EP1347262A2 - Antriebseinheit für grosskalibrige Munition - Google Patents
Antriebseinheit für grosskalibrige Munition Download PDFInfo
- Publication number
- EP1347262A2 EP1347262A2 EP03002493A EP03002493A EP1347262A2 EP 1347262 A2 EP1347262 A2 EP 1347262A2 EP 03002493 A EP03002493 A EP 03002493A EP 03002493 A EP03002493 A EP 03002493A EP 1347262 A2 EP1347262 A2 EP 1347262A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- cartridge
- propellant charge
- section
- sleeve
- 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
Links
- 239000003380 propellant Substances 0.000 title claims description 36
- 239000004429 Calibre Substances 0.000 title 1
- 239000004020 conductor Substances 0.000 claims abstract description 28
- 239000000700 radioactive tracer Substances 0.000 claims description 6
- 239000007789 gas Substances 0.000 claims 1
- 230000001681 protective effect Effects 0.000 description 11
- 239000000843 powder Substances 0.000 description 8
- 238000004026 adhesive bonding Methods 0.000 description 3
- 239000000428 dust Substances 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 238000000926 separation method Methods 0.000 description 3
- 239000011324 bead Substances 0.000 description 2
- 239000013013 elastic material Substances 0.000 description 2
- 230000003628 erosive effect Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 241000282373 Panthera pardus Species 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000004323 axial length Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009429 electrical wiring Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/18—Caseless ammunition; Cartridges having combustible cases
- F42B5/181—Caseless ammunition; Cartridges having combustible cases consisting of a combustible casing wall and a metal base; Connectors therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/0823—Primers or igniters for the initiation or the propellant charge in a cartridged ammunition
- F42C19/0826—Primers or igniters for the initiation or the propellant charge in a cartridged ammunition comprising an elongated perforated tube, i.e. flame tube, for the transmission of the initial energy to the propellant charge, e.g. used for artillery shells and kinetic energy penetrators
Definitions
- the invention relates to a cartridge with a cartridge case and a projectile, wherein in the cartridge case an extending in the direction of the longitudinal axis of the cartridge Propellant lighter and in the floor an electrically programmable projectile detonator are arranged and wherein the projectile detonator has at least one electrical line connected to an electrode arranged on the cartridge bottom is.
- a disadvantage of this known cartridge is, among other things, the complex protection of the spiral wound cable (large installation space) and the rigid connector, which is not a theoretically "infinite" revolution between the two conductor sections allows.
- the electrical line is very long, so that both final ballistic disturbances of the projectile as well as a danger to the tank personnel when the case is ejected after the ammunition has been fired. After all, one is time-consuming assembly of the electrical line through the floor-side opening the cartridge case required.
- DE 101 02 624 A1 describes a cartridge of the type mentioned at the beginning with a programmable projectile detonator known in the case of the propellant lighter a plug-type contact piece is attached on the front, which is connected via a first, in the propellant charge electrical conductor section with the the electrode located on the base of the cartridge is connected.
- the projectile side of the propellant lighter has a contact piece enclosing hood-shaped receptacle with at least one socket-shaped Contact via a second conductor section running in the floor is electrically conductively connected to the projectile fuse.
- To connect the two Conductor sections become the socket-shaped associated with this when assembling the projectile Contact piece on the plug-shaped assigned to the propellant charge lighter Pushed contact piece.
- a disadvantage of this cartridge is, among other things, that the manufacture of the plug and socket-shaped contacts is relatively expensive. In addition, one is on the tailgate supporting hood is required to accommodate the socket-shaped contact. Finally, there may be heavy loads when the projectile is installed come on the connector, so that the plug-shaped contact breaks off or the hood is bent.
- the present invention has for its object a cartridge of the beginning Specify the type mentioned, in which the between the cartridge bottom and the projectile fuse to be arranged electrical line can be introduced in a simple manner can and also with a large number of rotations of the projectile compared to the Cartridge bottom does not tear.
- the invention provides an at least two-piece cartridge case with at least one Separation point in the area between the front end of the propellant lighter and the tailgate.
- the sleeve sections floating merged so that through a remaining gap shortly before final assembly the short ends of the two conductor sections by means of a can be contacted in rotatable connector.
- at least one suitable one resilient element e.g. a spiral wound spring plate which is attached to a conductor section in an advantageous manner, is for the laboratory needed space created and at the same time ensured that with the sleeve sections connected conductor sections each have only a short length.
