EP1277024B1 - Electronic self-destruct device - Google Patents
Electronic self-destruct device Download PDFInfo
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- EP1277024B1 EP1277024B1 EP01936123A EP01936123A EP1277024B1 EP 1277024 B1 EP1277024 B1 EP 1277024B1 EP 01936123 A EP01936123 A EP 01936123A EP 01936123 A EP01936123 A EP 01936123A EP 1277024 B1 EP1277024 B1 EP 1277024B1
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- Prior art keywords
- capacitor
- comparator
- voltage
- capacitors
- time
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- 239000003990 capacitor Substances 0.000 claims abstract description 33
- 238000010304 firing Methods 0.000 claims description 8
- 238000007599 discharging Methods 0.000 claims description 3
- 238000000354 decomposition reaction Methods 0.000 description 3
- 230000003111 delayed effect Effects 0.000 description 3
- 230000001419 dependent effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 238000004146 energy storage Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
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Classifications
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- 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
- F42C15/44—Arrangements for disarming, or for rendering harmless, fuzes after arming, e.g. after launch
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
- F42C11/02—Electric fuzes with piezo-crystal
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
- F42C11/06—Electric fuzes with time delay by electric circuitry
-
- 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
- F42C9/16—Double fuzes; Multiple fuzes for self-destruction of ammunition
Definitions
- the present invention relates to a device for an electronic self-destructor in a projectile fuze without the use of a battery installed in the fuze.
- a self-decomposition function is also required in addition to the main ignition criteria such as service or time function, which ignites the explosive means even after not responding to the primary ignition criteria after expiration of a maximum operating time.
- This function which is connected in parallel with the other ignition criteria, is intended to limit the danger zone of the ammunition in the weft direction and / or to minimize the occurrence of unexploded ordnance. As a result, operations in previously fought areas safer because of lower risk of own duds.
- this function also allows the detonation of an entrapped enemy without endangering opposing troops or civil facilities beyond a reasonable level.
- the piezo element emits a high voltage during the firing process as a result of the high accelerations occurring there for a period of a few milliseconds, which is reloaded into storage capacitors for the longer-term operation of a power-saving electronics with a different voltage level.
- the problem of such a power supply is the use of the electronics to realize the most accurate time function, although the supply voltage varies greatly, since the power supply capacitors are charged only by the launch, but are then constantly discharged by the power to be supplied.
- the time function should be realized instead of mechanical oscillators, such as quartz or resonators that can be damaged during firing, for cost and reliability reasons with RC elements.
- the oscillation frequency of RC oscillators are so much dependent on the operating voltage that use for self-decomposition is generally out of the question.
- the comparator output changes state after this time. This change is used to ignite a downstream Zündthyristors that discharges a likewise charged separately by the piezoelectric element ignition capacitor in an electrical ignition means.
- the disadvantage lies in the dependence of Diszerlegerzeit t S of U 0 and U S. Since piezoelectric elements are subject to production fluctuations and are temperature-dependent, the voltage U 0 can fluctuate from shot to shot and thus also the self-destructor times. In addition, a stable switching threshold U S in turn requires a variable operating voltage circuit complexity, which leads to a higher complexity and power consumption.
- the comparator K is a commercially available integrated module with extremely low current consumption ( ⁇ 1 ⁇ A), very small input currents ( ⁇ 1 pA) and a common mode range extending to the operating voltage limits.
- the delayed supply of the operating voltage is to prevent a malfunction during the tube passage phase and the delayed charged capacitor C3 supplies the energy for driving the thyristor Th at the time of ignition.
- the ignition capacitor C4 is charged via the diode D3, and remains until the ignition of the thyristor at a sufficient voltage level.
- the two capacitors C1 and C2 are charged to the same voltage U o by the piezoelectric element via the two high-blocking diodes D1 and D2.
- the capacitor C1 is connected via a voltage divider R1 and R2 to the positive input of the comparator K.
- the capacitor C2 is connected directly to the negative input of the comparator and is discharged after the firing via the resistor R3.
- the potential at C2 (at the negative input of the comparator K) drops below the potential of C1 which decreases more slowly and is reduced by the factor R2 * / R e at the plus input of the comparator K.
