EP2157398A2 - Lanceur de contre-mesures - Google Patents

Lanceur de contre-mesures Download PDF

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Publication number
EP2157398A2
EP2157398A2 EP09167816A EP09167816A EP2157398A2 EP 2157398 A2 EP2157398 A2 EP 2157398A2 EP 09167816 A EP09167816 A EP 09167816A EP 09167816 A EP09167816 A EP 09167816A EP 2157398 A2 EP2157398 A2 EP 2157398A2
Authority
EP
European Patent Office
Prior art keywords
axis
counter
unit
abschusseinheit
elevation
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
EP09167816A
Other languages
German (de)
English (en)
Other versions
EP2157398A3 (fr
EP2157398B1 (fr
Inventor
Jens Grünewald
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.)
KNDS Deutschland GmbH and Co KG
Original Assignee
Krauss Maffei Wegmann GmbH and Co KG
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
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First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=41056955&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP2157398(A2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of EP2157398A2 publication Critical patent/EP2157398A2/fr
Publication of EP2157398A3 publication Critical patent/EP2157398A3/fr
Application granted granted Critical
Publication of EP2157398B1 publication Critical patent/EP2157398B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00—Defence installations; Defence devices
    • F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
    • F41A23/24—Turret gun mountings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/06—Mechanical systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
    • F41F1/08—Multibarrel guns, e.g. twin guns