- the spring element pulls the electrical line into a protected one and fixed position back. The installation space remains so small that through a suitable hood (protective element) made of elastic material the connector is protected against erosion and powder dust.
- the invention can meet the requirements mentioned at the beginning of the signal line be fulfilled.
- Fig. 1, 1 denotes a cartridge which has a cartridge base 2, a cartridge case 3 and a wing-stabilized projectile 4 with a programmable detonator includes whose tip-side part protruding from the cartridge case 3 is not shown is.
- the cartridge case 3 is composed of two axially one behind the other and together connectable sleeve sections 5, 6 together.
- first sleeve section 5 connected to the cartridge base 2 and extends to the front end 7 of a propellant charge lighter 8 connected to the cartridge base 2.
- the second sleeve section 6 is connected to the floor 4.
- the rear area 9 of the projectile 4 extends into the vicinity of the first sleeve section 5 facing end of the second sleeve section 6. In the rear area 9th there is a tracer 10 on the floor.
- the first ladder section 11 can outside of the propellant charge lighter 8 under or over: one possibly existing shrink tubing along.
- the conductor section 11 preferably ends in a center as possible Position.
- the end of the first conductor section 11 is socket-shaped Part 12 of a smooth first rotatable, preferably angled at an angle Provide connector 13.
- the powder grains 14 of the propellant powder in the first sleeve section 5 with a cover 15, preferably made of Silk gauze to cover.
- undesirable graphite dust is 7 of the propellant charge lighter 8 a hood-shaped receptacle (protective sleeve) 16 attached.
- the protective sleeve 16 should preferably consist of an elastic material, such as. Rubber or foam. This makes the axial and radial movements the tail unit 17 of the wing-stabilized projectile 4 in relation to the propellant lighter 8 (e.g. with environmental pollution such as vibration and falling pollution) added, without losing the sealing function. Burnable is also conceivable Material that has little elasticity and the relative movements within the cartridge case 3 can only compensate with difficulty.
- the attachment of the protective sleeve 16 to the propellant charge lighter 8 can e.g. by gluing or, as indicated in Figures 1 and 3, by a positive connection be created.
- the positive connection is through one circumferential bead 18 realized as a slip barrier.
- the protective sleeve 16 has in this Case a corresponding circumferential groove 19 on the inner diameter.
- a combination from the types of fastening (form locking and gluing) is also conceivable.
- the protective sleeve 16 is designed so that it the electrical line 110 and the others components in the grommet area after the laboratory work encloses.
- the axial length of the protective sleeve 16 is dimensioned such that that it is under axial pressure after the laboratory, to the inevitably existing Compensate length tolerances in the cartridge 1 and around a good and relative to ensure a tight fit at the tail end 20.
- second conductor section 21 of the electrical line 110 in or on the tail unit 17 along and is also with a sleeve-shaped part 22 of a second rotatable connector 23 connected.
- the second conductor section 21 is connected to the tail unit by means of a spring plate 24 17 pressed.
- the spring plate 24 is fixed on one side so that it is due to its elasticity lifting the second conductor section 21 in the direction of the propellant charge lighter 8 permits. This allows a laboratory gap 25 for the introduction of tools be handled generously.
- the spring plate 24th circular, such that the outlet opening 26 of the tracer set 10th remains free.
- the connector should be preferred be arranged axially.
- the first sleeve section 5 is suspended while being labored.
- the Lid 15 prevents the propellant powder already filled from escaping. All the necessary components on the propellant lighter 8 are already before the laboratory been assembled.
- the first sleeve section 5 is so far on the vertical and with the first Sleeve section 5 aligned second sleeve section 6 lowered that there is still a sufficient laboratory gap 25.
- the second is in this position Sleeve section 6 already filled with powder.
- the second conductor section 21 is already connected to the spring plate 24.
- the last step in the laboratory is to connect the first to the second sleeve section 5, 6 e.g. by gluing.
- the conductor sections 11, 21, 28 through the spring plate 24 so led that they remain within the space required for the protective sleeve 16 and the protective sleeve 16 is undisturbed under pressure against the tail unit 17 or the floor can put on (Fig. 3).
- the cartridge 1 is essentially finished.