- the comparator switches its output voltage to positive potential and thus ignites the ignition thyristor Th the current limiting resistor R6 and the voltage divider R7 and R8.
- the capacitor C5 is used for interference suppression and plays no role for the operating principle.
- the energy stored in the ignition capacitor C4 is thereby switched through to the electrical ignition means EZ and this causes it to trigger.
- the thyristor Th can be ignited by other circuit parts not shown here also on the Hauptzündkriterien.
- a changed field of use of the circuit is revealed when you can do the charging of the capacitors C0 to C4 instead of a piezoelectric element when fired by a voltage in a warhead, either permanently applied or shortly before the emission of submunition, controlled by a warhead electronics produced becomes.
- the circuit then serves for timed initiation of a self-decomposition of the ejected submunition. As long as on-board voltage is applied, neither C1 nor C2 discharges and nothing happens at the comparator output. Only when the voltage supply stops (ejection of the submunition), the self-destruct device is activated; the capacitors C1 and C2 begin to discharge and, as described, initiate the ignition process
- a shock generator can also be used.
- the piezoelectric element P would then be replaced by a shock generator, not shown.
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Abstract
Description
Die vorliegende Erfindung bezieht sich auf ein Vorrichtung für eine elektronische Selbstzerlegereinrichtung in einem Geschoßzünder ohne Verwendung einer im Zünder eingebauten Batterie.The present invention relates to a device for an electronic self-destructor in a projectile fuze without the use of a battery installed in the fuze.
Für heutige Geschoß- oder Submunitionszünder wird neben den Hauptzündkriterien wie Aufschlag- oder Zeitfunktion häufig auch eine Selbstzerlegungsfunktion gefordert, die das Sprengmittel auch nach Nichtansprechen der primären Zündkriterien nach Ablauf einer maximalen Funktionszeit zündet. Diese den anderen Zündkriterien parallelgeschaltete Funktion soll den Gefährdungsbereich der Munition in Schußrichtung begrenzen und / oder das Auftreten von Blindgängern minimieren. Dadurch werden Einsätze in vorher erkämpften Gebieten wegen geringerer Gefährdung durch eigene Blindgänger sicherer. Andererseits erlaubt diese Funktion auch den Beschuß eines eingeschlossenen Gegners ohne gegenüberstehende eigene Truppen oder zivile Einrichtungen über ein vertretbares Maß hinaus zu gefährden.For today's projectile or Submunitionszünder often a self-decomposition function is also required in addition to the main ignition criteria such as service or time function, which ignites the explosive means even after not responding to the primary ignition criteria after expiration of a maximum operating time. This function, which is connected in parallel with the other ignition criteria, is intended to limit the danger zone of the ammunition in the weft direction and / or to minimize the occurrence of unexploded ordnance. As a result, operations in previously fought areas safer because of lower risk of own duds. On the other hand, this function also allows the detonation of an entrapped enemy without endangering opposing troops or civil facilities beyond a reasonable level.
Mechanische, pyrotechnische und elektronische Selbstzerlegereinrichiungen sind in verschiedenen Ausführungsformen bekannt. Der vorliegenden Aufgabenstellung liegt der geforderte Betrieb einer elektronischen Selbstzerlegereinrichtung ohne die Verwendung einer Batterie zugrunde. Dies hat den Vorteil, daß die Selbstzerlegerfunktion derartig ausgerüsteter Zünder mit sehr großer Zuverlässigkeit auch über einen langen Lagerzeitraum des Zünders erhalten bleibt, da die Zuverlässigkeit von Zünderfunktionen im wesentlichen von der Zuverlässigkeit der Energieversorgung abhängt. Die Zuverlässigkeit der Selbstzerlegerfunktion ist jedoch über den taktischen Einsatz nicht nur funktionskritisch sondern sicherheitskritisch. Deswegen sollen möglichst alle die Funktionszuverlässigkeit beeinträchtigenden Bauelemente eliminiert werden.Mechanical, pyrotechnic and electronic Selbstzerlegereinrichiungen are known in various embodiments. The present task is based on the required operation of an electronic self-destructor without the use of a battery. This has the advantage that the Selbstzerlegerfunktion thus equipped igniter with very high reliability is maintained over a long storage period of the igniter, since the reliability of igniter functions depends essentially on the reliability of the power supply. However, the reliability of the self-destructor function is not only critical to the functioning of the tactical use but safety-critical. For this reason, as far as possible all functional reliability-impairing components should be eliminated.
