ZA200901311B - Fuze for a projectile - Google Patents

Fuze for a projectile Download PDF

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Publication number
ZA200901311B
ZA200901311B ZA2009/01311A ZA200901311A ZA200901311B ZA 200901311 B ZA200901311 B ZA 200901311B ZA 2009/01311 A ZA2009/01311 A ZA 2009/01311A ZA 200901311 A ZA200901311 A ZA 200901311A ZA 200901311 B ZA200901311 B ZA 200901311B
Authority
ZA
South Africa
Prior art keywords
firing
fuze
explosive
relay
booster
Prior art date
Application number
ZA2009/01311A
Inventor
Frank Martin Kienzler
Markus Kopf
Frank Weisser
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
Publication of ZA200901311B publication Critical patent/ZA200901311B/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00Details of fuzes
    • F42C19/02Fuze bodies; Fuze housings
    • 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

Description

. ~~ lle "2000/0154, ) | Fuze for a projectile
Field of the Invention
This invention relates to a fuze for a projectile having a primary firing arrangement and having a secondary firing arrangement, which is separated from the primary firing arrangement by a barrier and has a firing relay with a relay explosive in a sleeve component, and has a firing booster.
Background to the Invention
Fuzes for artillery projectiles, mortar shells or direct projectiles are normally fitted with a primary firing arrangement with a primary firing chain, or a primary firing element and a secondary firing arrangement with a secondary firing chain, or a secondary firing element. A barrier is arranged between the firing chains or firing elements and inhibits inadvertent crossover from the primary firing chain to the secondary firing chain. The barrier may be formed by a plate which is arranged between the firing chains when in the safe position, and is pivoted out of the area between the firing chains when in the armed position. The barrier is frequently formed by a detonator for the primary firing chain, which is pivoted out of a firing line when in the safe position, in such a way that a firing impulse from an initial detonator cannot strike the detonator and no firing impulse from the detonator can strike the second firing chain.
In order to avoid inadvertent firing within the secondary firing chain, it is advantageous for the firing elements for the secondary firing arrangement to be provided with insensitive explosive. In accordance with the - international STANAG standard, an insensitive explosive is an explosive which does not fire when a standard initiator is detonated at a distance of at most 15 mm, water column. It must therefore withstand the pressure wave transmitted by a water column of 15 mm, without firing. This results in a high degree of insensitivity of the explosive to an accidental impact of a ha = **2009/015,, ® bullet or shell fragment, or to an adjacent explosion, in such a way that, for example, an ammunition depot can withstand being fired at.
Accordingly, a need exists for providing a reliably firing fuze for a projectile, which has a high degree of safety against inadvertent firing.
Summary of the Invention
According to the invention, there is provided a fuze for a projectile having a primary firing arrangement and having a secondary firing arrangement, which is separated from the primary firing arrangement by a barrier and has a firing relay with a relay explosive in a sleeve component, and has a firing booster, wherein the sleeve component forms a substantially gas-tight seal for the secondary firing arrangement with respect to the primary firing arrangement.
The invention is in this case based on the idea that insensitive explosive is relatively difficult to fire. A firing element in the primary firing chain, for example a detonator, should therefore be fitted as closely as possible to the insensitive explosive to be fired, for example a firing relay of the secondary firing chain. This requirement is contrary to detonator safety requirements, for example in accordance with AOP Standard 20 which, in addition to the barrier, require that the secondary firing chain be sealed from contact with the hot gases which are developed when a primary initiating device is fired. No fragments, perforations, combustion points, smoke, carbonization or singeing or melting damage may therefore occur oT on the secondary firing arrangement, which in addition must not exhibit any evidence of glowing. A seal must therefore be provided between the : primary and the secondary firing arrangement which is sufficiently gas-tight when it reliably inhibits the damage mentioned above. The barrier can generally not provide a seal such as this since it is intended to allow intentional crossover, that is to say, for example, it must be open. The seal must therefore be provided by an additional component. :
~~ ® The invention is based on the further idea that, in order to form an insensitive firing relay, its relay explosive must be pressed into a housing and must be held in a housing in the fuze. Intentional crossover must therefore pass through both the seal and the housing of the firing relay and sufficient energy must then still be available for crossover to the insensitive firing relay. In order to reliably ensure crossover to an insensitive firing relay, any energy loss caused by the seal and the housing should therefore be as little as possible.
If the housing for the relay explosive and/or the sleeve component intrinsically itself forms a gas-tight seal, then there is no need for a separate seal and energy loss is less than that of two separate components. More energy is therefore available for firing the firing relay, which can therefore be designed to be less sensitive. The sealing sleeve component therefore makes it possible to enhance the safety against inadvertent firing of the firing relay, since this can be kept insensitive.