- the ladder sections 11 and 21 are connected to each other, the spring plate 24 is in the rest position and holds the second connector 23 in place. Now turn Tail 17 (and thus the floor 4) and the cartridge floor 2 with the propellant lighter 8 in the opposite direction, the electrical conductor sections 11 and 21 turn without twisting.
- the invention is of course not based on the embodiment described above limited.
- a second rotatable connector to be dispensed with can be dispensed with.
- the spring plate can be dispensed with entirely if the distance between TLAnz and tail unit is due to skillful laboratory work, z. B. "crooked" insertion of the TL sleeves, kept low in the laboratory can be. In this case, the plug connection (on the tail side) would be directly in the tail unit be arranged.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Details Of Connecting Devices For Male And Female Coupling (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Connector Housings Or Holding Contact Members (AREA)
- Air Bags (AREA)
Abstract
Description
- geringe Kosten/geringer Aufwand;
- Laborierfähigkeit;
- einwandfreie Daten- und Energieübertragung;
- Verdrehbarkeit des elektrischen Leiters;
- Vermeidung axialer oder radialer Kräfte auf den Treibladungsanzünder;
- elastische Aufnahme axialer oder radialer Verschiebungen;
- EMV-Standfest;
- Vermeidung langer Kabelreste nach Schußabgabe am Treibladungsanzünder und damit Gewährleistung einer ausreichenden Sicherheit der Besatzung;
- Vermeidung langer Kabelreste nach Trennung am Leitwerk und damit Vermeidung außenballistischer Störungen;
- Schutz der elektrischen Leitung vor Pulverstäuben;
- Vermeidung von Kabelrückständen im Waffenrohr.
- 1
- Patrone
- 2
- Patronenboden
- 3
- Patronenhülse
- 4
- Geschoß
- 5
- (erster) Hülsenabschnitt
- 6
- (zweiter) Hülsenabschnitt
- 7
- vordere Ende (Treibladungsanzünder)
- 8
- Treibladungsanzünder
- 9
- heckseitiger Bereich (Geschoß), Geschoßheck
- 10
- Leuchtspursatz
- 11
- (erster) Leiterabschnitt
- 110
- elektrische Leitung
- 12
- buchsenförmiger Teil
- 13
- erste (drehbare) Steckverbindung
- 14
- Pulverkorn
- 15
- Deckel
- 16
- Aufnahme, Schutztülle
- 17
- Leitwerk
- 18
- Wulst
- 19
- Nut
- 20
- Leitwerksende
- 21
- (zweiter) Leiterabschnitt
- 22
- buchsenförmiger Teil
- 23
- zweite (drehbare) Steckverbindung
- 24
- Federblech, federndes Element
- 25
- Laborierspalt
- 26
- Austrittsöffnung
- 27
- Blechnase
- 28
- (dritter) Leiterabschnitt
Claims (7)
- Patrone mit einer Patronenhülse (3) und einem Geschoß (4), wobei in der Patronenhülse (3) ein sich in Richtung der Längsachse der Patrone (1) erstreckender Treibladungsanzünder (8) und in dem Geschoß (4) ein elektrisch programmierbarer Geschoßzünder angeordnet sind und wobei der Geschoßzünder über mindestens eine elektrische Leitung (110) mit einer am Patronenboden (2) angeordneten Elektrode verbunden ist, mit den Merkmalen:a) die Patronenhülse (3) besteht aus mindestens zwei axial hintereinander angeordneten und miteinander verbundenen Hülsenabschnitten (5, 6), wobei der erste Hülsenabschnitt (5) mit dem Patronenboden (2) verbunden ist und sich bis zum vorderen Ende (7) des Treibladungsanzünders (8) erstreckt und der zweite Hülsenabschnitt (6) mit dem Geschoß (4) verbunden ist, dessen heckseitiger Bereich (9) sich bis in die Nähe des dem ersten Hülsenabschnitt (5) zugewandten Endes des zweiten Hülsenabschnittes (6) erstreckt;b) die elektrische Leitung (110) weist im Bereich zwischen dem vorderen Ende (7) des Treibladungsanzünders (8) und dem Geschoßheck (9) eine erste drehbare Steckverbindung (13) auf, so daß der mit in oder an dem Treibladungsanzünder (8) angeordnete erste Leiterabschnitt (11) der elektrischen Leitung (110) gegenüber dem an dem Geschoß (4) angeordneten zweiten Leiterabschnitt (21) verdrehbar ist;c) an dem Geschoßheck (9) ist ein federndes Element (24) angeordnet, welches auf den zweiten Leiterabschnitt (21) wirkt und diesen mit einer vorgegebenen Kraft zum Geschoßheck (9) hin zieht.
