter 20 auf einen in einemGeschoss 10befestigten Kopfzünder 11 mittels Bajonettverschluss aufgesetzt. Durch den Abschussschock, beim Abschuss des Geschosses, durchbricht derElektrodenstapel 25 eine am Deckel desElektrolytgehäuses 26angebrachte Sollbruchstelle 36 und bildet nun, zusammen mit demortsfesten Elektrolytgehäuse 26, eine aktivierbare Elektrolytbatterie. EinDichtring 34 sorgt dafür, dass die Elektrolytflüssigkeit nicht in den nun leeren Raum abfliessen kann. Nach einer bestimmten Aktivierzeit steht an den Batteriepolen eine Spannung für die Abstands- und Zündelektronik bereit. Die elektrische Verbindung kann beispielsweise über den Kontaktstift und einen daran isoliert angebrachten Kontaktring mit entsprechenden Kontaktstellen der Schaltungsplatte erfolgen. Ein Abstandssensor bekannter Art, z.B. gemäss DE 2608066 C2, DE 2456162 C2 oder DE 2949521 C2 misst nun laufend die Entfernung zu einem Ziel und zündet innerhalb eines vorgegebenen Abstandes vom Ziel das Zündmittel, in diesem Fall dieelektrische Gasdruckkapsel 27 überelektrische Kontaktbahnen 41 und 42 sowieKontakstellen 43 und 44. DieGasdruckkapsel 27 ihrerseits drückt simultan denBetätigungsknopf 13 des Kopfzünders und löst dadurch über denZündstift 14 die Geschosszündung aus.
- If there is a need for a detonator, for example in the field, an
adapter 20 is placed on adetonator 11 fastened in astorey 10 by means of a bayonet catch. Due to the firing shock, when the projectile is fired, theelectrode stack 25 breaks through apredetermined breaking point 36 attached to the cover of theelectrolyte housing 26 and now forms, together with the stationary electrolyte housing 26, an activatable electrolyte battery. Asealing ring 34 ensures that the electrolyte liquid cannot flow into the now empty space. After a certain activation time, a voltage is available at the battery poles for the distance and ignition electronics. The electrical connection can be made, for example, via the contact pin and an insulated attached contact ring with corresponding contact points on the circuit board. A distance sensor of a known type, for example in accordance with DE 2608066 C2, DE 2456162 C2 or DE 2949521 C2, now continuously measures the distance to a target and ignites the ignition means within a predetermined distance from the target, in this case the electricalgas pressure capsule 27 via 41 and 42 andelectrical contact tracks 43 and 44. Thecontact points gas pressure capsule 27 in turn presses the actuatingbutton 13 of the head igniter and thereby triggers the projectile ignition via theignition pin 14.
Durch die Verschiebbarkeit des Teiles 31 im Adaptergehäuse 21 werden die Funktionen Handhabungs-, Transport- und eine bestimmte Fallsicherheit für den Adapter 20 als Einzelteil gewährleistet, indem erst durch das Aufsetzen auf den Kopfzünder das Elektrodengehäuse 26 ortsfest gehalten wird. Aber auch in dieser Stellung muss durch Krafteinwirkung zuerst eine Sollbruchstelle 36 durchschlagen werden, um die Batterie zu aktivieren, womit auch Ladungssicherheit gegeben ist.Due to the displaceability of the
- 10 Geschosskörper10 bullet bodies
- 11 Kopfzünder11 igniter
- 12 Schaltvorrichtung12 switching device
- 13 Betätigungsknopf13 operating button
- 14 Zündstift14 firing pin
- 20 Adapter20 adapters
- 21 Adaptergehäuse21 adapter housing
- 22 Abstandssensor22 distance sensor
- 23 Schaltungsplatte23 circuit board
- 24 Kontaktstift24 contact pin
- 25 Elektrodenstapel25 electrode stacks
- 26 Elektrolytgehäuse26 electrolyte housing
- 27 Gasdruckkapsel27 gas pressure capsule
- 28 Stifte28 pens
- 29 Ausnehmungen29 recesses
- 30 Tragfläche30 wing
- 31 Teil31 part
- 32 Ausnehmung32 recess
- 33 Stift33 pin
- 34 Dichtungsring34 sealing ring
- 35 Tragfläche35 wing
- 36 Sollbruchstelle36 predetermined breaking point
- 41 Kontaktbahnen41 contact tracks
- 42 Kontaktbahnen42 contact tracks
- 43 Kontakstellen43 contacts
- 44 Kontaktstellen.44 contact points.
