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EP2049281B1 - Method and device for explosion forming - Google Patents

Method and device for explosion forming Download PDF

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Publication number
EP2049281B1
EP2049281B1 EP07724979A EP07724979A EP2049281B1 EP 2049281 B1 EP2049281 B1 EP 2049281B1 EP 07724979 A EP07724979 A EP 07724979A EP 07724979 A EP07724979 A EP 07724979A EP 2049281 B1 EP2049281 B1 EP 2049281B1
Authority
EP
European Patent Office
Prior art keywords
explosion
ignition
tool
energy beam
explosive
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.)
Not-in-force
Application number
EP07724979A
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German (de)
French (fr)
Other versions
EP2049281A1 (en
Inventor
Alexander Zak
Andreas Stranz
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.)
Cosma Engineering Europe AG
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Cosma Engineering Europe AG
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Publication date
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Publication of EP2049281A1 publication Critical patent/EP2049281A1/en
Application granted granted Critical
Publication of EP2049281B1 publication Critical patent/EP2049281B1/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D26/00Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
    • B21D26/02Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
    • B21D26/06Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure by shock waves
    • B21D26/08Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure by shock waves generated by explosives, e.g. chemical explosives

Definitions

  • the invention relates to a method and an apparatus for explosion forming with the features of the preamble of claim 1 and 7, respectively.
  • a workpiece is placed in a tool and ignited by igniting an explosive substance, e.g. of a gas mixture, reshaped.
  • an explosive substance e.g. of a gas mixture
  • the explosive substance is introduced into the tool and ignited here as well.
  • the tool or the ignition mechanism must be suitable for triggering the explosion targeted and withstand the high loads occurring during the explosion, on the other hand, repeatable good forming results in the shortest possible set-up times can be achieved.
  • the hollow body is placed in a tool and the upper opening of the hollow body sealed with a stopper. Via a line in the plug, an explosive gas is introduced into the cavity, which is then ignited via a plug arranged in the spark plug.
  • a workpiece to be deformed is also arranged in a tool and filled with an explosive gas mixture.
  • the ignition takes place here by means of explosive mercury and a heating or glow wire Both methods are particularly suitable for the production of individual parts and could not prevail in practice for mass production.
  • the DE 29 08 561 A1 describes a method in which an explosive in with a suitable. Energy transfer means provided or filled workpiece is inserted without any igniter. The covering of the explosive is done so that one for a laser beam overcome space is created. After closing the die and damaging the workpiece openings, the explosive is ignited by means of a laser beam.
  • the US 3, 742, 746 describes an apparatus for improved reshaping with reduced electrode consumption by igniting an explosive mixture above a liquid.
  • the liquid is applied to a membrane, which is stretched over the lower end of a chamber. As the mixture explodes, the pressure is passed through the membrane to reshape a workpiece into a die.
  • the US Pat. No. 3,661,004 discloses a rupture-resistant piston and an explosive insert disposed therein for deforming a tube.
  • an explosive charge is arranged in the piston and a transfer agent such. Gum, is placed over the piston to form the insert.
  • the insert is inserted into a tube and ignited the explosion charge, whereby the tube against a sleeve or a. Form is deformed.
  • the invention has for its object to improve a method and an apparatus of the type mentioned in that a technically easy-to-handle ignition mechanism with low makeready arises, which allows the most accurate ignition of the explosive substance with repeatable accuracy.
  • Ignition by means of an energy beam allows the explosion in the tool to be well controlled.
  • the energy beam is relatively precisely positioned on a firing point, from which the explosion is expected.
  • the amount of energy supplied to the explosive by the energy beam is easily adjustable.
  • the energy beam and thus the explosion is also relatively precisely timed controllable. The above factors make it easy to control the explosion and its course within the tool. Thus, a good predictability and repeatability of the forming result is possible.
  • the energy beam can be generated with the help of a laser.
  • a laser beam is easy to control in terms of temporal and local accuracy.
  • the energy beam from an energy source with the aid of a deflection arrangement can be passed to at least one ignition point.
  • the energy beam can be quickly and technically easily guided to the desired locations in the room, despite the possibility of a stationary energy beam generator.
  • the energy beam may be directed from an energy source by means of a mirror arrangement to at least one ignition point.
  • the mirror arrangement is particularly suitable for energy beams in the form of laser beams and offers the above-mentioned advantages of a deflection arrangement.
  • the explosive can be ignited simultaneously at several points of the device. For example, you can create multiple detonation fronts within a tool. Depending on where the explosive is located within the tool and at which point it is ignited, the course of the detonation fronts can be adapted to the requirements of the forming process. Alternatively, in this process, however, it is also possible to ignite explosives in several tools of the device simultaneously, for example. So several, Also different workpieces are formed almost simultaneously. This helps to shorten the cycle times.
  • the explosive can be ignited at several points of the device with a time delay. If the time-delayed ignition on a single tool of the device, it can be generated multiple detonation fronts within a tool. The temporal offset allows a tuning of the time course of the individual detonation fronts within the tool. If the staggered ignition of different tools of the device, the energy beam z. B. ignite all the tools of the device sequentially. This helps to shorten the cycle times if the parallel forming processes overlap in time.
  • any combination of simultaneous and time-delayed ignition of one and / or more tools of the device are possible. This makes it easy to adapt the process to different production requirements.
  • the basic idea of controlling the propagation of detonation fronts via a time-variable ignition at one or more points of the tool and thus influencing the forming result, would also be independent of the type of ignition, whether with energy beam or otherwise, feasible.
  • multiple detonation fronts can be created within a tool.
  • a good forming result can be achieved.
  • At least one respective detonation front can be generated within several tools of the device.
  • the effectiveness of an ignition device with energy beam can be increased.
  • the energy beam can be introduced into an ignition tube of the tool.
  • a part of the tool namely the ignition tube, can be adapted to the special requirements of the ignition and explosion process.
  • the energy beam can enter the explosion space through a transparent medium. This is technically well feasible and ensures a good impact of the energy beam on the explosive. An energy jet generator can thus be placed outside the tool and is largely protected from the direct effects of the explosion inside the tool.
  • the energy beam ensures good ignition of the explosive. It is technically easy to produce and can overcome distances quickly. As a result, the explosive can be ignited with good timing accuracy.
  • the energy beam generator may comprise a laser.
  • the laser represents a technically simple possibility of energy beam generation. It offers a well-bundled and thus easily positionable energy or laser beam with adjustable amount of energy.
  • the tool may have at least one point of introduction, which is permeable to the energy beam.
  • the energy beam can penetrate into the tool and ignite the explosive contained therein.
  • the energy jet generator can be arranged outside the tool and thus largely protected from the direct effects of the explosion.
  • the point of introduction can have at least one transparent medium. This is particularly suitable for laser beams. It ensures a good transmission of the energy beam with relatively little energy loss.
  • the transparent medium may have a glass insert.
  • Glass is a cheap and easy to process material, which provides the above advantages and is sufficiently resistant to the explosive forces occurring.
  • the transparent medium or the glass insert may have a thickness in the range of 5 to 15 mm, preferably in the range of 7 to 12 mm and in particular in the range of 9 to 11 mm. This thickness has been in the Practice proven advantageous. It ensures sufficient stability to withstand the requirements of the explosion.
  • the transparent medium or the glass insert may have an outer diameter of about 5 to 15 mm, preferably 7 to 12 mm and in particular 9 to 11 mm. It has been shown that this outer diameter allows a sufficiently good and fast positioning of the energy beam with at the same time good stability of the medium.
  • the transparent medium can be lens-like, convex. This allows the energy beam to be well bundled.
  • the transparent medium may have an approximately quadrangular cross-section. This ensures good stability and good transmission properties.
  • the transparent medium may have an octagonal cross-section.
  • the energy beam can be bundled in this way.
  • the transparent medium may comprise a socket containing copper. It has been found that copper alloys, in particular copper-beryllium alloys, provide sufficiently good stability and good sealing properties for this application.
  • the transparent medium can be arranged with a seal in the tool, which seals the explosion space from the environment. This protects the environment from explosion and explosion products.
  • the tool can have a plurality of introduction points.
  • the explosive can be ignited at several points of the tool simultaneously and / or with a time delay. For example, several detonation fronts can be created in the tool.
  • several tools can be provided with at least one introduction point.
  • several, possibly even different tools of the device can be ignited simultaneously or with a time delay. If the resulting parallel forming processes overlap in time, the efficiency of the device can be increased.
  • At least one deflection arrangement can be provided in the beam path of the energy beam generator, by means of which the energy beam can be directed to at least one ignition point. This makes the energy beam technically easy, fast and easy to position.
  • the deflection arrangement may be a mirror arrangement. This is particularly suitable for laser beams and offers the above-mentioned advantages of a deflection arrangement.
  • the deflecting arrangement can have at least one mirror element that is partially transparent to the energy beam. This makes it technically easy to divide the energy beam into several beams.
  • Fig. 1 shows an apparatus for explosion forming according to a first embodiment of the invention.
  • the device 1 has a tool 2 and an energy beam generator 3.
  • the tool 2 is in this embodiment of the invention in several parts and has a forming means 4 and an ignition tube 5 on.
  • a forming means 4 here indicated by a dotted line workpiece 18 is arranged.
  • an ignition chamber 6 is provided inside the ignition tube 5, inside the ignition tube 5, an ignition chamber 6 is provided. In it there is an explosive 7.
  • an explosive gas mixture is provided as the explosive 7, which can be introduced into the ignition chamber 6 via the connection 8.
  • other explosive means may also be used in gaseous form.
  • the terminal 8 is then formed according to the respective explosive means.
  • the energy beam generator 3 can optionally generate an energy beam 12 and in this embodiment is a laser device, which is mounted rotatably about a vertical axis 9 on a foot 10. It is powered via a line 11 with energy and can generate an energy, in this case, a laser beam 12, if necessary.
  • the wall 13 of the ignition tube 5 has a permeable to the energy beam 12 discharge point 14.
  • a transparent medium 15 is provided, which is at least partially permeable to the energy beam 12.
  • the transparent medium 15 has a glass insert 19, which in Fig. 2 is shown in more detail.
  • the laser device 3 is arranged so that the laser beam 12 can penetrate through the transparent medium 15 into the ignition chamber 6 of the ignition tube 5. As a result, the explosive 7 is ignited in the ignition chamber 6.
  • the tool 2 of the device 1 can also have a plurality of introduction points 14 for the energy beam 12 or ignition points.
  • the device 1 can, as dashed lines here is shown, for example, a further ignition tube 5 ', which is formed in this embodiment analogous to the first ignition tube 5. Accordingly, it also has an ignition chamber 6 'filled with an ignition means 7, a transparent medium 15' and a connection 8 '.
  • the laser device 3 By rotating the laser device 3 about the vertical axis 9, the laser device 3 can be brought from its first position 16, in which the laser beam 12 enters the ignition chamber 6 of the first ignition tube 5, in a second position 17, in which the laser beam 12 through the transparent medium 15 'in the ignition chamber 6' of the second ignition tube 5 'falls, as in Fig. 1 shown in dashed lines.
