EP1133670B1 - Mörserzünder mit einem windrad - Google Patents

Mörserzünder mit einem windrad Download PDF

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Publication number
EP1133670B1
EP1133670B1 EP99961015A EP99961015A EP1133670B1 EP 1133670 B1 EP1133670 B1 EP 1133670B1 EP 99961015 A EP99961015 A EP 99961015A EP 99961015 A EP99961015 A EP 99961015A EP 1133670 B1 EP1133670 B1 EP 1133670B1
Authority
EP
European Patent Office
Prior art keywords
battery
wheel
mortar
activating
container
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
EP99961015A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP1133670A1 (de
Inventor
Rainer Heck
Reiner Hennig
Frank Kienzler
Detlef Pabst
Jürgen Voigt
Wolfgang Zehnder
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 Feinwerktechnik GmbH and Co KG
Junghans Microtec GmbH
Original Assignee
Junghans Feinwerktechnik GmbH and Co KG
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 Feinwerktechnik GmbH and Co KG, Junghans Microtec GmbH filed Critical Junghans Feinwerktechnik GmbH and Co KG
Priority to SI9930294T priority Critical patent/SI1133670T1/xx
Publication of EP1133670A1 publication Critical patent/EP1133670A1/de
Application granted granted Critical
Publication of EP1133670B1 publication Critical patent/EP1133670B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F42C15/295Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids operated by a turbine or a propeller; Mounting means therefor
    • 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
    • F42C11/00Electric fuzes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/21Rotors for wind turbines
    • F05B2240/211Rotors for wind turbines with vertical axis

Definitions

  • the invention relates to a mortar detonator with a wind turbine according to the preamble of claim 1.
  • a wind turbine generator which is characterized by the Wind wheel rotating in the air flow to generate the energy for the detonator and for driving the safety device serves
  • Such wind turbine generators have the disadvantage that the energy generated depends on the speed of the wind generator, which is at the apex the trajectory of the mortar can drop to zero. This can lead to a power cut, at least lead to impairment of the reliability of the igniter.
  • Another problem is that the wind turbine freezes and during flight can come to a standstill, also with the problem of energy failure.
  • the invention has set itself the goal of creating a mortar detonator of high reliability, in which the power supply of the igniter does not depend on a constant rotation of the Wind turbine depends.
  • the invention solves this problem according to the feature of the invention Main claim.
  • the invention is therefore based on the fact that by using a known activatable Battery during the flight an activation wheel driven by the wind wheel with a predetermined time delay between firing the projectile and reaching the Activation position is activated. Depending on the type of battery used, activation is required again a certain period of time before the battery is fully functional. At the latest At this point, the speed of the igniter is no longer important of the wind turbine.
  • the Invention provided that the activation wheel along a worm gear on the axis of rotating wind wheel can be moved and brought into contact with the activatable battery.
  • the activatable battery from a battery container with the battery cells and one immediately adjacent, but separate acid container, the latter by the Activation wheel is piercable, causing acid to flow into the battery container.
  • the activation wheel has a magnet that turns on its rotation passes a coil and generates energy.
  • This energy is used to power the battery during the activation phase Igniter and in particular for the energy supply for a counter that the time function of Zünders controls.
  • one, one or more Emergency power supply containing capacitors is provided, which with the Activation wheel works together and the function of the counter in any Power failure of the battery ensures.
  • the emergency power supply is also with the Can be used with a wind turbine generator.
  • Fig. 1 the essential components in connection with the invention are one Mortar detonator drawn in a highly schematic representation.
  • 1 is a wind turbine, with 2 a battery, with 3 the safety device, with 4 the electronics and with 5 the ignition designated.
  • the battery 2 consists of a battery container 6 and battery cells 7.
  • the battery container is in the idle state of the igniter, i.e. in the not shot down Condition, no acid.
  • the battery is therefore not yet functional.
  • Above the Battery container is an acid container 8, which in the activation case after Launch is destroyed, so that the acid in the battery container below can drain.
  • the battery container and the acid container are each annular and form one cylindrical space, which is penetrated by the axis 9 of the wind turbine.
  • a worm gear 10 is attached, on which in turn a gear 11 is longitudinally displaceable can move.
  • the gear 11 runs along the Worm gear 10 upwards and destroys the acid container 8.
  • Electric coil 12 which has a magnetic assignment 13 on the gear 11th cooperates and in which when the gear rotates energy for the power supply the igniter and any emergency power supply are generated.
  • a double bolt is designated, which is the primary The fuse system of the detonator is released when fired and thereby the wind turbine 1 releases.
  • This double bolt is a common component in detonators and will not be described here described.
  • a worm wheel 15 and a serves for the mechanical release of the safety device 3 Safety bolt 16.
  • the worm wheel meshes on axis 9 and works with one Worm gear on a safety pin 16 together.
  • axis 9 is rotated unscrewed over the worm wheel 15 of the locking bolt 16 and the Security device 3, which has a mechanical detonator 3a and an ignition transmitter 3b, released in focus.
  • a spring 13 serves to secure the arming device.
  • the ignition electronics 4 consists of an ignition circuit 4a and an electrical detonator 4b and is powered by the battery or coil 12.
  • the worm wheel 15 is rotated by the axis 9 and in turn rotates the Safety bolt 16 out of its rest position, whereby the safety device 3rd released and pressed by the spring 3c in its focus.
  • the detonator is now fully focused.
  • This emergency power supply will charged by the current pulses generated in the coil 12 by the magnet 13 and stores its energy content for the duration of the flight of the projectile.
  • the coil 12 A rectifier 17 is arranged downstream, to which a first supply capacitor 18 is connected for the power supply of the downstream ignition electronics 19 and a second Supply capacitor 20 are connected to a subordinate time counter 21.
  • On Controller 22 serves to control the ignition electronics 19 and the time counter 21 Speed of the wind turbine 1 and thus the output voltage of the coil 12, under one predetermined threshold value, the controller 22 is switched via the rectifier 17 and switches off the ignition electronics 19 as well as itself.

