EP1133670B1 - Mörserzünder mit einem windrad - Google Patents
Mörserzünder mit einem windrad Download PDFInfo
- 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
Links
- 239000004570 mortar (masonry) Substances 0.000 title claims abstract description 18
- 230000004913 activation Effects 0.000 claims abstract description 17
- 239000002253 acid Substances 0.000 claims abstract description 14
- 239000003990 capacitor Substances 0.000 claims description 7
- 230000003213 activating effect Effects 0.000 claims 7
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 abstract 1
- 239000000696 magnetic material Substances 0.000 abstract 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000007420 reactivation 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
- F42C15/295—Arming-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
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/21—Rotors for wind turbines
- F05B2240/211—Rotors 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
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Wind Motors (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Vaporization, Distillation, Condensation, Sublimation, And Cold Traps (AREA)
- Fuses (AREA)
- Toys (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)
- Preparation Of Clay, And Manufacture Of Mixtures Containing Clay Or Cement (AREA)
- Manufacturing Of Micro-Capsules (AREA)
- Agricultural Chemicals And Associated Chemicals (AREA)
- Road Signs Or Road Markings (AREA)
- External Artificial Organs (AREA)
- Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
- Air Bags (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Medicines Containing Plant Substances (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Battery Mounting, Suspending (AREA)
Description
- Fig. 1
- ein erstes Ausführungsbeispiel der Erfindung,
- Fig. 2
- ein zweites Ausführungsbeispiel der Erfindung,
- Fig. 3
- ein Blockschaltbild einer Notstromversorgung.
Claims (6)
- Mörserzünder mit einem Windrad (1), einer aktivierbaren Batterie (2), welche durch ein von dem Windrad (1) angetriebenes Aktivierungsrad (11) in Funktion bringbar ist,
das Aktivierungsrad (11) in Funktion bringbar ist,
das Aktivierungsrad (11) längs eines Schneckenganges (10) des drehenden Windrades (1) verschiebbar und in Kontakt mit der aktivierbaren Baüerie (2) bringbar ist,
dadurch gekennzeichnet, daß das Aktivierungsrad (11) einen Magneten (13) aufweist, der bei dessen Drehung an einer Spule (12) vorbeiläuft und darin Energie erzeugt. - Mörserzünder nach Anspruch 1,
dadurch gekennzeichnet, daß die aktivierbaren Batterie (2) aus einem Batteriebehälter (6) mit den Batteriezellen (7) und einem unmittelbar benachbarten, jedoch davon getrennten Säurebehälter (8) besteht, welch letzterer durch das Aktivierungsrad (11) anstechbar ist, wodurch Säure in den Batteriebehälter (6) fließt. - Mörserzünder nach Anspruch 1,
dadruch gekennzeichnet, daß ein Sicherungsbolzen (16) durch das drehende Windrad (1) aus der Sicherungsposition herausbewegt wird und die Sicherungseinrichtung (3, 3a, 3b) freigibt. - Mörserzünder nach Anspruch 1,
dadurch gekennzeichnet, daß die Energie, die das Aktivierungsrad (11) erzeugt, zur Stromversorgung des Zünders während der Aktivierungsphase der Batterie (2) und insbesondere zur Energieversorgung für einen Zähler (21) dienen, der die Zeitfunktion des Zünders steuert - Mörserzünder nach Anspruch 4,
dadurch gekennzeichnet, daß eine, einen oder mehrere Kondensatoren (18, 20) enthaltende Notstromversorgung. vorgesehen ist, welche mit dem Aktivierungsrad (11) zusammenarbeitet und die Funktion des Zählers (21) bei einem etwaigen Stromausfall der Batterie oder eines Windradgenerators sicherstellt. - Mörserzünder nach Anspruch 1,
dadurch gekennzeichnet, daß ein Doppelbolzen (14) als Auslöser für das Windrad (1) vorgesehen ist.