  • the ignition means 7 in the ignition tubes 5, 5 ' for example, be ignited successively by the laser device 3.
  • the workpiece 18 may be arranged in this case, for example between the two ignition tubes 5, 5 ', as in Fig. 1 indicated by a dotted and a dashed line.
  • Fig. 2 shows a section II-II through the energy beam 12 permeable inlet point 14 of the ignition tube 5.
  • the in Fig. 2 Reference numerals used denote the same parts as in FIG Fig. 1 , so in this regard to the description of the Fig. 1 is referenced.
  • the transparent medium 15 in this embodiment of the invention has a round glass insert 19 with a quadrangular cross-section.
  • the outer diameter and the thickness of the glass insert are approximately equal.
  • the diameter as well as the thickness of the glass insert 19 is 10 mm.
  • this ratio may vary significantly.
  • the dimensions of the glass insert and its external shape can be adapted to the particular application.
  • the cross section through the glass body can also be octagonal.
  • the ignition chamber-side surface 20 and / or its opposite surface 21 of the glass insert 19 may be curved so that an approximately lens-like shape of the glass insert 19 results.
  • the material of the insert 19 may vary depending on the application. If, as here, a laser used as an energy beam generator, for example, pressure and heat resistant, yet translucent plastics are conceivable.
  • the transparent medium 15 also has a socket 22 in which the glass insert 19 is arranged.
  • the socket 22 is made in this embodiment of the invention from a copper-beryllium alloy. This is stable and holds the dynamic, abruptly occurring relatively high loads from the explosion well. Alternatively, however, the socket 22 may be made of a different copper alloy or any other material which will withstand the high explosive loads. Its wall 23 has an L-like cross-section. The inner contour of the socket 22 corresponds approximately to the outer dimensions of the glass insert 19th
  • the transparent medium 15 is arranged with a seal 24 in the ignition tube 5, which seals the ignition chamber 6 in the interior of the ignition tube 5 from the environment.
  • the wall 13 of the ignition tube 5 and the socket 22 form a press fit.
  • the device 1 in other embodiments of the invention may also comprise a plurality of tools 2, as in FIGS Fig. 3a . 3b exemplified.
  • the Fig. 3a and 3b show possible embodiments of a device according to the invention with a plurality of tools.
  • the tools 2a to 2d correspond to the in Fig. 1 shown and described tool 2.
  • the Fig. 3a and 3b merely show different possibilities to realize such a device.
  • the invention is by no means limited to the embodiments shown in these figures. Rather, those in the Fig. 3a and 3b shown operating principles in any way, depending on the application also combined.
  • Fig. 3a shows a schematic representation of an apparatus according to a second embodiment of the invention.
  • device 1 has a plurality of tools 2 and a plurality of energy beam generators or laser devices 3.
  • the training of these devices corresponds to that in the Fig. 1 and 2 shown training, multiple occurring, same components are therefore provided with the addition a, b, etc.
  • the device 1 here has four tools 2a to 2d and four laser devices 3a to 3d.
  • the tools 2a to 2d are arranged approximately on a dotted circle 30 indicated here.
  • the laser devices 3a to 3d are arranged approximately on a circle 31, which lies approximately concentrically within the circle 30.
  • the laser devices 3a to 3d are arranged in relation to the tools 2a to 2d so that each one of the laser beams 12a to 12d penetrate through the transparent medium 15 each one of the tools 3a to 3d in the ignition chamber 6a to 6d and there ignite the explosive 7 can.
  • the two laser devices 3a and 3b are replaced by a single, here shown in phantom laser device, which analog Fig. 1 is mounted rotatably about its vertical axis 9.
  • this laser device could occupy both the position of the laser device 3a and the position of the laser device 3b.
  • the laser devices 3c and 3d which are likewise replaceable by a single laser device rotatable about the vertical axis 9.
  • Fig. 3b shows a schematic representation of a device according to a third embodiment of the invention.
  • the Fig. 3a shown device 1 has a plurality of tools 2 and energy or laser beam generator 3.
  • the formation of the individual tools 2a to 2d and the energy beam generator 3 corresponds to that in the Fig. 1 and 2 shown tool 2 and energy beam generator. 3
  • the device 1 here additionally has a deflection arrangement 25 for the energy or laser beam 12.
  • the deflection arrangement 25 is a mirror arrangement. It has a central, polyhedron-like element 27 and a plurality, in this case three, further mirror elements 28.
  • the surfaces of the central element 27 also have mirrors 29.
  • four surfaces of the central element 27 are provided with mirrors 29.
  • At least one of the mirrors 29 may be partially transparent to the energy or laser beam 12.
  • a partially transmissive mirror 29 reflects a predetermined part of the laser light or beam 12 impinging on it. The remaining part of the laser beam 12 passes through almost unchanged the partially transmissive mirror.
  • the laser beam 12 emitted from the laser device 3 can be split.
  • the central, polyhedron-like element 27 is rotatable about its vertical axis 33, arranged approximately in the center of a circle 26 indicated dotted, while the mirror elements 28 are arranged approximately on the circle 26.
  • the mirror elements 28 are rotatably mounted about their respective vertical axis 32.
  • the individual parts 27, 28, 29 of the mirror assembly 25 are arranged in relation to the laser device 3 and the tools 2a to 2d so that the laser beam 12 depending on the orientation of the mirror 28 and 29 optionally through the transparent medium 15 of the tools 2a until 2d is conducted to an ignition point in the respective ignition chamber 6a to 6d.
  • the deflection or mirror arrangement 25 is shown and described here with a central, polyhedron-like element 27 and a plurality of mirror elements 28, the deflection arrangement 25 can also be designed completely differently in other embodiments of the invention.
  • the number and position of the mirror elements 28 may vary depending on the application.
  • the individual elements 27, 28, 29 of the deflection arrangement 25 also do not necessarily have to be arranged on or inside a circle 26, as shown here.
  • the central element 27, which here is polyhedron-shaped may also have another, e.g. have disc-like shape or omitted altogether.
  • the individual elements 27, 28, 29 of the deflection arrangement 25 can also be tilted relative to one another.
  • the height of the laser beam 12 above the ground on which the device stands varies.
  • the individual elements 27, 28, 29 of the deflection assembly 25 may be provided with rotary and / or ball joints.
  • the laser beam 12 may be e.g. also be guided by means of one or more glass fiber elements to one or more discharge points 14 in a tool 3.
  • the arrangement and design of the individual tools 2a to 2d may differ from the one shown here and vary depending on the application.
  • the functionality is based on the Fig. 1 and 2 first described for a device with a tool and an energy jet generator.
  • the energy jet generator or the laser device 3 of the device 1 in FIG Fig. 1 is positioned so that the laser beam 12 can fall through the transparent medium 15 in the wall 13 of the ignition tube 5 in the ignition chamber 6.
  • the tool 2 in this case the ignition tube 5 of the tool 2, is filled with the explosive 7.
  • an explosion means e.g. Oxyhydrogen, passed into the ignition chamber 6 of the ignition tube 5.
  • the terminal 8 is closed.
  • an energy beam in this case a laser beam 12, is generated in the energy beam generator or the laser device 3.
  • the emanating from the laser device 3 laser beam 12 strikes the transparent medium 15, penetrates this and strikes in the ignition chamber 6 on the explosive 7th
  • the laser beam 12 strikes here on the outer surface 21 of the glass insert 19 of the transparent medium 15. Due to the nature and shape of the glass insert 19, the laser beam penetrates the glass insert 19 largely unhindered and without much deflection and occurs on the ignition chamber side Surface 19 again from the glass insert 19 and thus in the ignition chamber 6 of the ignition tube 5 a. There, the laser beam 12 impinges on the explosive 7 and ignites it in the region of the ignition point 36.
  • the laser beam 12 can be changed.
  • the laser beam 12 can, for example in the case of a convex curvature continue to focus and focus on a specific ignition point. With a concave curvature, however, the laser beam 12 can be spread apart. If the surfaces 20, 21 are inclined relative to one another, as is the case, for example, with a polyhedral or octagonal cross-section, the direction of propagation of the laser beam 12 can be deflected.
  • the resulting in the explosion pressure or detonation front propagates along the ignition tube 5, so enters the workpiece 18 and presses this into the molding means 4.
  • the detonation front propagates in principle starting from the ignition point 36 from spherical. In this case, this means that a part 34 of the detonation front moves from the ignition point 36 in the direction of the workpiece 18. On the other hand, another part 35 of the detonation front moves away from the workpiece 18, as in FIG Fig. 2 shown.
  • the course of this second part 35 of the detonation front can be controlled.
  • the ignition tube 5 is designed such that this part of the detonation front is reflected when it has reached the end of the ignition tube 5, it is possible, for example, to generate two detonation fronts 34, 35, which move over the workpiece 18 offset in time.
  • the temporal offset of the two detonation fronts can be controlled via the position of the ignition point 36 or the point of introduction 14 and the shape of the ignition tube 5.
  • the tool 2 has a plurality of introduction 14 and ignition points 36, as in Fig. 1 indicated by dashed lines, the ignition of the explosive 7 can take place at several points of the tool.
  • the laser device 3 after it has delivered a first laser beam 12 into the ignition chamber 6 of the first ignition tube 5 and thus ignited the explosive 7 in the first ignition tube 5, rotated about the vertical axis 9 from a first position 16 to its second position 17. Subsequently, a further laser beam 12 is generated, which through the transparent medium 15 'of the second ignition tube 5' in the second ignition chamber 6 'falls. There he meets the explosive 7 and ignites it.
  • two detonation fronts within a tool can be created.
  • the course of the two detonation fronts can be influenced, for example, by the suitable arrangement of the inlet 14 or ignition points 36.
  • the inlet 14 or ignition points 36 In the in Fig. 1 As shown embodiment of the invention, so two detonation fronts arise, which move towards each other and meet at a certain point in the tool 2.
  • a tool 2 as in Fig. 1
  • tools 2a to 2d as in the Fig. 3a and 3b
  • the operating principle of these two variants of the invention is in the Fig. 3a and 3b illustrated.
  • the arrangement of the tools 2a to 2d and laser devices 3a to 3d in the Fig. 3a and 3b allows both a simultaneous and a time-delayed ignition of the explosive in the individual tools 2a to 2d.
  • a laser beam 12 is generated, which is so divided and deflected over the deflecting or mirror assembly 25 that it penetrates approximately simultaneously through the transparent media 15a to 15d in the ignition tubes 5a to 5d of the respective tools 2a to 2d and there the Explosive 7 ignited.
  • Fig. 3a delayed in the laser devices 3a to 3d for example, one after the other, each generates a laser beam 12a to 12d.
  • These then also meet successively in the ignition chambers 6a to 6d of the respective tools 2a to 2d and ignite the explosive means 7a to 7d in the tools 2a to 2d in succession. That is, first the explosive 7a in tool 2a, then the explosive 7b in tool 2b, etc.
  • the temporal offset between the generation of the laser beams 12a to 12d is arbitrary selectable.
  • the laser beams 12a and 12b can be simultaneously generated, while the laser beams 12c and 12d are connected in time. In principle, any combinations are conceivable.
  • the laser device 3 can successively generate a plurality of laser beams 12. Between the generation of the individual laser beams, the position of the individual elements 27, 28, 29 of the deflection arrangement relative to each other and / or the position of the laser device 3 is changed so that the laser beam 12 successively through the transparent medium 15a to 15d of another tool 3a to 3d penetrates and so ignites the explosive 7a to 7d.
  • the laser device 3 can generate a continuous laser beam 12, which is deflected by means of the deflection arrangement 25 into the ignition chamber 6a of the first tool 2a and ignites the explosive there. If now also the explosive in the tool 2b are ignited, the position of the individual elements 27, 28, 29 of the deflection assembly 25 to each other and / or the position of the laser device 3 is changed so that the laser beam 12 through the transparent medium 15b in the ignition chamber 6b falls. The procedure is similar for the ignition of the explosive in the tools 2c and 2d.
  • partially transparent deflecting elements in this case partially transparent mirror elements, can be used for the energy beam 12. These allow only a portion of the laser beam 12 to be deflected while the remainder of the laser beam maintains its original direction.
  • the laser beam 12 can be directed to an ignition point, for example in the tool 2a, in order to ignite the explosive 7 there.
  • a partially transparent mirror element a part of the laser beam 12 can be simultaneously directed to another ignition point, for example in the tool 2b, and there also ignite the explosive.