Landscapes

  • General Engineering & Computer Science (AREA)
  • Engineering & Computer Science (AREA)
  • Wind Motors (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Toys (AREA)
  • Fuses (AREA)
  • Preparation Of Clay, And Manufacture Of Mixtures Containing Clay Or Cement (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
  • Vaporization, Distillation, Condensation, Sublimation, And Cold Traps (AREA)
  • On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)
  • Medicines Containing Plant Substances (AREA)
  • External Artificial Organs (AREA)
  • Manufacturing Of Micro-Capsules (AREA)
  • Road Signs Or Road Markings (AREA)
  • Agricultural Chemicals And Associated Chemicals (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
  • Air Bags (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Battery Mounting, Suspending (AREA)
EP99961015A 1998-11-26 1999-11-26 Mörserzünder mit einem windrad Expired - Lifetime EP1133670B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SI9930294T SI1133670T1 (en) 1998-11-26 1999-11-26 Mortar fuze with a rotatable fan

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19854607 1998-11-26
DE19854607A DE19854607A1 (de) 1998-11-26 1998-11-26 Mörserzünder mit einem Windrad
PCT/EP1999/009195 WO2000031497A1 (de) 1998-11-26 1999-11-26 Mörserzünder mit einem windrad

Publications (2)

Publication Number Publication Date
EP1133670A1 EP1133670A1 (de) 2001-09-19
EP1133670B1 true EP1133670B1 (de) 2003-03-12

Family

ID=7889123

Family Applications (1)

Application Number Title Priority Date Filing Date
EP99961015A Expired - Lifetime EP1133670B1 (de) 1998-11-26 1999-11-26 Mörserzünder mit einem windrad

Country Status (18)

