EP1909059A1 - Fusée à détonateur - Google Patents

Fusée à détonateur Download PDF

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Publication number
EP1909059A1
EP1909059A1 EP07018763A EP07018763A EP1909059A1 EP 1909059 A1 EP1909059 A1 EP 1909059A1 EP 07018763 A EP07018763 A EP 07018763A EP 07018763 A EP07018763 A EP 07018763A EP 1909059 A1 EP1909059 A1 EP 1909059A1
Authority
EP
European Patent Office
Prior art keywords
detonator
projectile
time
ignition
flight
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP07018763A
Other languages
German (de)
English (en)
Other versions
EP1909059B1 (fr
Inventor
Frank Kienzler
Wolfgang Schillinger
Wolfgang Zehnder
Reiner Hennig
Esther Laufer
Siegfried Paulini
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Junghans Microtec GmbH
Original Assignee
Junghans Microtec GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Junghans Microtec GmbH filed Critical Junghans Microtec GmbH
Publication of EP1909059A1 publication Critical patent/EP1909059A1/fr
Application granted granted Critical
Publication of EP1909059B1 publication Critical patent/EP1909059B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/28Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
    • F42C15/31Arming-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/18Arming-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
    • F42C15/188Arming-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/40Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected electrically

Definitions

  • the invention relates to a projectile fuze according to the preamble of claim 1.
  • Such a projectile fuse is used for example as a mortar fuse.
  • Realized is such electrical safety overflight in such a way that by means of an external programmer, the time of flight of the projectile is programmed into the detonator electronics ie fed. After the launch of the projectile, a timer / counter is started, which counts up to the programmed flight time minus a fixed time value and then charges an electrical ignition circuit of the ignition electronics. This charging of the ignition circuit is in the msec range, so that the projectile fuze is ready to fire in time in the specified target.
  • the securing device is designed such that after a very short in relation to the total trajectory very short time period, the mechanical interruption of the ignition chain is canceled, i. the so-called pre-pipe safety is comparatively small.
  • the invention is in the knowledge of these circumstances, the task of creating a projectile fuse of the type mentioned, which has a programmable electrical and mechanical safety overflight and a comparatively large Vorrohrpiping.
  • the safety device is blocked by a pyrotechnic force element as long as possible, i. held in the safe until the programmed or, if necessary, also manually set flight time - minus a fixed time value (speed safety) is reached. If the set flight time minus the set time value is reached, the ignition circuit for the force element is charged and the safety device is unlocked by igniting the force element. The fuse then goes into focus, i. the ignition chain is broken and the ignition chain is then inline. Now, the actual ignition circuit of the projectile fuze according to the invention is charged, so that the detonator in the intended destination is ready in time to fire.
  • FIG. 1 illustrates a trajectory 10 of a projectile having a conventional projectile fuse, wherein the arrow V designates the pre-pipe safety, the arrow Ü the overflight safety, and the arrow T the time of flight or target distance. With h the ignition height of the projectile fuze is designated.
  • FIG. 2 illustrates, in a representation similar to FIG. 1, the trajectory 10 of a projectile having a projectile fuse according to the invention, the arrow V once again designating the mechanical pre-pipe safety and the arrow T designating the time of flight or target distance.
  • H in Figure 2 denotes the ignition height of the projectile fuze.
  • the arrow Ü also indicates the safety against overflight in FIG. 2, which, however, is an electrical / mechanical overflight safety, the point S designating the point of focus of the safety device of the projectile fuze.
  • FIG. 3 shows a longitudinal section of an embodiment of the projectile fuze 12 according to the invention, which has a pyrotechnic force element 14 which is interconnected with ignition electronics and blocks a safety device 16 until the time of flight T minus a predetermined time value ⁇ t (see FIG. 2). is reached. Once that is the case, an ignition circuit of the projectile fuze 12 is electrically charged and the safety device 16 is unlocked by igniting the pyrotechnic force element 14 in the armed position.
  • FIG. 3 shows the securing of the securing device.
  • the securing device 16 has a rotor 18 with a firing pin 20 and with a puncture detonator 22.
  • the firing pin 20 and the piercing detonator 22 are aligned with each other axially and are spaced from each other.
  • the projectile fuze 12 has an electric detonator 24, which is interconnected with the ignition electronics.
  • the projectile fuze 12 also has an booster charge 26 associated with the electric detonator 24.
  • the rotor 18 is provided between the electric detonator 24 and the booster charge 26.
  • FIG. 4 illustrates, in a longitudinal section similar to FIG. 3, another embodiment of the projectile fuse 12 according to the invention, wherein the same details are denoted by the same reference numerals as in FIG. 3, so that it is not necessary to describe all these details in connection with FIG.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Automotive Seat Belt Assembly (AREA)
  • Elimination Of Static Electricity (AREA)
EP07018763A 2006-10-02 2007-09-25 Fusée de projectile Active EP1909059B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102006046811A DE102006046811A1 (de) 2006-10-02 2006-10-02 Geschosszünder

