CN114787417A - Method for producing an electrically conductive structure - Google Patents
Method for producing an electrically conductive structure Download PDFInfo
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- CN114787417A CN114787417A CN202080085464.0A CN202080085464A CN114787417A CN 114787417 A CN114787417 A CN 114787417A CN 202080085464 A CN202080085464 A CN 202080085464A CN 114787417 A CN114787417 A CN 114787417A
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- laser radiation
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 8
- 239000012876 carrier material Substances 0.000 claims abstract description 33
- 239000000654 additive Substances 0.000 claims abstract description 32
- 230000000996 additive effect Effects 0.000 claims abstract description 28
- 230000005855 radiation Effects 0.000 claims abstract description 23
- 238000001465 metallisation Methods 0.000 claims abstract description 17
- 239000002131 composite material Substances 0.000 claims abstract description 9
- 229920001187 thermosetting polymer Polymers 0.000 claims abstract description 8
- 238000000034 method Methods 0.000 claims description 18
- 238000000691 measurement method Methods 0.000 claims description 2
- 239000000463 material Substances 0.000 abstract description 11
- 230000009471 action Effects 0.000 abstract description 4
- 238000007669 thermal treatment Methods 0.000 abstract description 2
- 239000002245 particle Substances 0.000 description 12
- 239000000047 product Substances 0.000 description 9
- 238000001994 activation Methods 0.000 description 8
- 239000000945 filler Substances 0.000 description 7
- 230000004913 activation Effects 0.000 description 6
- 238000002679 ablation Methods 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 150000002736 metal compounds Chemical class 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 239000013543 active substance Substances 0.000 description 3
- 239000010949 copper Substances 0.000 description 3
- 238000000354 decomposition reaction Methods 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 230000005670 electromagnetic radiation Effects 0.000 description 2
- 238000004299 exfoliation Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920000426 Microplastic Polymers 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 239000007857 degradation product Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 239000011256 inorganic filler Substances 0.000 description 1
- 229910003475 inorganic filler Inorganic materials 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000004901 spalling Methods 0.000 description 1
- 229910052596 spinel Inorganic materials 0.000 description 1
- 239000011029 spinel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/16—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
- C23C18/1601—Process or apparatus
- C23C18/1603—Process or apparatus coating on selected surface areas
- C23C18/1607—Process or apparatus coating on selected surface areas by direct patterning
- C23C18/1612—Process or apparatus coating on selected surface areas by direct patterning through irradiation means
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/16—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
- C23C18/1601—Process or apparatus
- C23C18/1603—Process or apparatus coating on selected surface areas
- C23C18/1607—Process or apparatus coating on selected surface areas by direct patterning
- C23C18/1608—Process or apparatus coating on selected surface areas by direct patterning from pretreatment step, i.e. selective pre-treatment
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/16—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
- C23C18/1601—Process or apparatus
- C23C18/1633—Process of electroless plating
- C23C18/1635—Composition of the substrate
- C23C18/1639—Substrates other than metallic, e.g. inorganic or organic or non-conductive
- C23C18/1641—Organic substrates, e.g. resin, plastic
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/16—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
- C23C18/1601—Process or apparatus
- C23C18/1633—Process of electroless plating
- C23C18/1655—Process features
- C23C18/1664—Process features with additional means during the plating process
- C23C18/1667—Radiant energy, e.g. laser
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/16—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
- C23C18/18—Pretreatment of the material to be coated
- C23C18/1851—Pretreatment of the material to be coated of surfaces of non-metallic or semiconducting in organic material
- C23C18/1862—Pretreatment of the material to be coated of surfaces of non-metallic or semiconducting in organic material by radiant energy
- C23C18/1868—Radiation, e.g. UV, laser
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/16—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
- C23C18/31—Coating with metals
Landscapes
- Chemical & Material Sciences (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- General Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Inorganic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Chemically Coating (AREA)
- Laminated Bodies (AREA)
Abstract
The invention relates to a method for producing a composite structure made of at least one electrically conductive structure, a carrier made of a non-conductive carrier material from a thermosetting plastic, and at least one electronic component, wherein the non-conductive carrier material contains an additive having catalytically active species formed in a metallization bath without an external current as a result of the action of laser radiation. By using pulsed laser radiation, a quasi non-thermal treatment of the carrier material is achieved in that the material directly evaporates due to the very high peak intensity, so that no or hardly any melt is produced.