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laser Beam Processing (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Forging (AREA)

Abstract

With the invention, a method and a device for explosive forming of work pieces, in which at least one work piece is arranged in at least one die and there deformed by means of an explosive to be ignited, is to be improved, in that an ignition mechanism that is technically easy to handle is produced with the shortest possible setup times, which permits the most precise possible ignition of the explosive with time-repeatable accuracy. This task is solved by a method and device, in which at least one work piece is arranged in at least one die and deformed there by means of an explosive being ignited, in which the explosive is ignited by means of at least one energy beam.

Description

Die Erfindung betrifft ein Verfahren und eine Vorrichtung zum Explosionsumformen mit den Merkmalen des Oberbegriffs des Anspruchs 1 bzw. 7.The invention relates to a method and an apparatus for explosion forming with the features of the preamble of claim 1 and 7, respectively.

Beim Explosionsumformen wird ein Werkstück in einem Werkzeug angeordnet und durch Zünden eines explosiven Stoffes, z.B. eines Gasgemische, umgeformt. In der Regel wird der explosive Stoff in das Werkzeug eingeleitet und auch hier gezündet. Dabei stellen sich zwei Probleme. Zum einen muss das Werkzeug bzw. der Zündmechanismus dazu geeignet sein, die Explosion gezielt auszulösen und den bei der Explosion auftretenden hohen Belastungen standzuhalten, zum anderen sollen wiederholbar gute Umformergebnisse in möglichst kurzen Rüstzeiten erzielt werden.In explosive forming, a workpiece is placed in a tool and ignited by igniting an explosive substance, e.g. of a gas mixture, reshaped. As a rule, the explosive substance is introduced into the tool and ignited here as well. There are two problems. On the one hand, the tool or the ignition mechanism must be suitable for triggering the explosion targeted and withstand the high loads occurring during the explosion, on the other hand, repeatable good forming results in the shortest possible set-up times can be achieved.

Bei einem aus der EP 0 830 907 bekannten Verfahren zum Verformen von Hohlkörpern, wie z.B. Dosen, wird der Hohlkörper in ein Werkzeug eingelegt und die obere Öffnung des Hohlkörpers mit einem Stopfen verschlossen. Über eine Leitung in dem Stopfen wird ein explosives Gas in den Hohlraum eingeleitet, welches anschließend über eine in dem Stopfen angeordnete Zündkerze gezündet wird.At one of the EP 0 830 907 known method for deforming hollow bodies, such as cans, the hollow body is placed in a tool and the upper opening of the hollow body sealed with a stopper. Via a line in the plug, an explosive gas is introduced into the cavity, which is then ignited via a plug arranged in the spark plug.

Bei einem in der US 3 342 048 beschriebenen Verfahren wird ein zu verformendes Werkstück ebenfalls in einem Werkzeug angeordnet und mit einem explosiven Gasgemisch gefüllt. Die Zündung erfolgt hier mittels Knallquecksilber und einem Heiz- bzw. Glühdraht Beide Verfahren eignen sich insbesondere für die Einzelteilfertigung und konnten sich in der Praxis nicht für die Massenproduktion durchsetzen.At one in the US 3,342,048 described method, a workpiece to be deformed is also arranged in a tool and filled with an explosive gas mixture. The ignition takes place here by means of explosive mercury and a heating or glow wire Both methods are particularly suitable for the production of individual parts and could not prevail in practice for mass production.

Die DE 29 08 561 A1 beschreibt ein Verfahren, bei welchem ein Sprengstoff in ein mit einem geeigneten. Energieübertragungsmittel versehen oder gefüllten Werkstück ohne jeden Zünder eingelegt wird. Das Abdecken des Sprengstoffs erfolgt so, dass ein für einen Laserstrahl überwindbarer Raum geschaffen wird. Nach Schließen des Gesenks und Verdämmen der Werkstücköffnungen erfolgt die Zündung des Sprengstoff mittels Laserstrahl.The DE 29 08 561 A1 describes a method in which an explosive in with a suitable. Energy transfer means provided or filled workpiece is inserted without any igniter. The covering of the explosive is done so that one for a laser beam overcome space is created. After closing the die and damaging the workpiece openings, the explosive is ignited by means of a laser beam.

Die US 3, 742, 746 beschreibt eine Vorrichtung zum Verbesserten Umformen mit reduziertem Elektrodenverbrauch, durch Zünden eines explosiven Gemisches oberhalb einer Flüssigkeit. Die Flüssigkeit liegt dabei an einer Membran an, welche über das untere Ende einer Kammer gespannt ist. Wenn das Gemisch explodiert, wird der Druck durch die Membran weitergegeben, um so ein Werkstück in einer Matrize umzuformen.The US 3, 742, 746 describes an apparatus for improved reshaping with reduced electrode consumption by igniting an explosive mixture above a liquid. The liquid is applied to a membrane, which is stretched over the lower end of a chamber. As the mixture explodes, the pressure is passed through the membrane to reshape a workpiece into a die.

Die US 3, 661, 004 offenbart einen reißfesten Kolben und einen darin angeordneten explosiven Einsatz zum Deformieren eines Rohres. Dabei ist eine explosive Ladung in dem Kolben angeordnet und ein Übertragungsmittel wie z. B. Gummi, ist über dem Kolben platziert um den Einsatz zu bilden. Der Einsatz wird in ein Rohr eingeführt und die Explosionsladung gezündet, wodurch das Rohr gegen eine Hülse oder eine. Form verformt wird.The US Pat. No. 3,661,004 discloses a rupture-resistant piston and an explosive insert disposed therein for deforming a tube. In this case, an explosive charge is arranged in the piston and a transfer agent such. Gum, is placed over the piston to form the insert. The insert is inserted into a tube and ignited the explosion charge, whereby the tube against a sleeve or a. Form is deformed.

Der Erfindung liegt die Aufgabe zugrunde, ein Verfahren sowie eine Vorrichtung der eingangs genannten Gattung dahingehend zu verbessern, dass ein technisch einfach handzuhabender Zündmechanismus mit geringen Rüstzeiten entsteht, welcher ein möglichst präzises Zünden des explosiven Stoffes mit zeitlich wiederholbarer Genauigkeit erlaubt.The invention has for its object to improve a method and an apparatus of the type mentioned in that a technically easy-to-handle ignition mechanism with low makeready arises, which allows the most accurate ignition of the explosive substance with repeatable accuracy.

Diese Aufgabe wird erfindungsgemäß gelöst mit einem Verfahren mit den Merkmalen des Anspruchs 1.This object is achieved according to the invention with a method having the features of claim 1.

Durch die Zündung mittels eines Energiestrahls lässt sich die Explosion in dem Werkzeug gut steuern. Der Energiestrahl ist relativ präzise auf eine Zündstelle positionierbar, von welcher die Explosion ausgehen soll. Auch die dem Explosionsmittel durch den Energiestrahl zugeführte Energiemenge ist gut einstellbar. Zudem ist der Energiestrahl und somit die Explosion auch zeitlich relativ genau steuerbar. Durch die obengenannten Faktoren lässt sich die Explosion und ihr Verlauf innerhalb des Werkzeugs gut steuern. So ist eine gute Vorhersagbarkeit und Wiederholgenauigkeit des Umformergebnisses möglich.Ignition by means of an energy beam allows the explosion in the tool to be well controlled. The energy beam is relatively precisely positioned on a firing point, from which the explosion is expected. Also, the amount of energy supplied to the explosive by the energy beam is easily adjustable. In addition, the energy beam and thus the explosion is also relatively precisely timed controllable. The above factors make it easy to control the explosion and its course within the tool. Thus, a good predictability and repeatability of the forming result is possible.

Der Energiestrahl kann mit Hilfe eines Lasers erzeugt werden. Ein Laserstrahl lässt sich bezüglich der zeitlichen und der örtlichen Genauigkeit gut steuern.The energy beam can be generated with the help of a laser. A laser beam is easy to control in terms of temporal and local accuracy.

Günstigerweise kann der Energiestrahl von einer Energiequelle mit Hilfe einer Umlenkanordnung zu wenigstens einer Zündstelle geleitet werden. So lässt sich der Energiestrahl trotz eines eventuell ortsfesten Energiestrahlenerzeugers schnell und technisch einfach zu den gewünschten Stellen im Raum leiten.Conveniently, the energy beam from an energy source with the aid of a deflection arrangement can be passed to at least one ignition point. In this way, the energy beam can be quickly and technically easily guided to the desired locations in the room, despite the possibility of a stationary energy beam generator.

Der Energiestrahl kann von einer Energiequelle mit Hilfe einer Spiegelanordnung zu wenigstens einer Zündstelle geleitet werden. Die Spiegelanordnung eignet sich insbesondere für Energiestrahlen in Form von Laserstrahlen und bietet die obengenannten Vorteile einer Umlenkanordnung.The energy beam may be directed from an energy source by means of a mirror arrangement to at least one ignition point. The mirror arrangement is particularly suitable for energy beams in the form of laser beams and offers the above-mentioned advantages of a deflection arrangement.

In einer weiteren Ausführungsform der Erfindung kann das Explosionsmittel an mehreren Stellen der Vorrichtung gleichzeitig gezündet werden. So lassen sich z.B. mehrere Detonationsfronten innerhalb eines Werkzeugs erzeugen. Je nachdem, an welcher Stelle sich das Explosionsmittel innerhalb des Werkzeugs befindet und an welcher Stelle es gezündet wird, kann der Verlauf der Detonationsfronten dabei den Erfordernissen des Umformprozesses angepasst werden. Alternativ können bei diesem Verfahren aber z.B. auch Explosionsmittel in mehreren Werkzeugen der Vorrichtung gleichzeitig gezündet werden. So können mehrere, auch unterschiedliche Werkstücke annähernd gleichzeitig umgeformt werden. Dies hilft die Taktzeiten zu verkürzen.In a further embodiment of the invention, the explosive can be ignited simultaneously at several points of the device. For example, you can create multiple detonation fronts within a tool. Depending on where the explosive is located within the tool and at which point it is ignited, the course of the detonation fronts can be adapted to the requirements of the forming process. Alternatively, in this process, however, it is also possible to ignite explosives in several tools of the device simultaneously, for example. So several, Also different workpieces are formed almost simultaneously. This helps to shorten the cycle times.

Vorteilhafterweise kann das Explosionsmittel an mehreren Stellen der Vorrichtung zeitversetzt gezündet werden. Erfolgt die zeitversetzte Zündung an einem einzelnen Werkzeug der Vorrichtung, können dadurch mehrere Detonationsfronten innerhalb eines Werkzeugs erzeugt werden. Der zeitliche Versatz erlaubt dabei eine Abstimmung des zeitlichen Verlaufs der einzelnen Detonationsfronten innerhalb des Werkzeugs. Erfolgt die zeitlich versetzte Zündung an unterschiedlichen Werkzeugen der Vorrichtung, kann der Energiestrahl z. B. alle Werkzeuge der Vorrichtung nacheinander zünden. Dies hilft die Taktzeiten zu verkürzen, wenn sich die parallel ablaufenden Umformprozesse zeitlich überlappen.Advantageously, the explosive can be ignited at several points of the device with a time delay. If the time-delayed ignition on a single tool of the device, it can be generated multiple detonation fronts within a tool. The temporal offset allows a tuning of the time course of the individual detonation fronts within the tool. If the staggered ignition of different tools of the device, the energy beam z. B. ignite all the tools of the device sequentially. This helps to shorten the cycle times if the parallel forming processes overlap in time.