- Patrone nach Anspruch 2, dadurch gekennzeichnet, daß an dem vorderen Ende (7) des Treibladungsanzünders (8) eine erste drehbare Steckverbindung (13) sowie im Bereich des federnden Elementes (24) eine zweite drehbare Steckverbindung (23) angeordnet ist und daß zwischen den beiden drehbaren Steckverbindungen (13, 23) ein steifer dritter Leiterabschnitt (28) vorgesehen ist.
- Patrone nach Anspruch 2, dadurch gekennzeichnet, daß die erste Steckverbindung (13) leichter drehbar ausgebildet ist als die zweite Steckverbindung (23).
- Patrone nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß es sich bei dem federnden Element (24) um ein Federblech handelt.
- Patrone nach Anspruch 4, dadurch gekennzeichnet, daß das Federblech (24) kreisförmig oder kreisabschnittförmig ausgebildet ist, derart, daß es bei einem Geschoß (4) mit Leuchtspursatz (10) die entsprechende Austrittsöffnung (26) der brennenden Gase freiläßt.
- Patrone nach Anspruch 2 und 5, dadurch gekennzeichnet, daß die zweite drehbare Steckverbindung (23) seitlich von dem Leuchtspursatz (10) des Geschosses (4) angeordnet ist.
- Patrone nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, daß an dem vorderen Ende (7) des Treibladungsanzünders (8) eine haubenförmige Aufnahme (16) vorgesehen ist, welche sich vorderseitig an dem Geschoßheck (9) abstützt und den zwischen dem Treibladungsanzünder (8) und dem Geschoßheck (9) befindlichen Leiterabschnitt der elektrischen Leitung (110) einschließlich der drehbaren Steckverbindung(en) (13, 23) umschließt.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10213098 | 2002-03-23 | ||
DE10213098 | 2002-03-23 | ||
DE10248697A DE10248697A1 (de) | 2002-03-23 | 2002-10-18 | Patrone |
DE10248697 | 2002-10-18 |
Publications (4)
Publication Number | Publication Date |
---|---|
EP1347262A2 true EP1347262A2 (de) | 2003-09-24 |
EP1347262A3 EP1347262A3 (de) | 2005-04-27 |
EP1347262B1 EP1347262B1 (de) | 2008-10-01 |
EP1347262B8 EP1347262B8 (de) | 2008-11-19 |
Family
ID=27789751
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP03002493A Expired - Lifetime EP1347262B8 (de) | 2002-03-23 | 2003-02-06 | Antriebseinheit für grosskalibrige Munition |
Country Status (4)
Country | Link |
---|---|
US (1) | US6725781B2 (de) |
EP (1) | EP1347262B8 (de) |
DE (2) | DE10248697A1 (de) |
ES (1) | ES2310628T3 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2038603A2 (de) * | 2006-07-10 | 2009-03-25 | Raytheon Company | Verfahren und vorrichtung für ein projektil-datenverknüpfungssystem |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005010125A1 (de) * | 2005-03-02 | 2006-09-07 | Rheinmetall Waffe Munition Gmbh | Munition, insbesondere programmierbare großkalibrige Munition |
US8146502B2 (en) | 2006-01-06 | 2012-04-03 | Armtec Defense Products Co. | Combustible cartridge cased ammunition assembly |
CA2652642C (en) * | 2006-02-09 | 2015-12-08 | General Dynamics Ordnance And Tactical Systems - Canada Valleyfield Inc. | Black powder substitutes for small caliber firearms |
US8042470B2 (en) * | 2006-02-09 | 2011-10-25 | Stephan Dietrich | Remote setting for electronic systems in a projectile for chambered ammunition |
US7913625B2 (en) * | 2006-04-07 | 2011-03-29 | Armtec Defense Products Co. | Ammunition assembly with alternate load path |
US7984676B1 (en) | 2007-06-29 | 2011-07-26 | Taser International, Inc. | Systems and methods for a rear anchored projectile |
DE102007039532B4 (de) * | 2007-08-21 | 2021-03-18 | Rheinmetall Waffe Munition Gmbh | Patrone |