The projectile may be an artillery projectile, a mortar shell or a direct projectile, in particular in the calibre range from 30 mm to 70 mm. The barrier may be a detonator which can be pivoted out of an armed position, or a shield in the form of a plate. It is expediently provided in addition to the sleeve component. Substantial gas-tightness is achieved if, when a detonator in the primary firing arrangement is fired when in the safe position, no fragments, perforations, combustion points, smoke traces, carbonization or singeing or melting damage occurs on the secondary firing arrangement. The sleeve component is expediently formed integrally. It may be a component of the substantially gas-tight seal, but need not carry out this function on its own. The firing arrangements may each include firing chains, in which case the primary firing arrangement may be provided with just one firing element instead of the firing chain. The secondary firing arrangement includes the firing relay which is provided in order to fire the firing booster. The firing booster is used to fire the main charge of the projectile.
) In one advantageous embodiment of the invention, the sleeve component forms a housing for booster explosive of the firing booster. The booster explosive can thus be held in a defined manner on the relay explosive without the two explosives being held by two components. An undesirable distance between the two explosives can be avoided, as could occur, for example, as a result of manufacturing tolerances of two components. Since the crossover is caused by a pressure wave, the firing relay can be designed to be smaller, with a very small gap being provided or no gap reliably being provided, than when a relatively large gap must be calculated in for safety reasons or tolerance reasons. In the case of a small firing relay, a detonator for the primary firing device can be pivoted, in a physically small form, out of the firing line or the area of the firing relay.
The sleeve component advantageously clasps the booster explosive at least from two directions, in particular from the front and on all sides, in which case the expression sides should be understood as meaning with respect to the fuze alignment. Only at the rear - which in this context should not be understood as meaning a side - can the sleeve component remain open for filling, and can be closed by a closure, for example a plate, after being filled, and can be sealed against moisture.
The sleeve component expediently forms at least a part of hermetically sealed encapsulation of the relay explosive and of the booster explosive for the firing booster. There is no need for any additional, for example side, seals and a high degree of safety can be achieved.
In a further embodiment of the invention, the sleeve component forms a housing for the primary firing arrangement. This allows the primary firing arrangement, and therefore its detonator as well, to be shielded well from the outside, so that combustion gases are inhibited from passing from the primary firing arrangement to the secondary firing arrangement.
The booster explosive of the firing booster can be particularly insensitive and can thus be designed to be particularly safe while it can nevertheless
® be fired reliably, if the relay explosive has different firing characteristics than the booster explosive of the firing booster. If the relay explosive can be fired more easily, this makes it possible to ensure reliable relaying.
Since the firing relay is considerably smaller than the firing booster and it is therefore considerably more difficult for shell fragments or the like to strike it, it is not necessary for the relay explosive to be completely insensitive, in accordance with STANAG. However, the booster explosive is expediently insensitive, in particular in accordance with STANAG. The relay explosive is therefore advantageously a different substance than the booster explosive of the firing booster.
A high degree of safety can nevertheless be achieved if the relay explosive is at least insensitive to a temperature of up to 200°C, since high temperatures can also pass through to a small firing relay.
In a further advantageous embodiment variant of the invention, the sleeve component forms the only material barrier between the relay explosive and an armed detonator for the primary firing arrangement. Reliable crossover can be achieved when the primary firing arrangement is in the armed position.
The fuze has a fuze housing which shields the components arranged in it from the outside and ensures stability on firing and impact. Good shielding of the secondary firing arrangement without the use of additional components can be achieved if the sleeve component forms a load-bearing housing part of the fuze housing. The shielding characteristic of the fuze housing can be used to shield the secondary firing arrangement. The relay explosive can be introduced directly into the sleeve component, and therefore directly into the fuze housing.
The fuze is subject to extremely high accelerations on firing and impact of the projectile, which mechanical and if appropriate electrical components in particular in the primary firing arrangement should withstand with as little damage as possible. For this purpose, the components can be held firmly ’
[ by a solid supporting plate in a fuze housing. A compact arrangement can be achieved if the sleeve component is a supporting plate for supporting the primary firing arrangement. The supporting plate may be the firmest element which holds fuze components arranged further forwards on the fuze housing. It may itself be a component of the fuze housing which surrounds all the elements of the fuze except for the secondary firing arrangement, which can be arranged externally on the load-bearing part of the fuze housing and can be protected from the outside just by a cover.