Prinzipiell sind beliebige Kombinationen der gleichzeitigen und der zeitversetzten Zündung an einem und/oder mehreren Werkzeugen der Vorrichtung möglich. So lässt sich das Verfahren gut an unterschiedliche Produktionsanforderungen anpassen. Die Grundidee, die Ausbreitung von Detonationsfronten über eine zeitlich variierbare Zündung an einer oder mehreren Stellen des Werkzeugs zu steuern und so das Umformergebnis zu beeinflussen, wäre auch unabhängig von der Art der Zündung, ob mit Energiestrahl oder anders, realisierbar.In principle, any combination of simultaneous and time-delayed ignition of one and / or more tools of the device are possible. This makes it easy to adapt the process to different production requirements. The basic idea of controlling the propagation of detonation fronts via a time-variable ignition at one or more points of the tool and thus influencing the forming result, would also be independent of the type of ignition, whether with energy beam or otherwise, feasible.

In einer günstigen Ausführungsform der Erfindung können mehrere Detonationsfronten innerhalb eines Werkzeugs erzeugt werden. Dadurch und insbesondere durch die zeitliche Steuerung des Verlaufs der Detonationsfronten, kann ein gutes Umformergebnis erzielt werden.In a favorable embodiment of the invention, multiple detonation fronts can be created within a tool. As a result, and in particular by the timing of the course of the detonation fronts, a good forming result can be achieved.

Vorteilhafterweise kann wenigstens je eine Detonationsfront innerhalb mehrerer Werkzeuge der Vorrichtung erzeugt werden. So lässt sich die Effektivität einer Zündvorrichtung mit Energiestrahl steigern.Advantageously, at least one respective detonation front can be generated within several tools of the device. Thus, the effectiveness of an ignition device with energy beam can be increased.

Der Energiestrahl kann in ein Zündrohr des Werkzeugs eingeleitet werden. So kann ein Teil des Werkzeugs, nämlich das Zündrohr, an die speziellen Anforderungen des Zünd- und Explosionsvorgangs angepasst werden.The energy beam can be introduced into an ignition tube of the tool. Thus, a part of the tool, namely the ignition tube, can be adapted to the special requirements of the ignition and explosion process.

Der Energiestrahl kann durch ein transparentes Medium in den Explosionsraum gelangen. Dies ist technisch gut realisierbar und gewährleistet ein gutes Auftreffen des Energiestrahls auf das Explosionsmittel. Ein Energiestrahlerzeuger lässt sich so außerhalb des Werkzeugs platzieren und ist vor den direkten Auswirkungen der Explosion im Inneren des Werkzeugs weitgehend geschützt.The energy beam can enter the explosion space through a transparent medium. This is technically well feasible and ensures a good impact of the energy beam on the explosive. An energy jet generator can thus be placed outside the tool and is largely protected from the direct effects of the explosion inside the tool.

Die Aufgabe wird erfindungsgemäß ferner gelöst durch die Merkmale des Anspruchs 7.The object is also achieved by the features of claim 7.

Der Energiestrahl gewährleistet eine gute Zündung des Explosionsmittels. Er ist technisch gut erzeugbar und kann Entfernungen schnell überwinden. Dadurch kann das Explosionsmittel mit guter zeitlicher Genauigkeit gezündet werden.The energy beam ensures good ignition of the explosive. It is technically easy to produce and can overcome distances quickly. As a result, the explosive can be ignited with good timing accuracy.

Der Energiestrahlerzeuger kann einen Laser aufweisen. Der Laser stellt eine technisch einfache Möglichkeit der Energiestrahlerzeugung dar. Er bietet einen gut gebündelten und somit gut positionierbaren Energie- bzw. Laserstrahl mit einstellbarer Energiemenge.The energy beam generator may comprise a laser. The laser represents a technically simple possibility of energy beam generation. It offers a well-bundled and thus easily positionable energy or laser beam with adjustable amount of energy.

Günstigerweise kann das Werkzeug wenigstens eine Einleitungsstelle aufweisen, welche für den Energiestrahl durchlässig ist. So kann der Energiestrahl in das Werkzeug dringen und das darin enthaltene Explosionsmittel zünden. Der Energiestrahlerzeuger ist so außerhalb des Werkzeugs anordenbar und damit weitgehend vor den direkten Auswirkungen der Explosion geschützt.Conveniently, the tool may have at least one point of introduction, which is permeable to the energy beam. Thus, the energy beam can penetrate into the tool and ignite the explosive contained therein. The energy jet generator can be arranged outside the tool and thus largely protected from the direct effects of the explosion.

In einer Variante der Erfindung kann die Einleitungsstelle wenigstens ein transparentes Medium aufweisen. Dieses eignet sich insbesondere für Laserstrahlen. Es gewährleistet eine gute Transmission des Energiestrahls bei relativ geringem Energieverlust.In a variant of the invention, the point of introduction can have at least one transparent medium. This is particularly suitable for laser beams. It ensures a good transmission of the energy beam with relatively little energy loss.

Günstigerweise kann das transparente Medium einen Glaseinsatz aufweisen. Glas ist ein günstiger und gut zu verarbeitender Werkstoff, welcher die obengenannten Vorteile bietet und ausreichend widerstandsfähig für die auftretenden Explosionskräfte ist.Conveniently, the transparent medium may have a glass insert. Glass is a cheap and easy to process material, which provides the above advantages and is sufficiently resistant to the explosive forces occurring.

Der transparente Medium bzw. der Glaseinsatz kann eine Dicke im Bereich von 5 bis 15 mm, vorzugsweise im Bereich von 7 bis 12 mm und insbesondere im Bereich von 9 bis 11 mm aufweisen. Diese Dicke hat sich in der Praxis als vorteilhaft erwiesen. Sie gewährleistet eine ausreichende Stabilität, um den Anforderungen durch die Explosion standzuhalten.The transparent medium or the glass insert may have a thickness in the range of 5 to 15 mm, preferably in the range of 7 to 12 mm and in particular in the range of 9 to 11 mm. This thickness has been in the Practice proven advantageous. It ensures sufficient stability to withstand the requirements of the explosion.

Das transparente Medium bzw. der Glaseinsatz kann einen Außendurchmesser von etwa 5 bis 15 mm, vorzugsweise 7 bis 12 mm und insbesondere von 9 bis 11 mm aufweisen. Es hat sich gezeigt, dass dieser Außendurchmesser eine ausreichend gute und schnelle Positionierung des Energiestrahls bei gleichzeitig guter Stabilität des Mediums erlaubt.The transparent medium or the glass insert may have an outer diameter of about 5 to 15 mm, preferably 7 to 12 mm and in particular 9 to 11 mm. It has been shown that this outer diameter allows a sufficiently good and fast positioning of the energy beam with at the same time good stability of the medium.

Vorteilhafterweise kann das transparente Medium linsenartig, konvex geformt sein. So lässt sich der Energiestrahl gut bündeln.Advantageously, the transparent medium can be lens-like, convex. This allows the energy beam to be well bundled.

In einer Variante der Erfindung kann das transparente Medium einen etwa viereckigen Querschnitt aufweisen. Dies gewährleistet eine gute Stabilität sowie gute Transmissionseigenschaften.In a variant of the invention, the transparent medium may have an approximately quadrangular cross-section. This ensures good stability and good transmission properties.

Vorteilhafterweise kann das transparente Medium einen achteckigen Querschnitt aufweisen. Je nach Ausformung des Achtecks lässt sich der Energiestrahl so bündeln.Advantageously, the transparent medium may have an octagonal cross-section. Depending on the shape of the octagon, the energy beam can be bundled in this way.

In einer weiteren Ausführungsform der Erfindung kann das transparente Medium eine Fassung aufweisen, welche Kupfer enthält. Es hat sich gezeigt, dass Kupferlegierungen, insbesondere Kupfer-Beryllium-Legierungen, eine ausreichend gute Stabilität und gute Dichtungseigenschaften für diesen Anwendungsfall bieten.In a further embodiment of the invention, the transparent medium may comprise a socket containing copper. It has been found that copper alloys, in particular copper-beryllium alloys, provide sufficiently good stability and good sealing properties for this application.

Günstigerweise kann das transparente Medium mit einer Dichtung in dem Werkzeug angeordnet sein, welche den Explosionsraum gegenüber der Umgebung abdichtet. So ist die Umgebung vor der Explosion und den Explosionsprodukten geschützt.Conveniently, the transparent medium can be arranged with a seal in the tool, which seals the explosion space from the environment. This protects the environment from explosion and explosion products.

In einer Variante der Erfindung kann das Werkzeug mehrere Einleitungsstellen aufweisen. So kann das Explosionsmittel an mehreren Stellen des Werkzeugs gleichzeitig und/oder zeitversetzt gezündet werden. So können z.B. mehrere Detonationsfronten in dem Werkzeug erzeugt werden.In a variant of the invention, the tool can have a plurality of introduction points. Thus, the explosive can be ignited at several points of the tool simultaneously and / or with a time delay. For example, several detonation fronts can be created in the tool.

Bei einer vorteilhaften Ausführungsform der Erfindung können mehrere Werkzeuge mit mindestens je einer Einleitungsstelle vorgesehen sein. Dadurch können mehrere, eventuell auch unterschiedliche Werkzeuge der Vorrichtung gleichzeitig oder zeitversetzt gezündet werden. Überlappen sich die dabei entstehenden parallelen Umformprozesse zeitlich, kann so die Effizienz der Vorrichtung erhöht werden.In an advantageous embodiment of the invention, several tools can be provided with at least one introduction point. As a result, several, possibly even different tools of the device can be ignited simultaneously or with a time delay. If the resulting parallel forming processes overlap in time, the efficiency of the device can be increased.

Günstigerweise kann wenigstens eine Umlenkanordnung im Strahlengang des Energiestrahlenerzeugers vorgesehen sein, mittels welcher der Energiestrahl zu wenigstens einer Zündstelle lenkbar ist. Dadurch lässt sich der Energiestrahl technisch einfach, schnell und gut positionieren.Conveniently, at least one deflection arrangement can be provided in the beam path of the energy beam generator, by means of which the energy beam can be directed to at least one ignition point. This makes the energy beam technically easy, fast and easy to position.

Die Umlenkanordnung kann eine Spiegelanordnung sein. Diese eignet sich insbesondere für Laserstrahlen und bietet die obengenannten Vorteile einer Umlenkanordnung.The deflection arrangement may be a mirror arrangement. This is particularly suitable for laser beams and offers the above-mentioned advantages of a deflection arrangement.

Die Umlenkanordnung kann wenigstens ein für den Energiestrahl teildurchlässiges Spiegelelement aufweisen. So lässt sich der Energiestrahl technisch einfach in mehrere Strahlen aufteilen.The deflecting arrangement can have at least one mirror element that is partially transparent to the energy beam. This makes it technically easy to divide the energy beam into several beams.

Im Folgenden werden Ausführungsformen der erfindungsgemäßen Vorrichtung anhand der folgenden Zeichnungen beschrieben. Dabei zeigen:

Fig. 1
eine Vorrichtung zum Explosionsumformen gemäß einer ersten Ausführungsform der Erfindung,
Fig. 2
einen Schnitt II-II durch das Werkzeug der Vorrichtung aus Fig. 1,
Fig. 3a
eine Vorrichtung gemäß einer zweiten Ausführungsform der Erfindung, und
Fig. 3b
eine Vorrichtung gemäß einer dritten Ausführungsform der Erfindung.
Embodiments of the device according to the invention will now be described with reference to the following drawings. Showing:
Fig. 1
an explosion-shaping apparatus according to a first embodiment of the invention,
Fig. 2
a section II-II through the tool of the device Fig. 1 .
Fig. 3a
a device according to a second embodiment of the invention, and
Fig. 3b
a device according to a third embodiment of the invention.