US8166881B2 (en) * | 2008-12-17 | 2012-05-01 | Stephan Dietrich | Remote setting for electronic systems in a projectile for chambered ammunition |
US9009163B2 (en) | 2009-12-08 | 2015-04-14 | Intellectual Ventures Fund 83 Llc | Lazy evaluation of semantic indexing |
US8774528B2 (en) | 2010-09-24 | 2014-07-08 | Kodak Alaris Inc. | Method of selecting important digital images |
EP3980713A1 (de) * | 2019-06-07 | 2022-04-13 | Rabuffo SA | Munitionspatrone mit einem rohr zur übertragung der anfangsenergie auf die treibladung |
US11912231B2 (en) | 2020-10-27 | 2024-02-27 | Arc Technology Holding Limited | Inflator with open center generant holder |
US11988491B1 (en) * | 2021-07-29 | 2024-05-21 | Revolutionary Rounds L.L.C. | Projectile and caseless cartridge |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10052741A1 (de) | 2000-10-25 | 2002-05-08 | Rheinmetall W & M Gmbh | Patrone |
DE10102624A1 (de) | 2001-01-20 | 2002-07-25 | Rheinmetall W & M Gmbh | Patrone |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4033266A (en) * | 1975-01-31 | 1977-07-05 | General Electric Company | Electrical fuze with selectable modes of operation |
DE3507758C2 (de) * | 1985-03-05 | 1987-03-26 | Obisco Textil Trading & Consulting S.A., Küsnacht | Handfeuerwaffe und Schrotmunition hierfür |
DE3716450C1 (en) * | 1987-05-16 | 1990-05-17 | Rheinmetall Gmbh | Setting electronic timer for munition detonator - entering type, temp. of drive charge weather and target data in fuse ignition computer |
US4887534A (en) * | 1988-06-10 | 1989-12-19 | Honeywell Inc. | Ignition system for high intrusion projectile |
DE58901599D1 (de) * | 1988-10-21 | 1992-07-09 | Rheinmetall Gmbh | Vorrichtung zur zuendereinstellung. |
DE4102287C2 (de) * | 1991-01-26 | 1999-10-21 | Diehl Stiftung & Co | Munition |
US5078051A (en) * | 1991-02-14 | 1992-01-07 | Alliant Techsystems Inc. | Ammunition data transmission system |
US5097765A (en) * | 1991-03-28 | 1992-03-24 | The United States Of America As Represented By The Secretary Of The Army | Electric fuze with selectable modes |
US5485788A (en) * | 1994-09-27 | 1996-01-23 | Hughes Missile Systems Company | Combination explosive primer and electro-explosive device |
-
2002
- 2002-10-18 DE DE10248697A patent/DE10248697A1/de not_active Withdrawn
-
2003
- 2003-02-06 EP EP03002493A patent/EP1347262B8/de not_active Expired - Lifetime
- 2003-02-06 ES ES03002493T patent/ES2310628T3/es not_active Expired - Lifetime
- 2003-02-06 DE DE50310560T patent/DE50310560D1/de not_active Expired - Lifetime
- 2003-03-24 US US10/394,581 patent/US6725781B2/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10052741A1 (de) | 2000-10-25 | 2002-05-08 | Rheinmetall W & M Gmbh | Patrone |
DE10102624A1 (de) | 2001-01-20 | 2002-07-25 | Rheinmetall W & M Gmbh | Patrone |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2038603A2 (de) * | 2006-07-10 | 2009-03-25 | Raytheon Company | Verfahren und vorrichtung für ein projektil-datenverknüpfungssystem |
EP2038603A4 (de) * | 2006-07-10 | 2013-05-01 | Raytheon Co | Verfahren und vorrichtung für ein projektil-datenverknüpfungssystem |
Also Published As
Publication number | Publication date |
---|---|
EP1347262B1 (de) | 2008-10-01 |
ES2310628T3 (es) | 2009-01-16 |
DE50310560D1 (de) | 2008-11-13 |
EP1347262A3 (de) | 2005-04-27 |
US20040003746A1 (en) | 2004-01-08 |
US6725781B2 (en) | 2004-04-27 |
EP1347262B8 (de) | 2008-11-19 |
DE10248697A1 (de) | 2003-10-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
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