Ausgehend von diesem Stand der Technik ist es daher die Aufgabe der vorliegenden Erfindung, eine neue Vorrichtung mit der Selbstzerlegerfunktion, speziell von Geschoßzündem anzugeben, die ohne Batterie auskommt.Starting from this prior art, it is therefore an object of the present invention to provide a new device with the Selbstzerlegerfunktion, especially of Geschoßzündem that does not require battery.
Bekannt ist, zum elektrischen Betrieb der Selbstzerlegereinrichtung die elektrische Energie eines oder mehrerer Piezoelemente zu verwenden. Das Piezoelement gibt beim Abschußvorgang infolge der dort auftretenden hohen Beschleunigungen für eine Zeitdauer von einigen Millisekunden eine hohe Spannung ab, die für den längerdauernden Betrieb einer stromsparenden Elektronik mit veränderter Spannungshöhe in Speicherkondensatoren umgeladen wird.It is known to use the electrical energy of one or more piezoelectric elements for the electrical operation of the self-destructor device. The piezo element emits a high voltage during the firing process as a result of the high accelerations occurring there for a period of a few milliseconds, which is reloaded into storage capacitors for the longer-term operation of a power-saving electronics with a different voltage level.
Das Problem einer derartigen Energieversorgung liegt beim Einsatz der Elektronik zur Realisierung einer möglichst genauen Zeitfunktion, obwohl die Versorgungsspannung sich sehr stark ändert, da die Energieversorgungskondensatoren nur durch den Abschuß geladen, anschließend jedoch durch den zu liefernden Strom ständig entladen werden. Die Zeitfunktion soll dabei statt durch mechanische Schwinger, wie Quarze oder Resonatoren, die beim Abschuß beschädigt werden können, aus Kosten- und Zuverlässigkeitsgründen mit RC-Gliedern realisiert werden. Die Schwingfrequenz von RC-Oszillatoren sind jedoch so stark von der Betriebsspannung abhängig, daß ein Einsatz für eine Selbstzerlegung im allgemeinen nicht in Frage kommt.The problem of such a power supply is the use of the electronics to realize the most accurate time function, although the supply voltage varies greatly, since the power supply capacitors are charged only by the launch, but are then constantly discharged by the power to be supplied. The time function should be realized instead of mechanical oscillators, such as quartz or resonators that can be damaged during firing, for cost and reliability reasons with RC elements. However, the oscillation frequency of RC oscillators are so much dependent on the operating voltage that use for self-decomposition is generally out of the question.
Nun könnte man die Ausgangsspannung eines Energiespeicherkondensators mit Hilfe eines Schaltreglers stabilisieren, um der Elektronik eine möglichst konstante Spannung anzubieten. Dies hat den Nachteil eines relativ großen Schaltungsaufwands verbunden mit Energieverlusten durch die Spannungsumsetzung.Now you could stabilize the output voltage of an energy storage capacitor using a switching regulator to offer the electronics as constant as possible voltage. This has the disadvantage of a relatively large amount of circuitry associated with energy losses through the voltage conversion.
Aus der
Eine zweite Lösung wäre, zur Realisierung der Zeitfunktion die Ausgangsspannung des Piezoelements zu verwenden, damit einen Kondensator C auf die Spannung Uo aufzuladen und diesen definiert über einen Widerstand R zu entladen, um mit Hilfe eines Komparators das Unterschreiten einer bestimmten Spannungshöhe US zu detektieren, das nach der Zeit
Bei dieser Lösung liegt der Nachteil in der Abhängigkeit der Selbstzerlegerzeit tS von U0 und US. Da Piezoelemente Fertigungschwankungen unterliegen und temperaturabhängig sind, kann die Spannung U0 von Schuß zu Schuß schwanken und damit auch die Selbstzerlegerzeiten. Zudem erfordert eine stabile Schaltschwelle US bei veränderlicher Betriebsspannung wiederum Schaltungsaufwand, der zu einer höheren Komplexität und Stromaufnahme führt.In this solution, the disadvantage lies in the dependence of Selbstzerlegerzeit t S of U 0 and U S. Since piezoelectric elements are subject to production fluctuations and are temperature-dependent, the voltage U 0 can fluctuate from shot to shot and thus also the self-destructor times. In addition, a stable switching threshold U S in turn requires a variable operating voltage circuit complexity, which leads to a higher complexity and power consumption.