Fig. 1 zeigt eine Vorrichtung zum Explosionsumformen gemäß einer ersten Ausführungsform der Erfindung. Die Vorrichtung 1 weist ein Werkzeug 2 und einen Energiestrahlerzeuger 3 auf. Fig. 1 shows an apparatus for explosion forming according to a first embodiment of the invention. The device 1 has a tool 2 and an energy beam generator 3.

Das Werkzeug 2 ist in dieser Ausführungsform der Erfindung mehrteilig und weist ein Umformmittel 4 und ein Zündrohr 5 auf. In dem Umformmittel 4 ist ein hier durch eine gepunktete Linie angedeutetes Werkstück 18 angeordnet. Im Inneren des Zündrohrs 5 ist eine Zündkammer 6 vorgesehen. In ihr befindet sich ein Explosionsmittel 7.The tool 2 is in this embodiment of the invention in several parts and has a forming means 4 and an ignition tube 5 on. In the forming 4 a here indicated by a dotted line workpiece 18 is arranged. Inside the ignition tube 5, an ignition chamber 6 is provided. In it there is an explosive 7.

In dieser Ausführungsform ist als Explosionsmittel 7 ein explosives Gasgemisch, Knallgas, vorgesehen, welches über den Anschluss 8 in die Zündkammer 6 eingebracht werden kann. In anderen Ausführungsformen der Erfindung können jedoch auch andere Explosionsmittel in gasförmiger Form zum Einsatz kommen. Der Anschluss 8 ist dann entsprechend dem jeweiligen Explosionsmittel ausgebildet.In this embodiment, an explosive gas mixture, explosive gas, is provided as the explosive 7, which can be introduced into the ignition chamber 6 via the connection 8. However, in other embodiments of the invention, other explosive means may also be used in gaseous form. The terminal 8 is then formed according to the respective explosive means.

Der Energiestrahlerzeuger 3 kann wahlweise einen Energiestrahl 12 erzeugen und ist in dieser Ausführungsform ein Lasergerät, welches um seine vertikale Achse 9 drehbar auf einem Fuß 10 gelagert ist. Es wird über eine Leitung 11 mit Energie versorgt und kann bei Bedarf einen Energie-, in diesem Fall einen Laserstrahl 12 erzeugen.The energy beam generator 3 can optionally generate an energy beam 12 and in this embodiment is a laser device, which is mounted rotatably about a vertical axis 9 on a foot 10. It is powered via a line 11 with energy and can generate an energy, in this case, a laser beam 12, if necessary.

Die Wandung 13 des Zündrohrs 5 weist eine für den Energiestrahl 12 durchlässige Einleitungsstelle 14 auf. Im Bereich der Einleitungsstelle 14 ist ein transparentes Medium 15 vorgesehen, welches für den Energiestrahl 12 wenigstens teilweise durchlässig ist. In dieser Ausführungsform der Erfindung weist das transparente Medium 15 einen Glaseinsatz 19 auf, welcher in Fig. 2 genauer dargestellt ist.The wall 13 of the ignition tube 5 has a permeable to the energy beam 12 discharge point 14. In the region of the introduction point 14, a transparent medium 15 is provided, which is at least partially permeable to the energy beam 12. In this embodiment of the invention, the transparent medium 15 has a glass insert 19, which in Fig. 2 is shown in more detail.

Das Lasergerät 3 ist so angeordnet, dass der Laserstrahl 12 durch das transparente Medium 15 in die Zündkammer 6 des Zündrohrs 5 dringen kann. Dadurch wird das Explosionsmittel 7 in der Zündkammer 6 gezündet.The laser device 3 is arranged so that the laser beam 12 can penetrate through the transparent medium 15 into the ignition chamber 6 of the ignition tube 5. As a result, the explosive 7 is ignited in the ignition chamber 6.

Optional kann das Werkzeug 2 der Vorrichtung 1 auch mehrere Einleitungsstellen 14 für den Energiestrahl 12 bzw. Zündstellen aufweisen. Die Vorrichtung 1 kann, wie hier gestrichelt dargestellt ist, z.B. ein weiteres Zündrohr 5' aufweisen, welches in dieser Ausführungsform analog des ersten Zündrohrs 5 ausgebildet ist. Es weist dementsprechend auch eine mit einem Zündmittel 7 gefüllte Zündkammer 6' ein transparentes Medium 15' und einen Anschluss 8' auf.Optionally, the tool 2 of the device 1 can also have a plurality of introduction points 14 for the energy beam 12 or ignition points. The device 1 can, as dashed lines here is shown, for example, a further ignition tube 5 ', which is formed in this embodiment analogous to the first ignition tube 5. Accordingly, it also has an ignition chamber 6 'filled with an ignition means 7, a transparent medium 15' and a connection 8 '.

Durch Drehen des Lasergeräts 3 um die vertikale Achse 9 kann das Lasergerät 3 aus seiner ersten Position 16, in welcher der Laserstrahl 12 in die Zündkammer 6 des ersten Zündrohrs 5 eindringt, in eine zweite Position 17 gebracht werden, in welcher der Laserstrahl 12 durch das transparente Medium 15' in die Zündkammer 6' des zweiten Zündrohrs 5' fällt, wie in Fig. 1 gestrichelt dargestellt. So kann das Zündmittel 7 in den Zündrohren 5, 5' z.B. nacheinander durch das Lasergerät 3 gezündet werden.By rotating the laser device 3 about the vertical axis 9, the laser device 3 can be brought from its first position 16, in which the laser beam 12 enters the ignition chamber 6 of the first ignition tube 5, in a second position 17, in which the laser beam 12 through the transparent medium 15 'in the ignition chamber 6' of the second ignition tube 5 'falls, as in Fig. 1 shown in dashed lines. Thus, the ignition means 7 in the ignition tubes 5, 5 ', for example, be ignited successively by the laser device 3.

Das Werkstück 18 kann in diesem Fall z.B. zwischen den beiden Zündrohren 5, 5' angeordnet sein, wie in Fig. 1 durch eine gepunktete und eine gestrichelte Linie angedeutet.The workpiece 18 may be arranged in this case, for example between the two ignition tubes 5, 5 ', as in Fig. 1 indicated by a dotted and a dashed line.

Fig. 2 zeigt einen Schnitt II-II durch die für den Energiestrahl 12 durchlässige Einleitungsstelle 14 des Zündrohrs 5. Die in Fig. 2 verwendeten Bezugszeichen bezeichnen dieselben Teile wie in Fig. 1, so dass diesbezüglich auf die Beschreibung der Fig. 1 verwiesen wird. Fig. 2 shows a section II-II through the energy beam 12 permeable inlet point 14 of the ignition tube 5. The in Fig. 2 Reference numerals used denote the same parts as in FIG Fig. 1 , so in this regard to the description of the Fig. 1 is referenced.

Das transparente Medium 15 weist in dieser Ausführungsform der Erfindung einen runden Glaseinsatz 19 mit einem viereckigen Querschnitt auf. Der Außendurchmesser und die Dicke des Glaseinsatzes sind annähernd gleich groß. In dieser Ausführungsform beträgt der Durchmesser wie auch die Dicke des Glaseinsatzes 19 10 mm.The transparent medium 15 in this embodiment of the invention has a round glass insert 19 with a quadrangular cross-section. The outer diameter and the thickness of the glass insert are approximately equal. In this embodiment, the diameter as well as the thickness of the glass insert 19 is 10 mm.

In anderen Ausführungsformen der Erfindung kann dieses Verhältnis jedoch deutlich variieren. Die Abmaße des Glaseinsatzes und seine äußere Form können dem jeweiligen Anwendungsfall angepasst werden. So kann der Querschnitt durch den Glaskörper z.B. auch achteckig sein. Zudem kann die zündkammerseitige Fläche 20 und/oder die ihr gegenüberliegende Fläche 21 des Glaseinsatzes 19 gewölbt sein, so dass sich eine annähernd linsenartige Form des Glaseinsatzes 19 ergibt. Auch das Material des Einsatzes 19 kann je nach Anwendungsfall variieren. Wird, wie hier, ein Laser als Energiestrahlerzeuger verwendet, sind z.B. druck- und hitzebeständige aber dennoch lichtdurchlässige Kunststoffe denkbar.However, in other embodiments of the invention, this ratio may vary significantly. The dimensions of the glass insert and its external shape can be adapted to the particular application. For example, the cross section through the glass body can also be octagonal. In addition, the ignition chamber-side surface 20 and / or its opposite surface 21 of the glass insert 19 may be curved so that an approximately lens-like shape of the glass insert 19 results. Also, the material of the insert 19 may vary depending on the application. If, as here, a laser used as an energy beam generator, for example, pressure and heat resistant, yet translucent plastics are conceivable.

Das transparente Medium 15 weist außerdem eine Fassung 22 auf, in welcher der Glaseinsatz 19 angeordnet ist. Die Fassung 22 ist in dieser Ausführungsform der Erfindung aus einer Kupfer-Beryllium-Legierung gefertigt. Diese ist stabil und hält den dynamisch, schlagartig auftretenden relativ hohen Belastungen durch die Explosion gut stand. Alternativ kann die Fassung 22 jedoch auch aus einer anderen Kupferlegierung oder einem beliebigen anderen Werkstoff gefertigt werden, der den hohen Belastungen durch die Explosion standhält. Ihre Wandung 23 weist einen L-artigen Querschnitt auf. Die Innenkontur der Fassung 22 entspricht dabei in etwa den Außenabmaßen des Glaseinsatzes 19.The transparent medium 15 also has a socket 22 in which the glass insert 19 is arranged. The socket 22 is made in this embodiment of the invention from a copper-beryllium alloy. This is stable and holds the dynamic, abruptly occurring relatively high loads from the explosion well. Alternatively, however, the socket 22 may be made of a different copper alloy or any other material which will withstand the high explosive loads. Its wall 23 has an L-like cross-section. The inner contour of the socket 22 corresponds approximately to the outer dimensions of the glass insert 19th

Das transparente Medium 15 ist mit einer Dichtung 24 in dem Zündrohr 5 angeordnet, welche die Zündkammer 6 im Inneren des Zündrohrs 5 gegenüber der Umgebung dichtet. Die Wandung 13 des Zündrohrs 5 und die Fassung 22 bilden dabei eine Presspassung.The transparent medium 15 is arranged with a seal 24 in the ignition tube 5, which seals the ignition chamber 6 in the interior of the ignition tube 5 from the environment. The wall 13 of the ignition tube 5 and the socket 22 form a press fit.

Obwohl der Aufbau der erfindungsgemäßen Vorrichtung hier anhand eines einzelnen Werkzeugs beschrieben ist, kann die Vorrichtung 1 in anderen Ausführungen der Erfindung auch mehrere Werkzeuge 2 aufweisen, wie in den Fig. 3a, 3b beispielhaft dargestellt.Although the structure of the device according to the invention is described here with reference to a single tool, the device 1 in other embodiments of the invention may also comprise a plurality of tools 2, as in FIGS Fig. 3a . 3b exemplified.

Die Fig. 3a und 3b zeigen mögliche Ausführungsformen einer erfindungsgemäßen Vorrichtung mit mehreren Werkzeugen. Die Werkzeuge 2a bis 2d entsprechen dabei dem in Fig. 1 gezeigten und beschriebenen Werkzeug 2. Die Fig. 3a und 3b zeigen lediglich unterschiedliche Möglichkeiten auf, eine derartige Vorrichtung zu realisieren. Die Erfindung ist keinesfalls auf die in diesen Figuren gezeigten Ausführungsformen beschränkt. Vielmehr können die in den Fig. 3a und 3b gezeigten Funktionsprinzipien in beliebiger Weise je nach Anwendungsfall auch miteinander kombiniert werden.The Fig. 3a and 3b show possible embodiments of a device according to the invention with a plurality of tools. The tools 2a to 2d correspond to the in Fig. 1 shown and described tool 2. The Fig. 3a and 3b merely show different possibilities to realize such a device. The invention is by no means limited to the embodiments shown in these figures. Rather, those in the Fig. 3a and 3b shown operating principles in any way, depending on the application also combined.