Country Link
US (1) US6481354B1 (ko)
EP (1) EP1133670B1 (ko)
JP (1) JP2002530626A (ko)
KR (1) KR20010101054A (ko)
AT (1) ATE234456T1 (ko)
CA (1) CA2350585A1 (ko)
CZ (1) CZ292721B6 (ko)
DE (2) DE19854607A1 (ko)
DK (1) DK1133670T3 (ko)
ES (1) ES2196896T3 (ko)
HU (1) HU221930B1 (ko)
IL (1) IL143312A0 (ko)
NO (1) NO20012576L (ko)
PL (1) PL347826A1 (ko)
PT (1) PT1133670E (ko)
SK (1) SK6552001A3 (ko)
WO (1) WO2000031497A1 (ko)
ZA (1) ZA200105211B (ko)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10038066B4 (de) * 2000-08-04 2004-07-08 Junghans Feinwerktechnik Gmbh & Co. Kg Aktivierbare Batterie für einen elektronischen Artilleriezünder
US6920826B2 (en) * 2000-09-15 2005-07-26 Junghans Feinwerktechnik Gmbh & Co. Kg Energy supply device having a shaft rotatably supported on a polytetrafluroethylene bearing surface
DE10045684C1 (de) * 2000-09-15 2002-06-13 Junghans Feinwerktechnik Gmbh Energieversorgungseinrichtung für eine durch ein Windrad aktivierbare Batterie o. dgl.
US6779457B2 (en) 2002-05-17 2004-08-24 Ruag Munition Percussion fuse (ignition device)
US7258068B2 (en) * 2003-06-30 2007-08-21 Kdi Precision Products, Inc. Safety and arming apparatus and method for a munition
FR2986613B1 (fr) 2012-02-08 2015-01-02 Mbda France Procede pour la levee d'une securite de mise a feu et projectile mettant en oeuvre ce procede
KR101408072B1 (ko) * 2013-01-31 2014-06-17 국방과학연구소 기어모터를 이용한 폭탄용 신관 안전장전장치 및 이를 구비한 기폭시스템
JP2018083604A (ja) * 2016-11-25 2018-05-31 計二 馬場 小型無人航空機の墜落に伴なう事故防止装置

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511872A (en) * 1950-06-20 Electric fuse
GB191308507A (en) * 1912-09-30 1913-11-06 Sprengstoff A G Carbonit Improvements in Bombs to be Dropped from Air Craft.
US2403567A (en) * 1942-01-13 1946-07-09 Jr Nathaniel B Wales Electrically energized fuse
US2900911A (en) * 1943-11-30 1959-08-25 Louis D Statham Fuze
US2989921A (en) * 1945-11-23 1961-06-27 Merrill G Leonard Control devices
US2775941A (en) * 1946-12-23 1957-01-01 Harold J Plumley Magnetic inertia controlled fuze
US2755737A (en) * 1947-11-25 1956-07-24 Allen S Clarke Rocket generator power supply
US2965035A (en) * 1948-05-14 1960-12-20 Robert O Wynn Impact nose fuze for a torpedo
US3757695A (en) * 1969-12-19 1973-09-11 Us Army Charging system for electric bomb fuzes (u)
US3680482A (en) * 1970-04-29 1972-08-01 Us Army Air current operated land mine
FR2633384A1 (fr) * 1988-06-28 1989-12-29 Thomson Brandt Armements Fusee electrique pour engins volants

Also Published As

Publication number Publication date
CZ20011842A3 (cs) 2002-06-12
ES2196896T3 (es) 2003-12-16
KR20010101054A (ko) 2001-11-14
ATE234456T1 (de) 2003-03-15
HUP0104087A2 (hu) 2002-03-28
NO20012576D0 (no) 2001-05-25
PL347826A1 (en) 2002-04-22
CZ292721B6 (cs) 2003-12-17
JP2002530626A (ja) 2002-09-17
IL143312A0 (en) 2002-04-21
SK6552001A3 (en) 2001-12-03
EP1133670A1 (de) 2001-09-19
HUP0104087A3 (en) 2002-04-29
CA2350585A1 (en) 2000-06-02
HU221930B1 (hu) 2003-02-28
ZA200105211B (en) 2002-05-08
US6481354B1 (en) 2002-11-19
DE59904566D1 (de) 2003-04-17
DE19854607A1 (de) 2000-05-31
WO2000031497A1 (de) 2000-06-02
DK1133670T3 (da) 2003-06-30
PT1133670E (pt) 2003-07-31
NO20012576L (no) 2001-05-25

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