Definitions

  • the invention relates to a counter-fire system according to the preamble of patent claim 1.
  • Counter-shot systems are used to protect objects such as vehicles, ships, helicopters or buildings by repelling enemy missiles.
  • counter-firing systems In order to detect missiles approaching the object, counter-firing systems have sensor units which detect the opposing missile, for example a rocket, and possibly anticipate its further trajectory via a suitable evaluation unit.
  • the missile Shortly before the anticipated impact, the missile is fired fully automatically in the vicinity of the object via a launching unit, which is brought into an appropriate alignment with the missile for this purpose.
  • the launching unit is pivotally mounted about two axes, a so-called azimuth and elevation axis, one axis of which is substantially vertical and the other axis is substantially horizontal.
  • the azimuth angle and the elevation angle of the launching unit can be adjusted independently of each other.
  • the movement of the launching unit about one axis does not affect its angular position with respect to the other axis. It is not necessary to make a compensation for achieving the desired angular position on a complex electronics.
  • the pivoting movements of the rotary element about the azimuth axis are decoupled from those of the launching unit about the elevation axis via a decoupling element.
  • a further embodiment provides that a first drive for the pivoting movements about the azimuth axis and a second drive for the pivoting movements about the elevation axis is provided.
  • both the first and the second drive are arranged fixed to the object.
  • the two drives are arranged on the mounting element.
  • the object-fixed arrangement reduces the number of components to be pivoted of the counter-shot system, whereby the mass of the components to be moved and thus the response time of the counter-shot system, i. the time that elapses before an enemy missile is attacked is also reduced.
  • this embodiment is also advantageous in terms of the electrical wiring of the drives, since they do not have to follow the pivoting movements of the rotary member.
  • the first drive connected via the decoupling element with the Abschussü is.
  • the connection via the decoupling element allows a kind of rotary coupling between the first drive and arranged on the rotary element Abschussechen.
  • the Abschussüen can be elevated, on the other hand, rotational movements of the rotary member or straightening the Abschussappelen in the azimuthal direction without affecting the first drive or the elevation angle of the Abschussappelen remains.
  • the decoupling element is arranged in a rotationally fixed manner with the rotary element.
  • the sensor unit is arranged on the rotary element.
  • the sensor unit occupies the same rotational position as the rotary element or the Abschussech so that it is in a certain pre-alignment to a detected missile.
  • the sensor unit arranged on the rotary element can in particular be a so-called tracking sensor, which senses the trajectory of the missile via a comparatively narrow radar lobe.
  • additional sensors can be provided on the object, which monitor the airspace over a large area.
  • the sensor unit is pivotally coupled to the Abschussü, whereby it always assumes the pivot angle of the Abschussü. If the sensor unit makes up a hostile missile at a certain pivoting angle, the launching unit is also in this pivoting position, as a result of which it is already in a pre-alignment with the enemy missile. This results in a short response time of the counter-shot system.
  • the azimuth axis intersect the elevation axis, resulting in a symmetrical arrangement with advantageous derivation of the launch reaction forces occurring upon actuation of the launching unit.
  • a rapid alignment of the counter-shot system it is beneficial if the azimuth axis passes through the center of gravity of the rotatable about the azimuth axis components, which reduces the mass moment of inertia to be overcome and with this the response time of the system.
  • the Abschussech has a launch tube whose tube axis intersects the elevation axis, resulting in a favorable, torque-neutral initiation of the launch reaction forces upon actuation of the Abschuss nie.
  • Fig. 1 shows by way of example the use of two inventive counter-shot systems 2 on a military vehicle 1.
  • the invention is not limited to an application in military vehicles, but can equally be used for example in buildings, ships, helicopters and so on.
  • military vehicle 1 is an armored vehicle in the rear area for the purpose of defense against enemy missiles, such as rockets, artillery or Mortar rounds, equipped with two identical counter-shot 2.
  • enemy missiles such as rockets, artillery or Mortar rounds
  • two counter-shot systems 2 opposing missiles approaching from both sides of the vehicle can be detected and fired fully automatically in the vicinity of the vehicle. This results in all-round protection for the combat vehicle 1.
  • the counter-shot system 2 is composed of a retaining element 3 fixed to the vehicle 1, for example by screwing or welding, and a rotary element 4 rotatable about a vertical axis relative to the retaining element 3.
  • the holding element 3 is designed in the manner of a mounting element for fixing to an outer wall of the vehicle and has a fitting to the vehicle outer contour back plate 3.1, which is provided for reasons of weight and material savings with recesses 3.2.
  • the back plate 3.1 In the region of the upper and the lower end of the back plate 3.1 it is provided with approximately triangular cross sheets 3.3, which are provided with recesses 3.4, a rim 3.6 and a passage opening 3.5 for the introduction of a bearing pin 4.1 of the rotary member 4.
  • the transverse plates 3.3 close with the back plate 3.1 in about a right angle and are firmly connected to this, for example by screwing, riveting or welding.
  • the rotary member 4 is of a total frame-shaped shape and has longer side walls 4.2 and connecting these transverse walls 4.3. Above the transverse walls 4.3 is a tubular, concentric to the azimuth axis A A extending bolt 4.1 after Provided type of stub axle, which extends into the opening 3.5 and passes through this.
  • launching units 6, 7 are provided one above the other in the intermediate space between the two side walls 4.2 of the rotary element 4, each having two launch tubes 8 arranged parallel to one another.
  • a radar-based sensor unit 5 is provided above the firing units 6, 7 .
  • the sensor unit 5 is a tracking sensor. Further sensors 23 are fixed to the vehicle on the roof of the vehicle.
  • a first electric motor drive 10 is provided for the movement of the rotary member 4 about the azimuth axis A A .
  • a second electromotive drive 20 is provided for the movement of the rotary member 4 about the azimuth axis A A . Both drives 10, 20 are arranged fixed to the object, so that they do not follow the rotational movements of the rotary member 4.
  • FIG. 3 The counter-shot system 2 is shown in a position in which the sensor unit 5 and the two launching units 6, 7 take an elevation angle ⁇ 1 of about - 10 ° relative to the horizontal. This is the lower end position in which the Abschussechen 6, 7 are pivoted by 10 ° relative to the horizontal downwards.
  • the sensor unit 5 and the Abschussstatten 6, 7 in the region of one end of their elevation axes A ES and A EA provided with gears 9, via which the elevation angle of the sensor unit 5 and the launching units 6, 7th can be set.