Fig. 3a zeigt eine schematische Darstellung einer Vorrichtung gemäß einer zweiten Ausführungsform der Erfindung. Die in Fig. 3a verwendeten Bezugszeichen bezeichnen dieselben Teile wie in den Fig. 1 und 2, so dass diesbezüglich auf die Beschreibung der Fig. 1 und 2 verwiesen wird. Die in Fig. 3a gezeigte Vorrichtung 1 weist mehrere Werkzeuge 2 und mehrere Energiestrahlenerzeuger bzw. Lasergeräte 3 auf. Die Ausbildung dieser Geräte entspricht der in den Fig. 1 und 2 gezeigten Ausbildung, mehrfach vorkommende, gleiche Bauteile werden daher mit dem Zusatz a, b, usw. versehen. Fig. 3a shows a schematic representation of an apparatus according to a second embodiment of the invention. In the Fig. 3a used reference numerals denote the same parts as in the Fig. 1 and 2 , so in this regard to the description of the Fig. 1 and 2 is referenced. In the Fig. 3a shown device 1 has a plurality of tools 2 and a plurality of energy beam generators or laser devices 3. The training of these devices corresponds to that in the Fig. 1 and 2 shown training, multiple occurring, same components are therefore provided with the addition a, b, etc.

Die Vorrichtung 1 weist hier vier Werkzeuge 2a bis 2d und vier Lasergeräte 3a bis 3d auf. Die Werkzeuge 2a bis 2d sind in etwa auf einem hier gepunktet angedeuteten Kreis 30 angeordnet. Auch die Lasergeräte 3a bis 3d sind in etwa auf einem Kreis 31 angeordnet, der etwa konzentrisch innerhalb des Kreises 30 liegt. Die Lasergeräte 3a bis 3d sind in Relation zu den Werkzeugen 2a bis 2d so angeordnet, dass je eine der Laserstrahlen 12a bis 12d durch das transparente Medium 15 je eines der Werkzeuge 3a bis 3d in die Zündkammer 6a bis 6d dringen und dort das Explosionsmittel 7 zünden kann.The device 1 here has four tools 2a to 2d and four laser devices 3a to 3d. The tools 2a to 2d are arranged approximately on a dotted circle 30 indicated here. Also, the laser devices 3a to 3d are arranged approximately on a circle 31, which lies approximately concentrically within the circle 30. The laser devices 3a to 3d are arranged in relation to the tools 2a to 2d so that each one of the laser beams 12a to 12d penetrate through the transparent medium 15 each one of the tools 3a to 3d in the ignition chamber 6a to 6d and there ignite the explosive 7 can.

Alternativ können bei der in Fig. 3a gewählten Anordnung die beiden Lasergeräte 3a und 3b auch durch ein einziges, hier strichpunktiert dargestelltes Lasergerät ersetzt werden, welches analog Fig. 1 um seine vertikale Achse 9 drehbar gelagert ist. Durch Drehen um die Achse 9 könnte dieses Lasergerät sowohl die Position des Lasergeräts 3a als auch die Position des Lasergeräts 3b einnehmen. Gleiches gilt für die Lasergeräte 3c und 3d, welche analog ebenfalls durch ein einzelnes um die vertikale Achse 9 drehbares Lasergerät ersetzbar sind.Alternatively, at the in Fig. 3a selected arrangement, the two laser devices 3a and 3b are replaced by a single, here shown in phantom laser device, which analog Fig. 1 is mounted rotatably about its vertical axis 9. By rotating about the axis 9, this laser device could occupy both the position of the laser device 3a and the position of the laser device 3b. The same applies to the laser devices 3c and 3d, which are likewise replaceable by a single laser device rotatable about the vertical axis 9.

Fig. 3b zeigt eine schematische Darstellung einer Vorrichtung gemäß einer dritten Ausführungsform der Erfindung. Die in den Fig. 1 und 2 verwendeten Bezugszeichen bezeichnen dieselben Teile wie in Fig. 3b, so dass diesbezüglich auf die Beschreibung der Fig. 1 und 2 verwiesen wird. Die in Fig. 3a gezeigte Vorrichtung 1 weist mehrere Werkzeuge 2 und Energie- bzw. Laserstrahlenerzeuger 3 auf. Die Ausbildung der einzelnen Werkzeuge 2a bis 2d und des Energiestrahlenerzeugers 3 entspricht dem in den Fig. 1 und 2 gezeigten Werkzeug 2 und Energiestrahlenerzeuger 3. Fig. 3b shows a schematic representation of a device according to a third embodiment of the invention. The in the Fig. 1 and 2 Reference numerals used denote the same parts as in FIG Fig. 3b , so in this regard to the description of the Fig. 1 and 2 is referenced. In the Fig. 3a shown device 1 has a plurality of tools 2 and energy or laser beam generator 3. The formation of the individual tools 2a to 2d and the energy beam generator 3 corresponds to that in the Fig. 1 and 2 shown tool 2 and energy beam generator. 3

Die Vorrichtung 1 weist hier zusätzlich eine Umlenkanordnung 25 für den Energie- bzw. Laserstrahl 12 auf. In diesem Fall ist die Umlenkanordnung 25 eine Spiegelanordnung. Sie weist ein zentrales, polyederartiges Element 27 und mehrere, in diesem Fall drei, weitere Spiegelelemente 28 auf. Die Flächen des zentralen Elementes 27 weisen ebenfalls Spiegel 29 auf. In dieser Ausführungsform der Erfindung sind vier Flächen des zentralen Elementes 27 mit Spiegeln 29 versehen. Wenigstens einer der Spiegel 29 kann dabei teildurchlässig für den Energie- bzw. Laserstrahl 12 sein. Hier sind drei der Spiegel 29 teildurchlässig. Ein teildurchlässiger Spiegel 29 reflektiert einen vorbestimmten Teil des auf ihn treffenden Laserlichts bzw. -strahls 12. Der restliche Teil des Laserstrahls 12 geht nahezu unverändert durch den teildurchlässigen Spiegel hindurch. So lässt sich der aus dem Lasergerät 3 emittierte Laserstrahl 12 aufspalten.The device 1 here additionally has a deflection arrangement 25 for the energy or laser beam 12. In this case, the deflection arrangement 25 is a mirror arrangement. It has a central, polyhedron-like element 27 and a plurality, in this case three, further mirror elements 28. The surfaces of the central element 27 also have mirrors 29. In this embodiment of the invention, four surfaces of the central element 27 are provided with mirrors 29. At least one of the mirrors 29 may be partially transparent to the energy or laser beam 12. Here are three of the mirror 29 partially transparent. A partially transmissive mirror 29 reflects a predetermined part of the laser light or beam 12 impinging on it. The remaining part of the laser beam 12 passes through almost unchanged the partially transmissive mirror. Thus, the laser beam 12 emitted from the laser device 3 can be split.

Das zentrale, polyederartige Element 27 ist um seine vertikale Achse 33 drehbar, etwa im Zentrum eines, gepunktet angedeuteten, Kreises 26 angeordnet, während die Spiegelelemente 28 in etwa auf dem Kreis 26 angeordnet sind. Auch die Spiegelelemente 28 sind um ihre jeweilige vertikale Achse 32 drehbar gelagert. Die einzelnen Teile 27, 28, 29 der Spiegelanordnung 25 sind dabei in Relation zu dem Lasergerät 3 und den Werkzeugen 2a bis 2d so angeordnet, dass der Laserstrahl 12 je nach Ausrichtung der Spiegel 28 und 29 wahlweise durch das transparente Medium 15 eines der Werkzeuge 2a bis 2d zu einer Zündstelle in der jeweiligen Zündkammer 6a bis 6d geleitet wird.The central, polyhedron-like element 27 is rotatable about its vertical axis 33, arranged approximately in the center of a circle 26 indicated dotted, while the mirror elements 28 are arranged approximately on the circle 26. The mirror elements 28 are rotatably mounted about their respective vertical axis 32. The individual parts 27, 28, 29 of the mirror assembly 25 are arranged in relation to the laser device 3 and the tools 2a to 2d so that the laser beam 12 depending on the orientation of the mirror 28 and 29 optionally through the transparent medium 15 of the tools 2a until 2d is conducted to an ignition point in the respective ignition chamber 6a to 6d.

Obwohl die Umlenk- bzw. Spiegelanordnung 25 hier mit einem zentralen, polyederartigen Element 27 und mehreren Spiegelelementen 28 dargestellt und beschrieben ist, kann die Umlenkanordnung 25 in anderen Ausführungsformen der Erfindung auch völlig anders ausgebildet sein. Die Anzahl und Position der Spiegelelemente 28 kann je nach Anwendungsfall variieren. Die einzelnen Elemente 27, 28, 29 der Umlenkanordnung 25 müssen auch nicht, wie hier gezeigt, zwangsläufig auf einem bzw. innerhalb eines Kreises 26 angeordnet sein. Das zentrale Element 27, welches hier polyederartig geformt ist, kann auch eine andere z.B. scheibenartige Form aufweisen oder ganz entfallen. Zudem können die einzelnen Elemente 27, 28, 29 der Umlenkanordnung 25 auch gegeneinander kippbar sein. So lässt sich z.B. die Höhe des Laserstrahls 12 über dem Untergrund, auf welchem die Vorrichtung steht, variieren. Hierfür können die einzelnen Elemente 27, 28, 29 der Umlenkanordnung 25 mit Dreh- und/oder Kugelgelenken versehen sein. In der Praxis sind auch andere Ausführungsformen der Umlenkanordnung 25 denkbar. So kann der Laserstrahl 12 z.B. auch mittels oder mehrerer Glasfaserelemente zu einer bzw. mehreren Einleitungsstellen 14 in einem Werkzeug 3 geleitet werden. Auch die Anordnung und Ausbildung der einzelnen Werkzeuge 2a bis 2d kann von der hier gezeigten abweichen und je nach Anwendungsfall variieren.Although the deflection or mirror arrangement 25 is shown and described here with a central, polyhedron-like element 27 and a plurality of mirror elements 28, the deflection arrangement 25 can also be designed completely differently in other embodiments of the invention. The number and position of the mirror elements 28 may vary depending on the application. The individual elements 27, 28, 29 of the deflection arrangement 25 also do not necessarily have to be arranged on or inside a circle 26, as shown here. The central element 27, which here is polyhedron-shaped, may also have another, e.g. have disc-like shape or omitted altogether. In addition, the individual elements 27, 28, 29 of the deflection arrangement 25 can also be tilted relative to one another. Thus, for example, the height of the laser beam 12 above the ground on which the device stands varies. For this purpose, the individual elements 27, 28, 29 of the deflection assembly 25 may be provided with rotary and / or ball joints. In practice, other embodiments of the deflection assembly 25 are conceivable. Thus, the laser beam 12 may be e.g. also be guided by means of one or more glass fiber elements to one or more discharge points 14 in a tool 3. The arrangement and design of the individual tools 2a to 2d may differ from the one shown here and vary depending on the application.

Im Folgenden wird die Funktionsweise der in den Fig. 1 bis 3b dargestellten Ausführungsbeispiele erläutert.The following is the operation of the in the Fig. 1 to 3b illustrated embodiments explained.