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 (de) |
EP (1) | EP1133670B1 (de) |
JP (1) | JP2002530626A (de) |
KR (1) | KR20010101054A (de) |
AT (1) | ATE234456T1 (de) |
CA (1) | CA2350585A1 (de) |
CZ (1) | CZ292721B6 (de) |
DE (2) | DE19854607A1 (de) |
DK (1) | DK1133670T3 (de) |
ES (1) | ES2196896T3 (de) |
HU (1) | HU221930B1 (de) |
IL (1) | IL143312A0 (de) |
NO (1) | NO20012576D0 (de) |
PL (1) | PL347826A1 (de) |
PT (1) | PT1133670E (de) |
SK (1) | SK6552001A3 (de) |
WO (1) | WO2000031497A1 (de) |
ZA (1) | ZA200105211B (de) |
Families Citing this family (8)
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)
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 |
-
1998
- 1998-11-26 DE DE19854607A patent/DE19854607A1/de not_active Withdrawn
-
1999
- 1999-11-26 HU HU0104087A patent/HU221930B1/hu not_active IP Right Cessation
- 1999-11-26 DE DE59904566T patent/DE59904566D1/de not_active Expired - Fee Related
- 1999-11-26 SK SK655-2001A patent/SK6552001A3/sk unknown
- 1999-11-26 EP EP99961015A patent/EP1133670B1/de not_active Expired - Lifetime
- 1999-11-26 PL PL99347826A patent/PL347826A1/xx unknown
- 1999-11-26 CA CA002350585A patent/CA2350585A1/en not_active Abandoned
- 1999-11-26 KR KR1020017006464A patent/KR20010101054A/ko active IP Right Grant
- 1999-11-26 IL IL14331299A patent/IL143312A0/xx unknown
- 1999-11-26 US US09/856,619 patent/US6481354B1/en not_active Expired - Fee Related
- 1999-11-26 PT PT99961015T patent/PT1133670E/pt unknown
- 1999-11-26 JP JP2000584265A patent/JP2002530626A/ja not_active Withdrawn
- 1999-11-26 ES ES99961015T patent/ES2196896T3/es not_active Expired - Lifetime
- 1999-11-26 CZ CZ20011842A patent/CZ292721B6/cs not_active IP Right Cessation
- 1999-11-26 AT AT99961015T patent/ATE234456T1/de not_active IP Right Cessation
- 1999-11-26 DK DK99961015T patent/DK1133670T3/da active
- 1999-11-26 WO PCT/EP1999/009195 patent/WO2000031497A1/de active IP Right Grant
-
2001
- 2001-05-25 NO NO20012576A patent/NO20012576D0/no unknown
- 2001-06-25 ZA ZA200105211A patent/ZA200105211B/en unknown
Also Published As
Publication number | Publication date |
---|---|
CZ20011842A3 (cs) | 2002-06-12 |
CZ292721B6 (cs) | 2003-12-17 |
NO20012576L (no) | 2001-05-25 |
KR20010101054A (ko) | 2001-11-14 |
PL347826A1 (en) | 2002-04-22 |
HUP0104087A2 (hu) | 2002-03-28 |
ATE234456T1 (de) | 2003-03-15 |
DK1133670T3 (da) | 2003-06-30 |
JP2002530626A (ja) | 2002-09-17 |
NO20012576D0 (no) | 2001-05-25 |
DE59904566D1 (de) | 2003-04-17 |
HUP0104087A3 (en) | 2002-04-29 |
EP1133670A1 (de) | 2001-09-19 |
HU221930B1 (hu) | 2003-02-28 |
ZA200105211B (en) | 2002-05-08 |
ES2196896T3 (es) | 2003-12-16 |
IL143312A0 (en) | 2002-04-21 |
CA2350585A1 (en) | 2000-06-02 |
PT1133670E (pt) | 2003-07-31 |
WO2000031497A1 (de) | 2000-06-02 |
US6481354B1 (en) | 2002-11-19 |
SK6552001A3 (en) | 2001-12-03 |
DE19854607A1 (de) | 2000-05-31 |
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