The sleeve component expediently forms a bottom screw of the fuze, as a result of which the described secure mounting can be linked to the compact design.
Ny It is also proposed that the sleeve component forms a tab in the direction of the primary firing arrangement, in which, in particular, relay explosive is arranged. An embodiment such as this allows the relay explosive to be moved towards the primary firing arrangement, that is to say allows it to be arranged closer to the primary firing arrangement than without the tab. A greater distance between the detonator and the firing relay can be avoided, and absorption of pressure-wave energy by an air space can be kept minor.
A compact design of the fuze and robust mounting of assemblies of the primary firing arrangement can be achieved if the tab engages in a recess in an assembly mount for the primary firing arrangement. The assembly mount allows robust mounting to be achieved and, as a result of the engagement, a distance which absorbs only a small amount of energy.
Detailed Description of the Invention
The invention will now be described by way of the following, non-limiting example with reference to the accompanying drawings from which further advantages of the invention will become evident.
® The drawings illustrate exemplary embodiments of the invention. The drawings and their description contain numerous features in combination which a person skilled in the art will expediently also consider individually and combine to form worthwhile further combinations.
In the figures:
Figure 1 shows a fuze for a projectile, in the form of a partially sectioned illustration,
Figure 2 shows an enlarged detail from Figure 1, with a sleeve component of the secondary firing arrangement, and
Figure 3 shows an alternative sleeve component of the secondary firing arrangement.
Figure 1 shows a fuze 2 for a projectile with a fuze housing 4, which is illustrated partially sectioned in its rear area 8. In the front area 6, the fuze housing 4 may, for example, surround an impact mechanism and possibly electronic components while, in contrast, a primary firing arrangement 10 and, behind it, a secondary firing arrangement 12 are arranged in the rear area 8.
The two firing arrangements 10, 12 are illustrated enlarged in Figure 2. The primary firing arrangement 10 includes a detonator 14 which is illustrated in its armed position in Figure 2. The detonator can be pivoted by means of a mechanism 16 from a safe position to the armed position, with the detonator 14 being arranged laterally offset with respect to the centre axis 18 of the fuze 2 when in the safe position, in such a way that it is not aligned with an opening 20 in a plate 22 which is used as an assembly mount for supporting assemblies of the first firing arrangement 10. The mechanism 16 can be interlocked by means of an interlock 24, for example a double-bolt system, such that it reliably holds the detonator 14 in its safe position.
® The secondary firing arrangement 12 includes a firing relay 26 with relay explosive 28 which rests directly on the booster explosive 30 of a firing booster 32. The relay explosive 28 is mounted in a sleeve component 34 which surrounds it at the front and on all four sides and is open only at the rear towards the booster explosive 30. The sleeve component 34 also forms a housing for the booster explosive 30, which holds this in the form of a pot with side walls 36 which provide shielding in all lateral directions. At the rear, the housing for the booster explosive 30 is closed by a cover 38 and additional sealing composed of a lacquer, so that the relay explosive 28 and the booster explosive 30 are hermetically sealed from the exterior.
The fuze housing 4 of the fuze 2 is fitted with all the assemblies that are present in it and is responsible for the mechanical robustness of the fuze 2 and the mechanically stable position of the assemblies in the fuze 2 during storage, firing, flight and impact. For this purpose, the fuze housing 4 has, inter alia, a base plate 40 which is screwed from the inside into a housing section which is arranged further forwards. The greatest part of the base plate 40 is formed by a bottom screw 42 which is screwed into the circumferential part of the base plate 40. The bottom screw 42.is formed by the front plate part of the sleeve component 34 and supports assemblies of the fuze 2 at the rear. The sleeve component 34 therefore forms a part of the fuze housing 4 of the fuze 2. The relay explosive 28 is therefore inserted or pushed directly into the fuze housing 4.
The sleeve component 34 is provided with a tab 44 which engages in a recess 46 in the plate 22. The opening 20 in the plate 22 is incorporated in this recess 46. The tab 44 ends at the front in a cover 48 which is directly adjacent to the opening 20, or alternatively may be located in the opening 20. This results in the sleeve component 34 being very close to the detonator 14, as a result of which little relay energy is lost from the detonator 14 to the firing relay 26.
When the fuze 2 is launched, the interlock 24 is unlocked by the launch
3 acceleration, and releases the mechanism 16 which moves the detonator 14 out of a peripheral position to its armed position, in which it is arranged : on the centre axis 18, as is illustrated in Figure 2. On impact of the fuze 2 or at a time which is predetermined by electronics, an initial detonator which is not illustrated is fired, and passes its relay energy through a channel 50 to the detonator 14. Its conventional explosive is fired and its pressure wave destroys the cover 48 of the sleeve component 34, in such a way that the pressure wave can reach the insensitive relay explosive 28.