Die Funktionsweise wird anhand der Fig. 1 und 2 zunächst für eine Vorrichtung mit einem Werkzeug und einem Energiestrahlerzeuger beschrieben. Der Energiestrahlerzeuger bzw. das Lasergerät 3 der Vorrichtung 1 in Fig. 1 wird so positioniert, dass der Laserstrahl 12 durch das transparente Medium 15 in der Wandung 13 des Zündrohrs 5 in die Zündkammer 6 fallen kann.The functionality is based on the Fig. 1 and 2 first described for a device with a tool and an energy jet generator. The energy jet generator or the laser device 3 of the device 1 in FIG Fig. 1 is positioned so that the laser beam 12 can fall through the transparent medium 15 in the wall 13 of the ignition tube 5 in the ignition chamber 6.

Anschließend wird das Werkzeug 2, in diesem Fall das Zündrohr 5 des Werkzeugs 2, mit dem Explosionsmittel 7 befüllt. Hierfür wird über den Anschluss 8 ein Explosionsmittel, z.B. Knallgas, in die Zündkammer 6 des Zündrohrs 5 geleitet. Hat sich eine vorbestimmte Menge des Explosionsmittels 7 in der Zündkammer 5 gesammelt, wird der Anschluss 8 geschlossen.Subsequently, the tool 2, in this case the ignition tube 5 of the tool 2, is filled with the explosive 7. For this purpose, an explosion means, e.g. Oxyhydrogen, passed into the ignition chamber 6 of the ignition tube 5. Has a predetermined amount of the explosive 7 collected in the ignition chamber 5, the terminal 8 is closed.

Zum Zünden des Explosionsmittels 7 wird in dem Energiestrahlerzeuger bzw. dem Lasergerät 3 ein Energiestrahl, in diesem Fall ein Laserstrahl, 12 erzeugt. Der von dem Lasergerät 3 ausgehende Laserstrahl 12 trifft auf das transparente Medium 15, durchdringt dieses und trifft in der Zündkammer 6 auf das Explosionsmittel 7.To ignite the explosive 7, an energy beam, in this case a laser beam 12, is generated in the energy beam generator or the laser device 3. The emanating from the laser device 3 laser beam 12 strikes the transparent medium 15, penetrates this and strikes in the ignition chamber 6 on the explosive 7th

Fig. 2 stellt diesen Vorgang genauer dar. Der Laserstrahl 12 trifft hier auf die äußere Fläche 21 des Glaseinsatzes 19 des transparenten Mediums 15. Aufgrund der Beschaffenheit und der Form des Glaseinsatzes 19 durchdringt der Laserstrahl den Glaseinsatz 19 weitgehend ungehindert und ohne große Ablenkung und tritt auf der zündkammerseitigen Fläche 19 wieder aus dem Glaseinsatz 19 aus und damit in die Zündkammer 6 des Zündrohrs 5 ein. Dort trifft der Laserstrahl 12 auf das Explosionsmittel 7 und entzündet dieses im Bereich der Zündstelle 36. Fig. 2 The laser beam 12 strikes here on the outer surface 21 of the glass insert 19 of the transparent medium 15. Due to the nature and shape of the glass insert 19, the laser beam penetrates the glass insert 19 largely unhindered and without much deflection and occurs on the ignition chamber side Surface 19 again from the glass insert 19 and thus in the ignition chamber 6 of the ignition tube 5 a. There, the laser beam 12 impinges on the explosive 7 and ignites it in the region of the ignition point 36.

Je nach Form des Glaseinsatzes 19 lässt sich der Laserstrahl 12 verändern. Durch einen linsenartig geformten Glaseinsatz 19 mit gekrümmter äußerer Fläche 21 und/oder gekrümmter zündkammerseitigen Fläche 20 lässt sich der Laserstrahl 12 z.B. im Fall einer konvexen Wölbung weiter bündeln und so auf eine bestimmte Zündstelle fokussieren. Mit einer konkaven Wölbung lässt sich der Laserstrahl 12 dagegen aufspreizen. Sind die Flächen 20, 21 gegeneinander geneigt, wie dies z.B. bei einem polyederartigen oder achteckigen Querschnitt der Fall ist, lässt sich die Ausbreitungsrichtung des Laserstrahls 12 ablenken.Depending on the shape of the glass insert 19, the laser beam 12 can be changed. By a lens-like shaped glass insert 19 with a curved outer surface 21 and / or curved ignition chamber side surface 20, the laser beam 12 can, for example in the case of a convex curvature continue to focus and focus on a specific ignition point. With a concave curvature, however, the laser beam 12 can be spread apart. If the surfaces 20, 21 are inclined relative to one another, as is the case, for example, with a polyhedral or octagonal cross-section, the direction of propagation of the laser beam 12 can be deflected.

Bei der daraus resultierenden Explosion des Explosionsmittels 7 entsteht innerhalb kurzer Zeit eine relativ große Druckänderung, welche relativ große Kräfte auf das Zündrohr 5 und das transparente Medium 15 ausübt, sowie eine relativ große Temperaturerhöhung. Die Schnittstelle des transparenten Mediums mit dem Zündrohr 5 wird auch während dieser schlagartigen, dynamischen Belastung durch die Dichtung 24 gedichtet. Auch die Schnittstelle zwischen dem Glaseinsatz 19 und der Fassung 22 wird durch die Dichtung 24 gedichtet. Dies gewährleistet zum einen einen guten Druckaufbau in dem Zündrohr 5 und schützt zum anderen die Umgebung, außerhalb des Werkzeugs 2 vor den direkten Auswirkungen der Explosion, wie Druck- und Temperaturänderungen, sowie vor den eventuell schädlichen Explosionsprodukten, wie z.B. Abgasen.In the resulting explosion of the explosive 7 is formed within a short time a relatively large pressure change, which exerts relatively large forces on the ignition tube 5 and the transparent medium 15, and a relatively large increase in temperature. The interface of the transparent medium with the ignition tube 5 is also sealed during this sudden, dynamic loading by the seal 24. The interface between the glass insert 19 and the socket 22 is sealed by the seal 24. This, on the one hand, ensures good pressure build-up in the ignition tube 5 and, on the other hand, protects the environment outside of the tool 2 from the direct effects of the explosion, such as pressure and temperature changes, as well as from potentially harmful explosive products, e.g. Exhaust gases.

Die bei der Explosion entstehende Druck- oder Detonationsfront breitet sich entlang des Zündrohrs 5 aus, gelangt so in das Werkstück 18 und presst dieses in das Formmittel 4. Die Detonationsfront breitet sich prinzipiell von der Zündstelle 36 ausgehend sphärisch aus. In diesem Fall heißt das, dass sich ein Teil 34 der Detonationsfront ausgehend von der Zündstelle 36 in Richtung des Werkstücks 18 bewegt. Ein anderer Teil 35 der Detonationsfront bewegt sich dagegen von dem Werkstück 18 weg, wie in Fig. 2 gezeigt. Je nach Ausbildung des Zündrohrs 5 und der Position der Einleitungs- 14 bzw. Zündstelle 36 lässt sich der Verlauf dieses zweiten Teils 35 der Detonationsfront steuern.The resulting in the explosion pressure or detonation front propagates along the ignition tube 5, so enters the workpiece 18 and presses this into the molding means 4. The detonation front propagates in principle starting from the ignition point 36 from spherical. In this case, this means that a part 34 of the detonation front moves from the ignition point 36 in the direction of the workpiece 18. On the other hand, another part 35 of the detonation front moves away from the workpiece 18, as in FIG Fig. 2 shown. Depending on the design of the ignition tube 5 and the position of the inlet 14 or ignition point 36, the course of this second part 35 of the detonation front can be controlled.

Ist das Zündrohr 5 so ausgebildet, dass dieser Teil der Detonationsfront reflektiert wird, wenn er am Ende des Zündrohrs 5 angelangt ist, lassen sich so z.B. zwei Detonationsfronten 34, 35 erzeugen, welche sich zeitlich versetzt über das Werkstück 18 hinwegbewegen. Der zeitliche Versatz der beiden Detonationsfronten lässt sich über die Position der Zündstelle 36 bzw. der Einleitungsstelle 14 und die Form des Zündrohrs 5 steuern.If the ignition tube 5 is designed such that this part of the detonation front is reflected when it has reached the end of the ignition tube 5, it is possible, for example, to generate two detonation fronts 34, 35, which move over the workpiece 18 offset in time. The temporal offset of the two detonation fronts can be controlled via the position of the ignition point 36 or the point of introduction 14 and the shape of the ignition tube 5.

Weist das Werkzeug 2 dagegen mehrere Einleitungs- 14 und Zündstellen 36 auf, wie in Fig. 1 gestrichelt angedeutet, kann die Zündung des Explosionsmittels 7 an mehreren Stellen des Werkzeugs erfolgen. Hierfür wird das Lasergerät 3, nachdem es einen ersten Laserstrahl 12 in die Zündkammer 6 des ersten Zündrohrs 5 abgegeben und damit das Explosionsmittel 7 im ersten Zündrohr 5 gezündet hat, um die vertikale Achse 9 aus einer ersten Position 16 in seine zweite Position 17 gedreht. Anschließend wird ein weiterer Laserstrahl 12 generiert, welcher durch das transparente Medium 15' des zweiten Zündrohrs 5' in die zweite Zündkammer 6' fällt. Dort trifft er auf das Explosionsmittel 7 und zündet dieses. So lassen sich mehrere, in diesem Fall zwei Detonationsfronten innerhalb eines Werkzeugs erzeugen.In contrast, the tool 2 has a plurality of introduction 14 and ignition points 36, as in Fig. 1 indicated by dashed lines, the ignition of the explosive 7 can take place at several points of the tool. For this purpose, the laser device 3, after it has delivered a first laser beam 12 into the ignition chamber 6 of the first ignition tube 5 and thus ignited the explosive 7 in the first ignition tube 5, rotated about the vertical axis 9 from a first position 16 to its second position 17. Subsequently, a further laser beam 12 is generated, which through the transparent medium 15 'of the second ignition tube 5' in the second ignition chamber 6 'falls. There he meets the explosive 7 and ignites it. Thus, several, in this case two detonation fronts within a tool can be created.

Neben der zeitlichen Steuerung der beiden Laserimpulse lässt sich der Verlauf der beiden Detonationsfronten z.B. durch die geeignete Anordnung der Einleitungs- 14 bzw. Zündstellen 36 beeinflussen. In der in Fig. 1 gezeigten Ausführungsform der Erfindung entstehen so zwei Detonationsfronten, die sich aufeinander zu bewegen und sich an einer bestimmten Stelle im Werkzeug 2 treffen.In addition to the timing of the two laser pulses, the course of the two detonation fronts can be influenced, for example, by the suitable arrangement of the inlet 14 or ignition points 36. In the in Fig. 1 As shown embodiment of the invention, so two detonation fronts arise, which move towards each other and meet at a certain point in the tool 2.

Sollen mehrere Zündstellen an einem Werkzeug 2, wie in Fig. 1, oder auch an mehreren Werkzeugen 2a bis 2d, wie in den Fig. 3a und 3b, gleichzeitig gezündet werden, kann man wahlweise mit mehreren Lasergeräten 3 oder mit nur einem Lasergerät 3 und einer Umlenkanordnung 25 arbeiten. Das Funktionsprinzip dieser beiden Varianten der Erfindung ist in den Fig. 3a und 3b illustriert. Je nach Anwendungsfall bietet sich auch eine Kombination aus beiden Möglichkeiten, also mehrere Lasergeräte 3 und wenigstens eine Umlenkanordnung 25 an.If several ignition points on a tool 2, as in Fig. 1 , or on several tools 2a to 2d, as in the Fig. 3a and 3b , be ignited simultaneously, one can optionally work with multiple laser devices 3 or with only one laser device 3 and a deflection device 25. The operating principle of these two variants of the invention is in the Fig. 3a and 3b illustrated. Depending on the application, it is also possible to use a combination of both options, that is to say a plurality of laser devices 3 and at least one deflection arrangement 25.

