EP1553381B1 - Zündeinrichtung - Google Patents

Zündeinrichtung Download PDF

Info

Publication number
EP1553381B1
EP1553381B1 EP04030557A EP04030557A EP1553381B1 EP 1553381 B1 EP1553381 B1 EP 1553381B1 EP 04030557 A EP04030557 A EP 04030557A EP 04030557 A EP04030557 A EP 04030557A EP 1553381 B1 EP1553381 B1 EP 1553381B1
Authority
EP
European Patent Office
Prior art keywords
rotor
force element
hole
ignition device
ignition
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
Application number
EP04030557A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP1553381A1 (de
Inventor
Wolfgang Zehnder
Kurt Pfundstein
Herbert Höni
Frank Kienzler
Alexander Zinell
Gerd Giesler
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
Priority to PL04030557T priority Critical patent/PL1553381T3/pl
Publication of EP1553381A1 publication Critical patent/EP1553381A1/de
Application granted granted Critical
Publication of EP1553381B1 publication Critical patent/EP1553381B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F42C15/18—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

Definitions

  • the invention relates to an ignition device according to the preamble of claim 1.
  • EP 0243987 discloses such an ignition device.
  • the force element cooperating with the rotor has a force element bolt, which is pulled out of the rotor for releasing the rotor for arming the ignition device. This means that in case of accidental ignition of the ignition device, the locking of the rotor canceled and thus a safe rotor lock is not guaranteed.
  • the invention is therefore an object of the invention to provide an ignition device of the type mentioned, in which at an unintentional ignition of the ignition device, the rotor remains reliably locked in the securing.
  • the rotor in the circumferential direction spaced from one another for securing associated first bore and a sharpening associated second bore, wherein the first bore is shorter than the second bore, and in that the force element comprises a force element bolt, the in the assurance of the rotor at an unintentional premature ignition of the ignition device is shot into the first bore and remains connected to the power element and locked the rotor, and which is fired to focus the rotor in the second bore and separated from the force element, after which the rotor the elastic drive element is rotated into the armed position, resulting in an inadvertent ignition advantageously a simple and safe rotor locking by the shot into the first bore of the rotor and connected to the force element remains en power element bolt.
  • first and the second bore are radially oriented in the rotor and the force element is radially oriented to the rotor.
  • the rotor is preferably formed with a circumferentially oriented elongated recess at one end of the first bore and at the opposite second end of the second bore is provided.
  • the force element bolt of the force element is in the securing position in the elongated recess of the rotor.
  • the pulse protection of the ignition device i. the first rotor lock, canceled, so the rotor rotates due to spin around an angle defined by the elongated recess in the rotor, the rotor however remains in the elongated recess in the securing by the engagement of the force element bolt.
  • the force element bolt In the armed position of the rotor, the force element bolt is shot into the second hole and is fixed in it - and separated from the force element - as has already been stated above.
  • the rotor can then rotate with the help of the elastic drive element provided on it in the armed position, so that the ignition chain of the swirl ammunition is "in line".
  • an ignition transformer is provided on the diametrically opposite side of the first and the second bore.
  • FIGS 1 to 4 illustrate an ignition device 10 for a swirl ammunition.
  • the ignition device 10 has a base 12, on which a rotor 14 is rotatably mounted. Between the base 12 and the rotor 14, an elastic drive element 16 is provided.
  • the elastic drive element 16 is formed by a mechanically tensioned coil spring.
  • the base part 12 has a force element 18 with a force element bolt 20.
  • the rotor 14 of the ignition device 10 is formed on its lateral surface 22 with an elongate recess 24 which is oriented in the circumferential direction of the rotor 14. At one end of the elongate recess 24 is a first bore 26 and at the opposite other end of the elongated recess 24, a second bore 28 is provided, which are radially oriented in the rotor 14. Accordingly, the force element 18 is radially oriented to the rotor 14.
  • a cover (not shown) can be arranged or arranged on the base part 12 in order to realize a self-contained ignition device 10.
  • pins 30 and holes 32 are formed.
  • an ignition transformer 34 is provided which is not “in line” in the illustrated in Fig. 1 assurance of the ignition device 10 with the ignition chain of the swirl ammunition.
  • the first bore 26 has a length that is smaller than the length of the second bore 28.
  • the ignition transformer 34 is provided in the rotor 14 of the ignition device 10 on the first and the second bore 26 and 28 diametrically opposite side.
  • the ignition transformer 34 provided in the rotor 14 is swung out of the ignition chain and secured.
  • This assurance of the rotor 14 is achieved by a (not shown) momentum protection of the rotor 14, which may be a per se known double bolt system, and characterized in that the force element bolt 20 of the force element 18 into the elongated recess 24 of the rotor 14 stands ,
  • the rotor 14 is locked in the Fig. 1 corresponding assurance. This locking is effected by the force element bolt 20 is shot into the first bore 26 of the rotor 14 and remains connected to the force element 18, because the first bore 26 is suitably short dimensioned. The rotor 14 remains locked in such a premature unintentional ignition so in the security; a further release is not possible.
  • the aforementioned first rotor protection i.e. the pulse fuse
  • the ignition device 10 remains in the securing position by engagement of the power element bolt 20 in the elongated recess 24 in the rotor 14, i. the ignition transformer 34 remains swung out of the ignition chain.
  • the arming of the rotor 14 of the ignition device 10 to its focus is done by shooting the power element pin 20 into the second bore 28, as Fig. 3 illustrates.
  • the second bore 28 has a length such that the force element pin 20 is separated from the force element 18 and fixed in the second bore 28.
  • the connection between the rotor 14 and the base part 12 of the ignition device 10 is released, so that the rotor 14 can rotate by means of the elastic drive element 16 in the armed position in which the ignition transformer 34 with the ignition chain is "in line".

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Devices For Conveying Motion By Means Of Endless Flexible Members (AREA)
  • Golf Clubs (AREA)
  • Toys (AREA)
EP04030557A 2004-01-12 2004-12-23 Zündeinrichtung Expired - Lifetime EP1553381B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL04030557T PL1553381T3 (pl) 2004-01-12 2004-12-23 Zapalnik

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102004001643 2004-01-12
DE102004001643A DE102004001643B3 (de) 2004-01-12 2004-01-12 Zündeinrichtung mit einem durch ein Kraftelement gesicherten Rotor

Publications (2)

Publication Number Publication Date
EP1553381A1 EP1553381A1 (de) 2005-07-13
EP1553381B1 true EP1553381B1 (de) 2007-11-28

Family

ID=34585395

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04030557A Expired - Lifetime EP1553381B1 (de) 2004-01-12 2004-12-23 Zündeinrichtung

Country Status (4)

Country Link
EP (1) EP1553381B1 (pl)
DE (2) DE102004001643B3 (pl)
IL (1) IL166095A (pl)
PL (1) PL1553381T3 (pl)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE444727B (sv) * 1982-04-30 1986-04-28 Bofors Ab Anordning vid sekringsorgan
SE452365B (sv) * 1986-03-13 1987-11-23 Ffv Affersverket Sekringsanordning for ammunitionstendror
DE10133832B4 (de) * 2001-07-12 2005-12-15 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Sicherungsvorrichtung für Zünder

Also Published As

Publication number Publication date
DE102004001643B3 (de) 2005-10-06
IL166095A0 (en) 2006-01-15
DE502004005598D1 (de) 2008-01-10
IL166095A (en) 2012-03-29
PL1553381T3 (pl) 2008-03-31
EP1553381A1 (de) 2005-07-13

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