As a result on the one hand of the close proximity of the relay explosive 28 to the detonator 14 and on the other hand the separation of the relay explosive 28 and the detonator 14 by just a single component, specifically the cover 48, little relay energy is lost and the detonator 14 is able to fire the firing relay 26. It is also feasible for the relay explosive 28, although it is not an insensitive explosive in accordance with STANAG, but is also not a conventional explosive, nevertheless to be characterized by at least being insensitive to high temperatures, for example up to 200°C.
The fired relay explosive 28 now itself fires the booster explosive 30, which is insensitive in accordance with STANAG and in turn fires the main charge of the projectile. As a result of the direct contact on the relay explosive 28 with the booster explosive 30, which is also regarded as being present when only a layer composed of air or material, for example lacquer of less than 300 um is present between the relay explosive 28 and the booster explosive 30, no relay energy or only a small amount of relay energy is lost, as a result of which the energy of the relatively small firing relay 26 is sufficient to fire the insensitive booster explosive 30. Its pressure wave blows off the cover 38 and a cover 52 which is screwed to the fuze housing 4, in order to protect the secondary firing arrangement 12, and fires the main charge.
If a large amount of energy is applied to the fuze 2 when in its safe position, for example by a high temperature resulting from the influence of combustion or by impact of a bullet or of a fragment on the fuze 2, then no
® explosive in the secondary firing arrangement 12 is fired since both the relay explosive 28 and the booster explosive 30 are insensitive in accordance with STANAG. If the relay explosive 28 is only temperature- insensitive, then it could admittedly be fired, for example, by a fragment striking it directly, but such an impact will with a high degree of probability be suppressed because of the highly protected position of the firing relay 26 in the sleeve component 34 and in the plate 22. This also results in a high level of safety.
Less protected and furthermore more sensitive are the explosive of the detonator and of the initial detonator which may be present. In the event of inadvertent firing of the detonator 14 or of the initial detonator, the firing relay 26 and its relay explosive 28 must not be adversely affected. This is achieved by the hermetic sealing of the secondary firing chain by the sleeve element 34, which surrounds the secondary firing chain and is formed integrally, in conjunction with the cover 38.
Figure 3 shows an alternative sleeve element 54 with a firing relay 56 inserted in it with relay explosive 58. The following description is restricted essentially to the differences from the exemplary embodiment in Figures 1 and 2, to which reference is made with regard to features and functions which remain the same. Components which remain essentially the same are in principle provided with the same reference symbols, and features which are not mentioned have been adopted in the following exemplary embodiment although they will not be described again.
The sleeve element 54 forms a housing for the primary firing arrangement 10 at the front, by means of a circumferential wall 60 at the side. The sleeve component 54 forms a part of the fuze housing 4 and can be screwed with the aid of a thread 62 to a section of the fuze housing 4 which is located further forwards. A rearward thread 64 is used for screwing on the cover 52. As in the case of the sleeve component 34, the relay explosive 58 is inserted, for example pressed, directly into the sleeve component 54 and therefore into the fuze housing 4. The firing booster 32
® can be attached to the sleeve element 54 behind the firing relay 56, for example with the aid of screw holes 66. It is likewise feasible to provide a side wall 36 on the sleeve element 54, as in the case of the sleeve element 34, in particular integrally.
As a result of the primary firing arrangement 10 being surrounded like a pot and the screw connection to the section of the fuze housing 4 which is located further forwards, the secondary firing chain with the firing relay 56 and the firing booster 32 located further to the rear is separated in a gas- tight manner from the detonator 14.
It is to be appreciated, that the invention is not limited to any particular embodiment or configuration as hereinbefore generally described or illustrated.
The claims which follow are to be considered an integral part of the present disclosure. Reference numbers (directed at the drawings) shown in the claims serve to facilitate the correlation of the integers of the claims with illustrated features of the preferred embodiment(s), but are not intended to restrict in any way the language of the claims to what is shown in the drawings, unless the contrary is clearly apparent from the context.
List of reference symbols: 2 Fuze 4 Fuze housing (of 2) 6 Area (of 4) 8 Area (of 4) 10 Primary firing arrangement (of 2) 12 Secondary firing arrangement (of 2) 14 Detonator (of 10) 16 Mechanism (of 10) 18 Centre axis (of 2) 20 Opening (of 22)
® 22 Plate (of 2)
24 Interlock (of 10) 26 Firing relay (of 12) 28 Relay explosive (of 26)
30 Booster explosive (of 32) 32 Firing booster (of 12) 34 Sleeve component (of 12) 36 Side wall (of 34) 38 Cover (of 34)
40 Base plate (of 4) 42 Bottom screw (of 4) 44 Tab (of 34) 46 Recess (of 22) 48 Cover (of 44)
50 Channel (of 10) 52 Cover (of 2) 54 Sleeve element (of 2) 56 Firing relay (of 12)
58 Relay explosive (of 56)
60 Wall (of 54) 62 Thread (of 54) 64 Thread (of 54) 66 Screw hole (of 54)