Publications (2)

Publication Number Publication Date
EP1909059A1 true EP1909059A1 (fr) 2008-04-09
EP1909059B1 EP1909059B1 (fr) 2011-01-26

Family

ID=38830372

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07018763A Active EP1909059B1 (fr) 2006-10-02 2007-09-25 Fusée de projectile

Country Status (4)

Country Link
US (1) US7614346B2 (fr)
EP (1) EP1909059B1 (fr)
DE (2) DE102006046811A1 (fr)
ZA (1) ZA200708353B (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8528478B2 (en) 2009-09-04 2013-09-10 Raytheon Company Safe arming system and method
US8291825B2 (en) * 2009-09-10 2012-10-23 Alliant Techsystems Inc. Methods and apparatuses for electro-mechanical safety and arming of a projectile

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3451340A (en) 1966-07-28 1969-06-24 Tamerlan Anstalt Percussion fuze including rotary delay provisions
EP0425877A2 (fr) * 1989-10-23 1991-05-08 Gebrüder Junghans Gmbh Dispositif de sécurité pour fusée de projectile
US5693906A (en) 1995-09-28 1997-12-02 Alliant Techsystems Inc. Electro-mechanical safety and arming device
EP1225418A1 (fr) 1999-10-27 2002-07-24 Instalaza, S.A. Ameliorations portant sur des fusees mecano-electroniques pour grenades a main

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4145971A (en) * 1977-10-19 1979-03-27 Motorola, Inc. Electronic time delay safety and arming mechanism
US4334475A (en) * 1980-02-07 1982-06-15 Fratelli Borletti S.P.A. Proximity fuses
DE10000177A1 (de) * 2000-01-05 2001-07-12 Junghans Feinwerktechnik Gmbh Zündeinrichtung, insbesondere für eine Mörsergranate
DE20023637U1 (de) * 2000-09-05 2005-05-19 Junghans Feinwerktechnik Gmbh & Co. Kg Zündervorrichtung für ein Geschoss
DE10133832B4 (de) * 2001-07-12 2005-12-15 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Sicherungsvorrichtung für Zünder
US6883434B2 (en) * 2001-09-17 2005-04-26 Junghans Feinwerktechnik Gmbh & Co. Kg Fuse device for a projectile
DE10302967B4 (de) * 2003-01-25 2006-04-06 Junghans Feinwerktechnik Gmbh & Co. Kg Geschosszünder mit einem Kraftelement
DE102005003942B4 (de) * 2005-01-28 2007-04-12 Junghans Feinwerktechnik Gmbh & Co. Kg Sicherungseinrichtung für einen Drallgeschosszünder
DE102005029326B4 (de) * 2005-06-24 2007-04-05 Junghans Feinwerktechnik Gmbh & Co. Kg Sicherungseinrichtung für einen Drallgeschosszünder mit einem kugelartigen Rotor

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3451340A (en) 1966-07-28 1969-06-24 Tamerlan Anstalt Percussion fuze including rotary delay provisions
EP0425877A2 (fr) * 1989-10-23 1991-05-08 Gebrüder Junghans Gmbh Dispositif de sécurité pour fusée de projectile
US5693906A (en) 1995-09-28 1997-12-02 Alliant Techsystems Inc. Electro-mechanical safety and arming device
EP1225418A1 (fr) 1999-10-27 2002-07-24 Instalaza, S.A. Ameliorations portant sur des fusees mecano-electroniques pour grenades a main

Also Published As

Publication number Publication date
US20080078299A1 (en) 2008-04-03
DE502007006356D1 (de) 2011-03-10
ZA200708353B (en) 2008-10-29
EP1909059B1 (fr) 2011-01-26
DE102006046811A1 (de) 2008-04-03
US7614346B2 (en) 2009-11-10

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