Eine ähnliche Lösung ist aus der
Es soll deshalb eine Schaltung bereitgestellt werden, die einerseits möglichst einfach und deswegen möglichst energiesparend, preiswert und dabei (wegen reduzierter Bauteileanzahl) zuverlässig ist und die andererseits die Zeitfunktion mit RC-Gliedern unabhängig von einer schwankenden Versorgungsspannungshöhe zu realisieren gestattet.It is therefore a circuit to be provided, on the one hand as simple as possible and energy-saving, inexpensive and thereby (due to reduced number of components) is reliable and on the other hand allows to realize the time function with RC elements regardless of a fluctuating supply voltage level.
Dies gelingt mit der im Patentanspruch 1 beschriebenen Vorrichtung. Dadurch wirken sich weder die Einflüsse einer sich ständig verändernden Betriebsspannung noch die Einflüsse der Abgabe von veränderlichen Spannungshöhen durch das Piezoelement auf die Zeitfunktion aus. Die Patentansprüche 2 bis 3 betreffen vorteilhafte Ausgestaltungen der Erfindung. Im folgenden sei anhand der beigefügten Fig. 1 die Erfindung kurz erläutert.This is possible with the device described in claim 1. As a result, neither the influences of a constantly changing operating voltage nor the influences of the output of variable voltage levels by the piezoelectric element affect the time function. The claims 2 to 3 relate to advantageous embodiments of the invention. In the following, the invention will be briefly explained with reference to the accompanying Fig. 1.
Über ein Piezoelement P, einen Vorwiderstand R0, eine Zenerdiode Z (zur Spannungsbegrenzung) und die Dioden D0 bis D3 werden beim Abschuß die Kondensatoren C0 bis C4 aufgeladen. Der aufgeladene Kondensator C0 stellt danach, über den Widerstand R4 und den zweiten Speicherkondensator C3 verzögert, die Versorgungsspannung für den Betrieb des Komparators K bereit. Der Komparator K ist ein handelsüblicher integrierter Baustein mit extrem kleiner Stromaufnahme (< 1 µA), sehr kleinen Eingangsströmen (< 1 pA) und einem bis an die Betriebsspannungsgrenzen reichenden Gleichtaktbereich.Via a piezoelectric element P, a series resistor R0, a Zener diode Z (for limiting the voltage) and the diodes D0 to D3, the capacitors C0 to C4 are charged during firing. The charged capacitor C0 then provides, via the resistor R4 and the second storage capacitor C3 delayed, the supply voltage for the operation of the comparator K ready. The comparator K is a commercially available integrated module with extremely low current consumption (<1 μA), very small input currents (<1 pA) and a common mode range extending to the operating voltage limits.
Die verzögerte Bereitstellung der Betriebsspannung soll eine Fehlfunktion während der Rohrdurchgangsphase verhindern und der verzögert aufgeladene Kondensator C3 liefert zum Zeitpunkt der Zündung die Energie zur Ansteuerung des Thyristors Th.The delayed supply of the operating voltage is to prevent a malfunction during the tube passage phase and the delayed charged capacitor C3 supplies the energy for driving the thyristor Th at the time of ignition.
Der Zündkondensator C4 wird über die Diode D3 aufgeladen, und bleibt bis zur Zündung des Thyristors auf einer ausreichenden Spannungshöhe.The ignition capacitor C4 is charged via the diode D3, and remains until the ignition of the thyristor at a sufficient voltage level.
Zur Realisierung einer von der durch das Piezoelement abgegebenen Spannung unabhängigen Zeitfunktion werden erfindungsgemäß über die beiden hochsperrenden Dioden D1 und D2 die beiden Kondensatoren C1 und C2 durch das Piezoelement auf die gleiche Spannung Uo aufgeladen.In order to realize a time-independent function of the voltage delivered by the piezoelectric element, the two capacitors C1 and C2 are charged to the same voltage U o by the piezoelectric element via the two high-blocking diodes D1 and D2.