Claims (17)

o wn NINN Co ee
1. A fuze (2) for a projectile having a primary firing arrangement (10) and having a secondary firing arrangement (12), which is separated from the primary firing arrangement (10) by a barrier and has a firing relay (26) with a relay explosive (28) in a sleeve component (34, 54), and has a firing booster (32), wherein the sleeve component (34, 54) forms a substantially gas-tight seal for the secondary firing arrangement (12) with respect to the primary firing arrangement (10).
2. A fuze (2) as claimed in claim 1, wherein the sleeve component (34, 54) forms a housing for booster explosive (30) of the firing booster (32).
3. A fuze (2) as claimed in claim 1 or claim 2, wherein the sleeve component (34, 54) forms at least a part of hermetically sealed encapsulation of the relay explosive (28) and of booster explosive (30) for the firing booster (32). :
4, A fuze (2) as claimed in any one of claims 1 to 3, wherein the sleeve component (54) forms a housing for the primary firing arrangement (10).
5. A fuze (2) as claimed in any one of the preceding claims, wherein the relay explosive (28) has different firing characteristics than a booster explosive (30) of the firing booster (32).
6. A fuze (2) as claimed in any one of the preceding claims, wherein relay explosive (28) is a different substance than a booster explosive (30) of the firing booster (32).
7. A fuze (2) as claimed in any one of the preceding claims, wherein the firing booster (32) has an insensitive booster explosive (30).
® 8. A fuze (2) as claimed in any one of the preceding claims, wherein the relay explosive (28) is insensitive to a temperature of up to 200°C.
9. A fuze (2) as claimed in any one of the preceding claims, wherein the sleeve component (34, 54) forms the only material barrier between the relay explosive (28) and an armed detonator (14) for the primary firing arrangement (10).
10. Afuze (2) as claimed in any one of the preceding claims, including a fuze housing (4), wherein the sleeve component (34, 54) forms a load-bearing housing part of the fuze housing (4).
11. A fuze (2) as claimed in any one of the preceding claims, wherein the sleeve component (34, 54) is a supporting plate for supporting the primary firing arrangement (10).
12. Fuze (2) according to one of the preceding claims, characterized in that the sleeve component (34) forms a bottom screw of the fuze housing (4). :
13. A fuze (2) as claimed in any one of the preceding claims, wherein the sleeve component (34, 54) forms a tab (44) in the direction of the primary firing arrangement.
14. A fuze (2) as claimed in claim 13, wherein the tab (44) engages with a recess (46) in an assembly mount for the primary firing arrangement (10).
15. A fuze (2) according to the invention substantially as hereinbefore described or exemplified.
C 16. A fuze (2) as specifically described with reference to or as illustrated in any one of the accompanying drawings.
17. A fuze (2) including any new and inventive integer or combination of integers, substantially as herein described. DATED AT PRETORIA THIS 24™ DAY OF FEBRUARY 2009. HAHN & HAHN INC. APPLICANT'S ATTORNEYS
ZA2009/01311A 2008-02-26 2009-02-24 Fuze for a projectile ZA200901311B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102008011081A DE102008011081B4 (en) 2008-02-26 2008-02-26 Igniter for a projectile