  • a common transmission element 11 is provided, which converts the drive movement generated by the drive 10 via the gears 9 in concurrent pivotal movements of the sensor element 5 and the Abschussechen 6, 7.
  • transmission element 11 is a rack, which is provided in its the gears 9 opposite longitudinal sections with a toothing, which meshes with the gears 9 over the entire travel of the rack 11.
  • the use of a rack 11 is to achieve a rectified pivotal movement of the sensor unit 5 with the launching units 6, 7 is not mandatory. It is also conceivable to use linkage couplings, toothed belts, transmission via further gear wheels or transmission via an electric or electronic control or else the use of direct drives on the respective axes A ES or A EA . Also, it is not necessary that the counter-shot system is provided with two launching units 6, 7. Also conceivable are solutions with more or fewer launching units, even with one or more launching tubes 8.
  • Fig. 3 the rack 11 is shown in its upper end position, in which the elevation angle ⁇ 1 is minimal.
  • Fig. 4 is the rack 11 in contrast a piece moved down, causing the gears 9 in the view according to Fig. 3 respectively.
  • Fig. 4 be rotated counterclockwise. With the gears 9 and the associated with these launch units 6, 7 and the sensor unit 5 in an elevation angle position ⁇ 2 of about 45 ° are pivoted.
  • the drive 10 is an electric motor which is connected via a belt 12 to a recirculating ball nut 13 formed on the circumference as a pulley in the lower end region of the rotary element 4. Details can be found in the detailed presentation in Fig. 6 remove.
  • the ball nut 13 is arranged such that this rotational movement is not transmitted to the rotary member 4.
  • the ball nut 13 is seated in an opening of the rotary member 4 and is formed such that rotations of the rotary member 4 are not transmitted to the ball screw nut 13 and vice versa.
  • a spindle 14 arranged inside the ball nut 13 is moved axially in the vertical direction.
  • the spindle 14 is axially coupled to the transmission element 11 and can only be axially reciprocated.
  • Rotary movements of the spindle 14 are blocked via torque arm, for example, by a provided on the spindle 14 Bolt which is guided in a provided on the holding element 3 slot.
  • the first drive 10 is connected via the spindle 14 and a decoupling element 15, which is formed in the embodiment of a hollow cylinder, with the rack 11.
  • the decoupling element 15 is designed such that the rack 11 follows the axial movements of the spindle 14, but at the same time rotational movements of the rotary member 4 are not transmitted to the spindle 14.
  • the decoupling element 15 has a circumferential collar 15.1, which is rotatable but axially immovable, in a circumferential groove 14.1 of the spindle 14. In this way, the rotational movement of the drive 10 is transferred via the decoupling element 15 in a translational movement of the rack 11, which is independent of the rotational position of the rotary member 4.
  • Fig. 5 shown is the lower end position of the transmission element 11, in which also the spindle 14 of the ball nut 13 is in its lower end position and the elevation angle ⁇ 3 has reached its maximum.
  • the elevation angle ⁇ 3 is approximately 60 °.
  • a separate drive 20 is provided, see. also the representation in Fig. 2 ,
  • the drive shaft of the drive 20 is provided with a pinion 17, which meshes with a fixed to the rotary member 4 gear 18 of larger diameter, which is why the motor 20 when energized, the rotary member 4 according to the transmission ratio of the gears 17, 18 about the azimuth axis A A drives, see. also Fig. 9 ,
  • This rotational movement is not transmitted to the spindle 14 and thus not to the drive 10 via the decoupling element 15 arranged on the rotary element 4.
  • the collar 15.1 of the decoupling element 15 rotates within the groove 14.1 of the spindle 14, without this being moved.
  • FIGS. 7 and 8 the counter-shot unit 2 is shown in further views that show the arrangement of the axes and motors of the system.
  • the drives 10 and 20 are arranged laterally of the holding element 3 in a vehicle-fixed, not pivotable together with the rotary member 4 position. It can be seen that the vertically extending azimuth axis A A intersects all of the horizontally extending elevation axes A ES and A EA at a right angle.
  • the reference symbol S denotes the center of gravity of the rotary element 4, including the components connected thereto, such as the launching units 6, 7 and the sensor unit 5. It can be seen that the azimuth axis A A passes through the center of gravity S, which gives a short response time.
  • the counter-shot system can be aligned within a period of about 100ms, so that missiles in the vicinity of the vehicle can be detected and shot within this period, even in the closest vicinity, such as at distances of 10m to 100m to the vehicle.
  • the illustration can be in Fig. 8 can be seen that the cup-like discharge tubes 8 of the launching units 6, 7 are arranged symmetrically to both sides near the azimuth axis A A , resulting in favorable launching reactions.
  • the representation in Fig. 9 shows that the tube axes A R of the launch tubes 8 intersect the elevation axes A EA at right angles.
  • the execution according to Fig. 9 also shows a special feature to the previously based on the representations in the FIGS. 3 to 5 described embodiments.
  • a gear segment 16 is provided, which, however, meshes with the toothed portions over the entire axial travel of the rack 11. The use of toothed segments 16 results in a low mass of the components to be moved.
  • a second embodiment of a counter-shot system 2 is shown, which is mounted on the vehicle roof.
  • the rotary member 4 can perform a full 360 ° rotation about the azimuth axis A A , which is why in this embodiment, a single counter-shot system 2 is sufficient for all-round protection of the vehicle.
  • the counter-shot system 2 is provided on the underside with a turntable 21 which is fixedly connected to the vehicle roof and insofar forms a retaining element 3.
  • the rotary member 4 is formed in this embodiment by a two side walls 4.2, above the plate-shaped support member 3 arranged element between the side walls 4.2, the sensor unit 5 and the two launch elements 6, 7 are pivotally received about their respective elevation axes A ES and A EA ,
  • an electric motor drive 10 which is provided in the region of the rotary member 4 together with this rotating.
  • About the drive 10 is connected via a belt 19th the rotational movement of the drive 10 in a pivoting movement of the lower Abschussech 7 about the elevation axis A EA transferred.
  • This pivoting movement about the elevation axis A EA is transmitted by means of a transmission element 22, which is embodied only in a very schematically illustrated manner, which in the case of this embodiment is designed in the manner of a linkage, such that, as shown in FIGS. 13 and 14 let it be seen that the elevation angles of the sensor unit 5 and the two firing units 6, 7 are always the same. Also conceivable are other transmission elements, as have been described in connection with the first embodiment.
  • the counter-shot systems described above are characterized in particular by their easy and quick alignability. In lateral arrangement on the vehicle whose width is only slightly increased.
  • the described counter-shot systems are also suitable as retrofit solutions for vehicles already in use.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
EP09167816.9A 2008-08-21 2009-08-13 Lanceur de contre-mesures Active EP2157398B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102008038603.0A DE102008038603C5 (de) 2008-08-21 2008-08-21 Gegenschussanlage