Claims (4)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH3448/83 | 1983-06-24 | ||
CH344883 | 1983-06-24 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0129679A1 true EP0129679A1 (en) | 1985-01-02 |
EP0129679B1 EP0129679B1 (en) | 1987-04-22 |
Family
ID=4256165
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP84105153A Expired EP0129679B1 (en) | 1983-06-24 | 1984-05-07 | Proximity fuze arrangement for missiles |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0129679B1 (en) |
CA (1) | CA1262321A (en) |
DE (2) | DE3463295D1 (en) |
NO (1) | NO158196C (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4831932A (en) * | 1987-08-17 | 1989-05-23 | Honeywell Inc. | Detonator |
DE102021123375A1 (en) | 2021-09-09 | 2023-03-09 | Rwm Schweiz Ag | Ignition device for ammunition, in particular medium-caliber ammunition, and associated method for detonating or self-destructing ammunition, in particular medium-caliber ammunition |
WO2023180278A1 (en) | 2022-03-23 | 2023-09-28 | Rheinmetall Air Defence Ag | Safety device for an igniter, use of the safety device and method of activating an igniter with this safety device |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105352376B (en) * | 2015-09-24 | 2017-07-28 | 北京航天长征飞行器研究所 | A kind of small-sized anti high overload butt switch |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB218586A (en) * | 1923-08-16 | 1924-07-10 | Leon Emile Remondy | Improvements in or relating to fuses for projectiles |
US3124073A (en) * | 1964-03-10 | Proximity fuse | ||
DE1935392A1 (en) * | 1969-07-11 | 1971-01-14 | Schaberger & Co Gmbh Josef | Ground clearance fuse, especially for wing-stabilized projectiles |
GB2011042A (en) * | 1977-12-21 | 1979-07-04 | Kongsberg Vapenfab As | Combination fuze for missiles |
DE2829001A1 (en) * | 1978-07-01 | 1980-09-11 | Messerschmitt Boelkow Blohm | Missile multiple warhead construction - has distance sensors firing main warhead via time delay after auxiliary warheads |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3877378A (en) * | 1954-09-28 | 1975-04-15 | Us Army | Safety and arming mechanism |
-
1984
- 1984-05-07 DE DE8484105153T patent/DE3463295D1/en not_active Expired
- 1984-05-07 EP EP84105153A patent/EP0129679B1/en not_active Expired
- 1984-05-09 DE DE19848414161 patent/DE8414161U1/en not_active Expired
- 1984-06-06 NO NO842278A patent/NO158196C/en unknown
- 1984-06-13 CA CA000456492A patent/CA1262321A/en not_active Expired
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3124073A (en) * | 1964-03-10 | Proximity fuse | ||
GB218586A (en) * | 1923-08-16 | 1924-07-10 | Leon Emile Remondy | Improvements in or relating to fuses for projectiles |
DE1935392A1 (en) * | 1969-07-11 | 1971-01-14 | Schaberger & Co Gmbh Josef | Ground clearance fuse, especially for wing-stabilized projectiles |
GB2011042A (en) * | 1977-12-21 | 1979-07-04 | Kongsberg Vapenfab As | Combination fuze for missiles |
DE2829001A1 (en) * | 1978-07-01 | 1980-09-11 | Messerschmitt Boelkow Blohm | Missile multiple warhead construction - has distance sensors firing main warhead via time delay after auxiliary warheads |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4831932A (en) * | 1987-08-17 | 1989-05-23 | Honeywell Inc. | Detonator |
DE102021123375A1 (en) | 2021-09-09 | 2023-03-09 | Rwm Schweiz Ag | Ignition device for ammunition, in particular medium-caliber ammunition, and associated method for detonating or self-destructing ammunition, in particular medium-caliber ammunition |
WO2023036879A1 (en) | 2021-09-09 | 2023-03-16 | Rwm Schweiz Ag | Ignition device for ammunition, in particular medium-caliber ammunition, and associated method for ignition or for self-destruction of ammunition, in particular medium-caliber ammunition |
WO2023180278A1 (en) | 2022-03-23 | 2023-09-28 | Rheinmetall Air Defence Ag | Safety device for an igniter, use of the safety device and method of activating an igniter with this safety device |
DE102022106883A1 (en) | 2022-03-23 | 2023-09-28 | Rheinmetall Air Defence Ag | Fuse unit for a detonator, use of the fuse unit and method for activating a detonator with this fuse unit |
Also Published As
Publication number | Publication date |
---|---|
DE8414161U1 (en) | 1984-08-30 |
NO842278L (en) | 1984-12-27 |
DE3463295D1 (en) | 1987-05-27 |
CA1262321A (en) | 1989-10-17 |
NO158196B (en) | 1988-04-18 |
NO158196C (en) | 1988-07-27 |
EP0129679B1 (en) | 1987-04-22 |
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