Die Anordnung der Werkzeuge 2a bis 2d und Lasergeräte 3a bis 3d in den Fig. 3a und 3b erlaubt sowohl eine gleichzeitige als auch eine zeitversetzte Zündung des Explosionsmittels in den einzelnen Werkzeugen 2a bis 2d.The arrangement of the tools 2a to 2d and laser devices 3a to 3d in the Fig. 3a and 3b allows both a simultaneous and a time-delayed ignition of the explosive in the individual tools 2a to 2d.

Für die gleichzeitige Zündung werden in Fig. 3a in allen vier Lasergeräten 3a bis 3d gleichzeitig Laserstrahlen 12a bis 12d generiert, die in etwa gleichzeitig durch die jeweiligen transparenten Medien 15a bis 15d in die Zündkammern 6a bis 6d der jeweiligen Werkzeuge 3a bis 3d dringen und dort das Explosionsmittel 7 entzünden.For simultaneous ignition will be in Fig. 3a in all four laser devices 3a to 3d simultaneously generated laser beams 12a to 12d, which penetrate approximately simultaneously through the respective transparent media 15a to 15d in the ignition chambers 6a to 6d of the respective tools 3a to 3d and there ignite the explosive 7.

In Fig. 3b dagegen wird nur ein Laserstrahl 12 erzeugt, welcher über die Umlenk- bzw. Spiegelanordnung 25 so aufgeteilt und abgelenkt wird, dass er etwa zeitgleich durch die transparenten Medien 15a bis 15d in die Zündrohre 5a bis 5d der jeweiligen Werkzeuge 2a bis 2d dringt und dort das Explosionsmittel 7 entzündet.In Fig. 3b In contrast, only a laser beam 12 is generated, which is so divided and deflected over the deflecting or mirror assembly 25 that it penetrates approximately simultaneously through the transparent media 15a to 15d in the ignition tubes 5a to 5d of the respective tools 2a to 2d and there the Explosive 7 ignited.

So entsteht in jedem der Werkzeuge 3a bis 3d etwa zeitgleich wenigstens eine Detonationsfront, wie bereits anhand Fig. 1 erklärt.Thus, in each of the tools 3a to 3d at least at the same time at least one detonation front, as already described Fig. 1 explained.

Für die zeitversetzte Zündung wird in Fig. 3a in den Lasergeräten 3a bis 3d zeitversetzt, z.B. nacheinander, jeweils ein Laserstrahl 12a bis 12d erzeugt. Diese treffen dann auch nacheinander in die Zündkammern 6a bis 6d der jeweiligen Werkzeuge 2a bis 2d und zünden die Explosionsmittel 7a bis 7d in den Werkzeugen 2a bis 2d nacheinander. D.h. zuerst das Explosionsmittel 7a in Werkzeug 2a, dann das Explosionsmittel 7b in Werkzeug 2b, usw.. Der zeitliche Versatz zwischen der Erzeugung der Laserstrahlen 12a bis 12d ist dabei beliebig wählbar. So können z.B. auch die Laserstrahlen 12a und 12b gleichzeitig erzeugt werden, während die Laserstrahlen 12c und 12d zeitlich nachgeschaltet sind. Prinzipiell sind beliebige Kombinationen denkbar.For the delayed ignition is in Fig. 3a delayed in the laser devices 3a to 3d, for example, one after the other, each generates a laser beam 12a to 12d. These then also meet successively in the ignition chambers 6a to 6d of the respective tools 2a to 2d and ignite the explosive means 7a to 7d in the tools 2a to 2d in succession. That is, first the explosive 7a in tool 2a, then the explosive 7b in tool 2b, etc. The temporal offset between the generation of the laser beams 12a to 12d is arbitrary selectable. For example, the laser beams 12a and 12b can be simultaneously generated, while the laser beams 12c and 12d are connected in time. In principle, any combinations are conceivable.

In Fig. 3b gibt es mehrere Möglichkeiten, das Explosionsmittel 7 in den Werkzeugen 2a bis 2d zeitversetzt zu zünden. Zum einen kann das Lasergerät 3 nacheinander mehrere Laserstrahlen 12 erzeugen. Zwischen der Erzeugung der einzelnen Laserstrahlen wird die Position der einzelnen Elemente 27, 28, 29 der Umlenkanordnung zueinander und/oder die Position des Lasergeräts 3 so geändert, dass der Laserstrahl 12 nacheinander jeweils durch das transparente Medium 15a bis 15d eines anderen Werkzeugs 3a bis 3d dringt und so das Explosionsmittel 7a bis 7d zündet.In Fig. 3b There are several ways to ignite the explosive 7 in the tools 2a to 2d with a time delay. On the one hand, the laser device 3 can successively generate a plurality of laser beams 12. Between the generation of the individual laser beams, the position of the individual elements 27, 28, 29 of the deflection arrangement relative to each other and / or the position of the laser device 3 is changed so that the laser beam 12 successively through the transparent medium 15a to 15d of another tool 3a to 3d penetrates and so ignites the explosive 7a to 7d.

Alternativ kann das Lasergerät 3 einen stetigen Laserstrahl 12 erzeugen, der mittels der Umlenkanordnung 25 in die Zündkammer 6a des ersten Werkzeugs 2a gelenkt wird und dort das Explosionsmittel zündet. Soll nun auch das Explosionsmittel in dem Werkzeug 2b gezündet werden, wird die Position der einzelnen Elemente 27, 28, 29 der Umlenkanordnung 25 zueinander und/oder die Position des Lasergeräts 3 so geändert, dass der Laserstrahl 12 durch das transparente Medium 15b in die Zündkammer 6b fällt. Analog verfährt man für die Zündung des Explosionsmittels in den Werkzeugen 2c und 2d.Alternatively, the laser device 3 can generate a continuous laser beam 12, which is deflected by means of the deflection arrangement 25 into the ignition chamber 6a of the first tool 2a and ignites the explosive there. If now also the explosive in the tool 2b are ignited, the position of the individual elements 27, 28, 29 of the deflection assembly 25 to each other and / or the position of the laser device 3 is changed so that the laser beam 12 through the transparent medium 15b in the ignition chamber 6b falls. The procedure is similar for the ignition of the explosive in the tools 2c and 2d.

Sollen auch hier mehrere, z.B. zwei, Werkzeuge gleichzeitig gezündet werden, können für den Energiestrahl 12 teildurchlässige Umlenkelemente, in diesem Fall teildurchlässige Spiegelelemente, verwendet werden. Diese erlauben es, nur einen Teil des Laserstrahls 12 abzulenken, während der restliche Teil des Laserstrahls seine ursprüngliche Richtung beibehält. So kann der Laserstrahl 12 auf eine Zündstelle, z.B. in dem Werkzeug 2a, gerichtet werden, um dort das Explosionsmittel 7 zu zünden. Mit Hilfe eines teildurchlässigen Spiegelelementes kann ein Teil des Laserstrahls 12 gleichzeitig zu einer weiteren Zündstelle, z.B. in dem Werkzeug 2b, gelenkt werden, und dort ebenfalls das Explosionsmittel zünden.If several, eg two, tools are to be ignited simultaneously as well, partially transparent deflecting elements, in this case partially transparent mirror elements, can be used for the energy beam 12. These allow only a portion of the laser beam 12 to be deflected while the remainder of the laser beam maintains its original direction. Thus, the laser beam 12 can be directed to an ignition point, for example in the tool 2a, in order to ignite the explosive 7 there. With the help of a partially transparent mirror element, a part of the laser beam 12 can be simultaneously directed to another ignition point, for example in the tool 2b, and there also ignite the explosive.

Claims (15)

  1. Method for explosion forming workpieces, wherein at least one workpiece (18) being arranged in at least one forming means (4) of a tool (2) and being formed at that location using an explosion means (7) which is to be ignited, the explosion means (7) being ignited by means of at least one energy beam (12), characterised in that the explosion means is gaseous and is provided at least partially in an ignition tube(5), which is separate from the forming means (4), of the tool (2) and the detonation front which is generated during the explosion, propagates within the explosion means (7) along the ignition tube (5) to the forming means (4) and into the workpiece (18).
  2. Method according to claim 1, characterised in that the energy beam (12) is directed from an energy source (3) to at least one ignition location (36) using a redirection arrangement (25).
  3. Method according to one of the preceding claims, characterised in that the explosion means (7) is ignited at several locations of the device (1) at the same time.
  4. Method according to any one of the preceding claims, characterised in that the explosion means (7) is ignited at several locations of the device (1) in a time-delayed manner.
  5. Method according to any one of the preceding claims, characterised in that multiple detonation fronts (34, 35) are generated within a tool (2).
  6. Method according to any one of the preceding claims, characterised in that at least one detonation front (34) is generated within each of a multiple of tools (2a to 2d) of the device (1).
  7. Device (1) for explosion forming, in particular for carrying out the method according to claim 1, wherein at least one workpiece (18) can be arranged in at least one forming means (4) of a tool (2) and can be formed using an explosion means (7) which is to be ignited, there being provided at least one energy beam generating device (3), the explosion means (7) can be ignited by means of an energy beam (12) of the energy beam generating device (3), characterised in that the explosion means is gaseous and is provided at least partially in an ignition pipe (5), which is separate from the forming means (4), of the tool (2) so that a detonation front which is generated during the explosion, can propagate along the ignition tube (5) to the forming means (4) and into the workpiece (18).
  8. Device (1) according to claim 7, characterised in that the tool (2) has at least one introduction location (14) which is permeable to the energy beam (12).
  9. Device (1) according to claim 8, characterised in that the introduction location (14) has at least one transparent medium (15).
  10. Device (1) according to claim 9, characterised in that the transparent medium (15) is shaped in a lenticular, convex manner.
  11. Device (1) according to either claim 9 or claim 10, characterised in that the transparent medium (15) has a holder (22) which contains copper.
  12. Device (1) according to any one of claims 9 to 11, characterised in that the transparent medium (15) is arranged in the tool (2) with a seal (24) which seals the explosion space (6) with respect to the environment.
  13. Device (1) according to any one of claims 7 to 12, characterised in that the tool (2) has multiple introduction locations (14).
  14. Device (1) according to any one of claims 7 to 13, characterised in that multiple tools (2) are each provided with at least one introduction location (14).
  15. Device (1) according to any one of claims 7 to 14, characterised in that there is provided in the beam path of the energy beam generating device (3), at least one redirection arrangement (25), by means of which the energy beam (12) can be directed to at least one ignition location (36).
EP07724979A 2006-08-11 2007-05-08 Method and device for explosion forming Not-in-force EP2049281B1 (en)

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DE102006037742A DE102006037742B4 (en) 2006-08-11 2006-08-11 Method and apparatus for explosion forming
PCT/EP2007/004055 WO2008017332A1 (en) 2006-08-11 2007-05-08 Method and device for explosion forming

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EP2049281B1 true EP2049281B1 (en) 2009-12-23

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EP (1) EP2049281B1 (en)
KR (1) KR20090037936A (en)
CN (1) CN101516543A (en)
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ATE452715T1 (en) 2010-01-15
US8252210B2 (en) 2012-08-28
DE502007002440D1 (en) 2010-02-04
US20100207287A1 (en) 2010-08-19
EP2049281A1 (en) 2009-04-22
DE102006037742B4 (en) 2010-12-09
DE102006037742A1 (en) 2008-02-14
CN101516543A (en) 2009-08-26
CA2660714A1 (en) 2008-02-14
WO2008017332A1 (en) 2008-02-14

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