Der Kondensator C1 ist über einen Spannungsteiler R1 und R2 an den Pluseingang des Komparators K angeschlossen. Der Kondensator C2 ist direkt mit dem Minuseingang des Komparators verbunden und wird nach dem Abschuß über den Widerstand R3 entladen.The capacitor C1 is connected via a voltage divider R1 and R2 to the positive input of the comparator K. The capacitor C2 is connected directly to the negative input of the comparator and is discharged after the firing via the resistor R3.
Zur schnellen und sicheren Umschaltung ist der Komparator K über den Widerstand R5 mitgekoppelt, besitzt also eine Hysterese. Nach dem Abschuß liegt wegen des Spannungsteilers R1 und R2 am Minuseingang des Komparators K eine höhere positive Spannung als am Pluseingang. Der Ausgang des Komparators befindet sich deshalb zu diesem Zeitpunkt auf Nullpotential. Der Kondensator C1 wird dann über den Ersatzwiderstand Re = R1 + R2* mit R2* = R2 ∥ R5 = R2 R5 / (R2 + R5) entladen.For fast and safe switching of the comparator K is coupled via the resistor R5, so has a hysteresis. After firing is because of the voltage divider R1 and R2 at the negative input of the comparator K, a higher positive voltage than at the plus input. The output of the comparator is therefore at zero potential at this time. The capacitor C1 is then discharged via the equivalent resistance R e = R 1 + R 2 * with R 2 * = R 2 ∥ R 5 = R 2 R 5 / (R 2 + R 5).
Die Zeitkonstanten τ1 = Re C1 und τ2 = R3 C2 sind so gewählt, daß τ1 > τ2, d.h. C2 entlädt sich schneller als C1. Zum Zeitpunkt der eingestellten Selbstzerlegerzeit
Die im Zündkondensator C4 gespeicherte Energie wird dadurch auf das elektrische Zündmittel EZ durchgeschaltet und dieses damit zur Auslösung gebracht. Über den skizzierten Eingang T kann der Thyristor Th von anderen hier nicht aufgezeigten Schaltungsteilen auch über die Hauptzündkriterien gezündet werden.The energy stored in the ignition capacitor C4 is thereby switched through to the electrical ignition means EZ and this causes it to trigger. On the sketched input T, the thyristor Th can be ignited by other circuit parts not shown here also on the Hauptzündkriterien.
Eine weitere Vereinfachung der Schaltung und der Berechnung ergibt sich, wenn man die Kondensatoren C1 und C2 gleich groß wählt: C1 = C2 = C. Die Selbstzerlegerzeit ts ergibt sich dann zu
Durch die Differenzbildung der vorliegenden Komparatorbeschaltung geht weder in die Gleichung (2) noch in die Gleichung (3) eine beim Schuß veränderliche Größe ein. Das Ziel der Aufgabenstellung ist damit erreicht.Due to the difference formation of the present comparator circuit, neither the equation (2) nor the equation (3) assumes a variable which is variable during firing. The goal of the task is thus achieved.
Ein verändertes Einsatzgebiet der Schaltung erschließt sich, wenn man die Aufladung der Kondensatoren C0 bis C4 statt durch ein Piezoelement beim Abschuß durch eine Spannung in einem Gefechtskopf erfolgen läßt, die entweder permanent anliegt oder kurz vor dem Ausstoß von Submunition, durch eine Gefechtskopfelektronik gesteuert, erzeugt wird. Die Schaltung dient dann zur zeitgesteuerten Auslösung einer Selbstzerlegung der ausgestoßenen Submunition. Solange Bordspannung anliegt, entlädt sich weder C1 noch C2 und am Komparatorausgang geschieht nichts. Erst wenn die Spannungsversorgung abreißt (Ausstoß der Submunition) wird die Selbstzerlegevorrichtung aktiviert; die Kondensatoren C1 und C2 beginnen sich zu entladen und leiten, wie beschrieben, den Zündvorgang einA changed field of use of the circuit is revealed when you can do the charging of the capacitors C0 to C4 instead of a piezoelectric element when fired by a voltage in a warhead, either permanently applied or shortly before the emission of submunition, controlled by a warhead electronics produced becomes. The circuit then serves for timed initiation of a self-decomposition of the ejected submunition. As long as on-board voltage is applied, neither C1 nor C2 discharges and nothing happens at the comparator output. Only when the voltage supply stops (ejection of the submunition), the self-destruct device is activated; the capacitors C1 and C2 begin to discharge and, as described, initiate the ignition process
An Stelle des im Zusammenhang mit dem Ausführungsbeispiel verwendeten Piezoelements kann auch ein Stoßgenerator verwendet werden. In Fig. 1 wäre das Piezoelement P dann durch einen nicht dargestellten Stoßgenerator zu ersetzen.Instead of the piezoelectric element used in connection with the exemplary embodiment, a shock generator can also be used. In Fig. 1, the piezoelectric element P would then be replaced by a shock generator, not shown.