Publications (1)

Publication Number Publication Date
ZA200901311B true ZA200901311B (en) 2010-02-24

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Family Applications (1)

Application Number Title Priority Date Filing Date
ZA2009/01311A ZA200901311B (en) 2008-02-26 2009-02-24 Fuze for a projectile

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US (1) US20090260533A1 (en)
EP (1) EP2096402A3 (en)
DE (1) DE102008011081B4 (en)
ZA (1) ZA200901311B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201106126D0 (en) 2011-04-11 2011-05-25 Secr Defence An explosive projectile

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US2537855A (en) * 1944-06-09 1951-01-09 Henry H Porter Point contact fuse
DE1202181B (en) * 1963-05-31 1965-09-30 Junghans Geb Ag Transport safety device for clockwork timer for twistless projectiles
CH419909A (en) * 1965-03-18 1966-08-31 Industrial Holding Ets Projectile rocket
FR1463669A (en) * 1965-04-02 1966-06-03 Mefina Sa Projectile fuze for rifled bore cannon
US3380385A (en) * 1965-12-08 1968-04-30 Magnavox Co Energy-absorbing interruptor
FR1528313A (en) * 1967-05-25 1968-06-07 Forsvarets Fabriksverk Firing delay device, in particular for projectile rockets, as well as projectile rockets or projectiles equipped with this device
US3455244A (en) * 1967-09-22 1969-07-15 Dynamit Nobel Ag Shockproof primer cover
CH517932A (en) * 1970-05-14 1972-01-15 Mefina Sa Rocket for non-rotating projectile
DE2509058A1 (en) * 1975-03-01 1976-09-09 Diehl Fa Delayed action ignition unit with explosive charges - has metallic expansion and delay elements between primary and secondary changes
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Publication number Publication date
US20090260533A1 (en) 2009-10-22
EP2096402A2 (en) 2009-09-02
EP2096402A3 (en) 2013-05-29
DE102008011081A1 (en) 2009-08-27
DE102008011081B4 (en) 2010-04-08

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