Publications (3)

Publication Number Publication Date
EP2157398A2 true EP2157398A2 (fr) 2010-02-24
EP2157398A3 EP2157398A3 (fr) 2012-07-18
EP2157398B1 EP2157398B1 (fr) 2017-10-11

Family

ID=41056955

Family Applications (1)

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EP09167816.9A Active EP2157398B1 (fr) 2008-08-21 2009-08-13 Lanceur de contre-mesures

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EP (1) EP2157398B1 (fr)
DE (1) DE102008038603C5 (fr)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017200460A1 (fr) * 2016-05-17 2017-11-23 Saab Ab Dispositif et procédé de limitation de direction de tir et agencement de contre-mesure
WO2017200455A1 (fr) * 2016-05-17 2017-11-23 Saab Ab Distributeur à magasin inclinable et procédé de lancement de contre-mesures
WO2017200454A1 (fr) * 2016-05-17 2017-11-23 Saab Ab Magasin et procédé de lancement de contre-mesures
WO2017200458A1 (fr) * 2016-05-17 2017-11-23 Saab Ab Magasin, cartouche et procédé pour la densité variable de groupe de projectiles d'une contre-mesure
WO2017200459A1 (fr) 2016-05-17 2017-11-23 Saab Ab Chargeur, cartouche et procédé pour lancer une contre-mesure
CN109539888A (zh) * 2018-12-17 2019-03-29 科立讯通信股份有限公司 反无人机监察装置
US10696401B2 (en) 2016-05-17 2020-06-30 Saab Ab Countermeasure dispenser with variable spoiler and method for launching a countermeasure
WO2020246931A1 (fr) * 2019-06-03 2020-12-10 Saab Ab Distributeur et procédé de lancement de contre-mesures
FR3105391A1 (fr) 2019-12-24 2021-06-25 Nexter Systems Dispositif lanceur de munitions
US20230002053A1 (en) * 2021-07-01 2023-01-05 Saab Ab Ejecting System, Method And Vehicle

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012002043C5 (de) * 2012-02-02 2016-05-12 Diehl Bgt Defence Gmbh & Co. Kg Waffenbasierte Schutzeinrichtung für Fahrzeuge
DE102024105508A1 (de) * 2024-02-27 2025-08-28 Rheinmetall Waffe Munition Gmbh Getriebeeinheit zur Aufnahme und Ausrichtung von Werfersegmenten einer Werfereinheit und Werfereinheit
DE102024105507A1 (de) * 2024-02-27 2025-08-28 Rheinmetall Waffe Munition Gmbh Getriebeeinheit zur Aufnahme und Ausrichtung von Werfersegmenten einer Werfereinheit und Werfereinheit
DE102024105505A1 (de) * 2024-02-27 2025-08-28 Rheinmetall Waffe Munition Gmbh Wurfeinrichtung und Verfahren zum Ausbringen von Wirkmitteln