Claims (3)
- Apparatus for the time-controlled self-destruction of a projectile by means of an electronic self-destruct device without batteries, wherein a plurality of capacitors (C0, C1, C2, C3, C4) which are charged during firing by a piezo element (P) or a surge generator are used for operation in the flight phase, characterised in that at least a first and a second of the capacitors (C1, C2) have the same voltage (U0) after charging, and in that the first capacitor (C1) is connected via a voltage divider (R1, R2) to the plus input of a comparator (K) and the second capacitor (C2) is connected directly to the minus input of the comparator (K) in such a way that the potential at the minus input of the comparator (K) after firing is greater than the potential at the plus input of the comparator (K), and in that the time constant (τ1) for discharging the first capacitor (C1) is greater than the time constant (τ2) for discharging the second capacitor (C2).
- Apparatus according to claim 1, characterised in that the first capacitor (C1) is discharged across the voltage divider (R1, R2) and the second capacitor (C2) is discharged across a resistor (R3).
- Apparatus according to one of the preceding claims, characterised in that the comparator (K) is coupled via a resistor (R5).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
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DE10020037A DE10020037C1 (en) | 2000-04-22 | 2000-04-22 | Electronic self-destruct device has capacitors connected to comparator so varying operating voltage and output of variable voltage amplitudes by piezoelement do not affect timing |
DE10020037 | 2000-04-22 | ||
PCT/EP2001/003263 WO2001081855A1 (en) | 2000-04-22 | 2001-03-22 | Electronic self-destruct device |
Publications (2)
Publication Number | Publication Date |
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EP1277024A1 EP1277024A1 (en) | 2003-01-22 |
EP1277024B1 true EP1277024B1 (en) | 2007-06-27 |
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Application Number | Title | Priority Date | Filing Date |
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EP01936123A Expired - Lifetime EP1277024B1 (en) | 2000-04-22 | 2001-03-22 | Electronic self-destruct device |
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US (1) | US6865989B2 (en) |
EP (1) | EP1277024B1 (en) |
AT (1) | ATE365902T1 (en) |
AU (1) | AU6212501A (en) |
DE (2) | DE10020037C1 (en) |
WO (1) | WO2001081855A1 (en) |
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US7752952B1 (en) * | 2005-03-22 | 2010-07-13 | The United States Of America As Represented By The Secretary Of The Army | Dynamic barrier system |
DE102005030263B3 (en) | 2005-06-29 | 2006-11-30 | Rheinmetall Waffe Munition Gmbh | Safety system for programmable munitions comprises self-destruct device that is activated if detonator test is failed and is overridden if detonator test is passed |
US10447179B2 (en) * | 2007-07-10 | 2019-10-15 | Omnitek Partners Llc | Inertially operated piezoelectric energy harvesting electronic circuitry |
US9910060B2 (en) * | 2007-07-10 | 2018-03-06 | Omnitek Partners Llc | Piezoelectric-based multiple impact sensors and their electronic circuitry |
US10581347B2 (en) * | 2007-07-10 | 2020-03-03 | Omnitek Partners Llc | Manually operated piezoelectric energy harvesting electronic circuitry |
US8281719B2 (en) * | 2008-06-10 | 2012-10-09 | Omnitek Partners LLC. | Integrated power source and safety mechanisms for submunitions self-destruct fuze and the like |
