EP2049281B1 - Verfahren und vorrichtung zum explosionsumformen - Google Patents
Verfahren und vorrichtung zum explosionsumformen Download PDFInfo
- 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
Links
- 238000000034 method Methods 0.000 title claims abstract description 25
- 238000004880 explosion Methods 0.000 title claims description 37
- 238000005474 detonation Methods 0.000 claims description 25
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 2
- 229910052802 copper Inorganic materials 0.000 claims description 2
- 239000010949 copper Substances 0.000 claims description 2
- 239000002360 explosive Substances 0.000 abstract description 61
- 239000011521 glass Substances 0.000 description 21
- 239000007789 gas Substances 0.000 description 6
- 239000000203 mixture Substances 0.000 description 5
- 230000002123 temporal effect Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 229910000952 Be alloy Inorganic materials 0.000 description 2
- 229910000881 Cu alloy Inorganic materials 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 230000003111 delayed effect Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000012528 membrane Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping 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
- B21D26/06—Shaping 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
- B21D26/08—Shaping 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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006037742A DE102006037742B4 (de) | 2006-08-11 | 2006-08-11 | Verfahren und Vorrichtung zum Explosionsumformen |
PCT/EP2007/004055 WO2008017332A1 (de) | 2006-08-11 | 2007-05-08 | Verfahren und vorrichtung zum explosionsumformen |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2049281A1 EP2049281A1 (de) | 2009-04-22 |
EP2049281B1 true EP2049281B1 (de) | 2009-12-23 |
Family
ID=38474435
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07724979A Not-in-force EP2049281B1 (de) | 2006-08-11 | 2007-05-08 | Verfahren und vorrichtung zum explosionsumformen |
Country Status (8)
Country | Link |
---|---|
US (1) | US8252210B2 (zh) |
EP (1) | EP2049281B1 (zh) |
KR (1) | KR20090037936A (zh) |
CN (1) | CN101516543A (zh) |
AT (1) | ATE452715T1 (zh) |
CA (1) | CA2660714A1 (zh) |
DE (2) | DE102006037742B4 (zh) |
WO (1) | WO2008017332A1 (zh) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005025660B4 (de) | 2005-06-03 | 2015-10-15 | Cosma Engineering Europe Ag | Vorrichtung und Verfahren zum Explosionsumformen |
DE102006037754B3 (de) | 2006-08-11 | 2008-01-24 | Cosma Engineering Europe Ag | Verfahren und Vorrichtung zum Explosionsumformen |
DE102006037742B4 (de) | 2006-08-11 | 2010-12-09 | Cosma Engineering Europe Ag | Verfahren und Vorrichtung zum Explosionsumformen |
DE102006056788B4 (de) | 2006-12-01 | 2013-10-10 | Cosma Engineering Europe Ag | Verschlusseinrichtung für das Explosionsumformen |
DE102006060372A1 (de) | 2006-12-20 | 2008-06-26 | Cosma Engineering Europe Ag | Werkstück und Verfahren für das Explosionsumformen |
DE102007007330A1 (de) | 2007-02-14 | 2008-08-21 | Cosma Engineering Europe Ag | Verfahren und Werkzeuganordnung zum Explosionsumformen |
US8443641B2 (en) | 2007-02-14 | 2013-05-21 | Cosma Engineering Europe Ag | Explosion forming system |
DE102007023669B4 (de) | 2007-05-22 | 2010-12-02 | Cosma Engineering Europe Ag | Zündeinrichtung für das Explosionsumformen |
DE102007036196A1 (de) | 2007-08-02 | 2009-02-05 | Cosma Engineering Europe Ag | Vorrichtung für die Zufuhr eines Fluids für Explosionsumformen |
DE102008006979A1 (de) | 2008-01-31 | 2009-08-06 | Cosma Engineering Europe Ag | Vorrichtung für das Explosionsumformen |
EP2303487B1 (en) * | 2008-04-30 | 2018-08-29 | Magna International Inc. | Explosion forming system |
US8534107B2 (en) * | 2011-06-10 | 2013-09-17 | Ford Global Technologies, Llc | Method and apparatus for pulsed forming, punching and trimming of tubular members |
CN103755502B (zh) * | 2014-01-28 | 2016-01-06 | 西北大学 | 基于动态措施与动态组分双重调节的火炸药配方设计方法 |
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DE102006037742B4 (de) | 2006-08-11 | 2010-12-09 | Cosma Engineering Europe Ag | Verfahren und Vorrichtung zum Explosionsumformen |
DE102006037754B3 (de) | 2006-08-11 | 2008-01-24 | Cosma Engineering Europe Ag | Verfahren und Vorrichtung zum Explosionsumformen |
DE102006056788B4 (de) | 2006-12-01 | 2013-10-10 | Cosma Engineering Europe Ag | Verschlusseinrichtung für das Explosionsumformen |
DE102006060372A1 (de) | 2006-12-20 | 2008-06-26 | Cosma Engineering Europe Ag | Werkstück und Verfahren für das Explosionsumformen |
DE102007007330A1 (de) | 2007-02-14 | 2008-08-21 | Cosma Engineering Europe Ag | Verfahren und Werkzeuganordnung zum Explosionsumformen |
DE102007023669B4 (de) | 2007-05-22 | 2010-12-02 | Cosma Engineering Europe Ag | Zündeinrichtung für das Explosionsumformen |
DE102007036196A1 (de) | 2007-08-02 | 2009-02-05 | Cosma Engineering Europe Ag | Vorrichtung für die Zufuhr eines Fluids für Explosionsumformen |
DE102008006979A1 (de) | 2008-01-31 | 2009-08-06 | Cosma Engineering Europe Ag | Vorrichtung für das Explosionsumformen |
-
2006
- 2006-08-11 DE DE102006037742A patent/DE102006037742B4/de not_active Expired - Fee Related
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- 2007-05-08 CA CA002660714A patent/CA2660714A1/en not_active Abandoned
- 2007-05-08 KR KR1020097002671A patent/KR20090037936A/ko not_active Application Discontinuation
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US20100207287A1 (en) | 2010-08-19 |
CA2660714A1 (en) | 2008-02-14 |
KR20090037936A (ko) | 2009-04-16 |
CN101516543A (zh) | 2009-08-26 |
US8252210B2 (en) | 2012-08-28 |
DE502007002440D1 (de) | 2010-02-04 |
DE102006037742A1 (de) | 2008-02-14 |
DE102006037742B4 (de) | 2010-12-09 |
ATE452715T1 (de) | 2010-01-15 |
WO2008017332A1 (de) | 2008-02-14 |
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