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DE102006050604B3 (de) 2006-10-26 2008-01-31 Moog Gmbh Richtantrieb für eine Waffe mit Differentialgetriebe

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Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3458793A4 (fr) * 2016-05-17 2019-12-25 Saab AB Dispositif et procédé de limitation de direction de tir et agencement de contre-mesure
IL262828B (en) * 2016-05-17 2022-08-01 Saab Ab Device and method for firing direction limitation and a countermeasure arrangement
WO2017200454A1 (fr) * 2016-05-17 2017-11-23 Saab Ab Magasin et procédé de lancement de contre-mesures
WO2017200458A1 (fr) * 2016-05-17 2017-11-23 Saab Ab Magasin, cartouche et procédé pour la densité variable de groupe de projectiles d'une contre-mesure
WO2017200460A1 (fr) * 2016-05-17 2017-11-23 Saab Ab Dispositif et procédé de limitation de direction de tir et agencement de contre-mesure
IL262820A (en) * 2016-05-17 2018-12-31 Saab Ab Ammunition depot, cartridge and method for launching countermeasures
IL262817A (en) * 2016-05-17 2018-12-31 Saab Ab Ammunition depot and method of launching countermeasures
IL262823A (en) * 2016-05-17 2018-12-31 Saab Ab Dispenser with a tiltable ammunition reservoir and a method of launching countermeasures
EP3458802A4 (fr) * 2016-05-17 2019-12-25 Saab AB Chargeur, cartouche et procédé pour lancer une contre-mesure
US10495424B2 (en) 2016-05-17 2019-12-03 Saab Ab Magazine, cartridge and method for variable projectile cluster density of a countermeasure
EP3458801A4 (fr) * 2016-05-17 2019-12-25 Saab AB Magasin, cartouche et procédé pour la densité variable de groupe de projectiles d'une contre-mesure
EP3458798A4 (fr) * 2016-05-17 2019-12-25 Saab Ab Distributeur à magasin inclinable et procédé de lancement de contre-mesures
WO2017200455A1 (fr) * 2016-05-17 2017-11-23 Saab Ab Distributeur à magasin inclinable et procédé de lancement de contre-mesures
EP3458797A4 (fr) * 2016-05-17 2019-12-25 Saab Ab Magasin et procédé de lancement de contre-mesures
WO2017200459A1 (fr) 2016-05-17 2017-11-23 Saab Ab Chargeur, cartouche et procédé pour lancer une contre-mesure
US10684099B2 (en) 2016-05-17 2020-06-16 Saab Ab Magazine, cartridge and method for launching a countermeasure
US10683092B2 (en) 2016-05-17 2020-06-16 Saab Ab Magazine and method for launching countermeasures
US10683090B2 (en) 2016-05-17 2020-06-16 Saab Ab Dynamically with tiltable magazine and method for launching countermeasures
US10696401B2 (en) 2016-05-17 2020-06-30 Saab Ab Countermeasure dispenser with variable spoiler and method for launching a countermeasure
US11008099B2 (en) 2016-05-17 2021-05-18 Saab Ab Device and method for firing direction limitation and a countermeasure arrangement
CN109539888A (zh) * 2018-12-17 2019-03-29 科立讯通信股份有限公司 反无人机监察装置
WO2020246931A1 (fr) * 2019-06-03 2020-12-10 Saab Ab Distributeur et procédé de lancement de contre-mesures
US11845552B2 (en) 2019-06-03 2023-12-19 Saab Ab Dispenser and method for launching countermeasures
FR3105391A1 (fr) 2019-12-24 2021-06-25 Nexter Systems Dispositif lanceur de munitions
WO2021130605A1 (fr) 2019-12-24 2021-07-01 Nexter Systems Dispositif lanceur de munitions
US11719500B2 (en) 2019-12-24 2023-08-08 Nexter Systems Ammunition launching device
US20230002053A1 (en) * 2021-07-01 2023-01-05 Saab Ab Ejecting System, Method And Vehicle
US11685526B2 (en) * 2021-07-01 2023-06-27 Saab Ab Ejecting system, method and vehicle

Also Published As

Publication number Publication date
DE102008038603C5 (de) 2018-04-19
EP2157398A3 (fr) 2012-07-18
EP2157398B1 (fr) 2017-10-11
DE102008038603A1 (de) 2010-03-04
DE102008038603B4 (de) 2013-08-08

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