US11248893B2 (en) * | 2008-06-29 | 2022-02-15 | Omnitek Partners Llc | Inertially operated piezoelectric energy harvesting electronic circuitry |
US10598473B2 (en) * | 2008-06-29 | 2020-03-24 | Omnitek Partners Llc | Inertially operated piezoelectric energy harvesting electronic circuitry |
WO2010053407A1 (en) * | 2008-11-05 | 2010-05-14 | Saab Ab | An ignition and delay circuit |
SG184603A1 (en) * | 2011-04-02 | 2012-10-30 | Advanced Material Engineering Pte Ltd | Electro-mechanical fuze for a projectile |
RU2479822C1 (en) * | 2011-11-07 | 2013-04-20 | Федеральное государственное унитарное предприятие "Российский Федеральный ядерный центр - Всероссийский научно-исследовательский институт экспериментальной физики" - ФГУП "РФЯЦ-ВНИИЭФ" | Electronic device of ammunition self-destruction |
DE102015116985A1 (en) | 2015-10-06 | 2017-04-06 | Rheinmetall Waffe Munition Gmbh | Self-consuming bullet |
US10097010B2 (en) * | 2016-04-19 | 2018-10-09 | Infineon Technologies Ag | Control of freewheeling voltage |
EP3575888B1 (en) | 2018-05-30 | 2023-04-12 | Rolex Sa | Timepiece comprising an aspheric lens |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4240350A (en) * | 1977-09-16 | 1980-12-23 | Werkzeugmaschinenfabrik Oerlikon-Buhrle | Electronic fuze |
Family Cites Families (9)
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---|---|---|---|---|
DE2143119C3 (en) * | 1971-08-28 | 1979-03-22 | Diehl Fa | Electric projectile fuse |
DE2314273C3 (en) * | 1973-03-22 | 1981-05-21 | Diehl GmbH & Co, 8500 Nürnberg | Ignition circuit for self-destruction of a projectile |
US4712477A (en) | 1985-06-10 | 1987-12-15 | Asahi Kasei Kogyo Kabushiki Kaisha | Electronic delay detonator |
DE3800328C2 (en) * | 1988-01-08 | 1996-01-04 | Diehl Gmbh & Co | Projectile with electronic detonator circuit |
GB2227384B (en) * | 1988-11-18 | 1992-05-27 | Graviner Ltd Kidde | Electrical timing arrangements and methods |
US5269223A (en) | 1992-10-06 | 1993-12-14 | Ems-Patvag | Piezoelectric fuse system with safe and arm device for ammunition |
DE4324486C1 (en) * | 1993-07-21 | 1995-01-19 | Siemens Ag | Arrangement for evaluating a Hall-probe signal |
DE19504870C2 (en) * | 1995-02-14 | 1997-01-23 | Siemens Ag | Sensor arrangement |
US5942714A (en) | 1997-12-31 | 1999-08-24 | Aai Corporation | Accurate ultra low power fuze electronics |
-
2000
- 2000-04-22 DE DE10020037A patent/DE10020037C1/en not_active Expired - Lifetime
-
2001
- 2001-03-22 AT AT01936123T patent/ATE365902T1/en not_active IP Right Cessation
- 2001-03-22 AU AU62125/01A patent/AU6212501A/en not_active Abandoned
- 2001-03-22 DE DE50112664T patent/DE50112664D1/en not_active Expired - Lifetime
- 2001-03-22 WO PCT/EP2001/003263 patent/WO2001081855A1/en active IP Right Grant
- 2001-03-22 EP EP01936123A patent/EP1277024B1/en not_active Expired - Lifetime
- 2001-03-22 US US10/258,235 patent/US6865989B2/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4240350A (en) * | 1977-09-16 | 1980-12-23 | Werkzeugmaschinenfabrik Oerlikon-Buhrle | Electronic fuze |
Also Published As
Publication number | Publication date |
---|---|
EP1277024A1 (en) | 2003-01-22 |
DE50112664D1 (en) | 2007-08-09 |
WO2001081855A1 (en) | 2001-11-01 |
AU6212501A (en) | 2001-11-07 |
DE10020037C1 (en) | 2001-08-23 |
US6865989B2 (en) | 2005-03-15 |
ATE365902T1 (en) | 2007-07-15 |
US20030136290A1 (en) | 2003-07-24 |
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