Description
The invention relates to a method for producing a composite structure by means of laser radiation, said composite structure being produced from at least one electrically conductive structure, a carrier and at least one electronic component, said carrier being produced from a non-conductive carrier material of plastic origin, said non-conductive carrier material containing an additive which subsequently forms a catalytically active substance by irradiation with laser radiation in a metallization bath without an external current.
In a process known as Laser-direct structuring (LDS), the carrier material is injection molded into a molded part in a single-component injection molding process using plastic granules with special additives. By means of a laser, the additive can be converted in a site-selective manner into catalytically active crystal nuclei in a physicochemical reaction in which the metal is deposited in the subsequent chemical metallization bath at the sites treated in this way.
DE 10132092 a1 describes a circuit structure on a non-conductive carrier material, which consists of metal nuclei and a metallization subsequently applied to the metal nuclei, the metal nuclei being generated by decomposition of a non-conductive inorganic metal compound contained in the carrier material in a finely distributed manner by means of electromagnetic radiation.
DE 102014114986 a1 describes a method for producing a circuit structure, in which selective laser irradiation is carried out on a circuit carrier in accordance with the circuit structure to be produced, and the circuit structure is then produced in a metallization bath without an external current. Here, for example, laser radiation having a wavelength of 1,064 nm and a pulse frequency of 100kHz is used.
In the method disclosed in DE 102013100016 a1 for producing such an electrically conductive structure, a thermoplastic copper oxide-polyester mixture is mixed into a carrier material and injection molded into a workpiece, which is then selectively activated for subsequent metallization by means of a laser.
Due to technical limitations, it is now possible to reliably manufacture line widths of a minimum of 150 μm by means of an LDS process. To further advance the desired MID miniaturization, this limitation must be further suppressed. For this purpose, efforts are being made to further focus the laser radiation and to direct it more precisely onto the surface of the shaped part.
DE 102012010635 a1 relates to a method for the direct 3D structuring of hard, brittle optical materials, in which the surface is structured with ultrashort pulsed lasers and the 3D structure or shape is thereby introduced in a targeted manner.
The occurrence of foreign deposits has proven to be a disadvantage in practice in the implementation of processes for producing electrically conductive structures on/in non-conductive carrier materials, for example by laser activation in the case of wires, in particular in the case of thermosets as carrier materials. Since the thermosetting plastic does not melt but decomposes, a large amount of carbon is released, which is catalytically active in the electroless metallisation bath.
In the subsequent metallization of the metal atoms, extraneous deposits also appear in an undesirable manner outside the processing region on catalytically active corrosion products in the metallization bath. Such foreign deposits can actually cause a short circuit if the distance between the resulting lines is small. Here, the degradation products also prove to be very problematic, since, owing to their high temperature during decomposition, they can bond again to the plastic surface outside the structured region and can therefore hardly be removed anymore. As the structures to be produced become more and more compact, these problems occur not only in thermosetting plastics but in principle in all plastics.
If the temperature is too high during structuring, the exfoliation products become so hot that they adhere strongly to the surface of the carrier material that it can no longer be cleaned reliably. The adhering, catalytically active peeling products can lead to "beading" in particular in the region of the recesses due to foreign deposits in the edge regions of the recesses. Although practice has shown that this effect can be minimized by significantly reducing the laser power, this results in significantly longer cycle times.
The object of the present invention is therefore to provide a method in which the damage to the electrically conductive structures produced in this way on a carrier material as a result of the ablation products is significantly reduced. According to the invention, in particular, a further reduction in the structural size of the electrically conductive structure should be enabled.
According to the invention, this object is achieved by a method according to the features of claim 1. Further embodiments of the invention can be found in the dependent claims.
In the method according to the invention for producing a composite structure by means of laser radiation, the composite structure being made of at least one electrically conductive structure, a carrier and at least one electronic component, the carrier being made of an electrically non-conductive carrier material from a thermosetting plastic, wherein the electrically non-conductive carrier material contains an additive which subsequently forms a catalytically active substance by irradiation with laser radiation in an electroless metallisation bath, the electrically conductive structure being formed by irradiation with pulsed laser radiation having a pulse duration of less than 100 picoseconds and subsequent electroless metallisation, and the pulse repetition rate being set such that, on the respective additive or additive region to be activated, successive pulses are deflected onto the additive or additive region one above the other.
The present invention is based on the unexpected recognition that: the method for producing electrically conductive structures by laser activation of metal compounds contained in additives, in particular with ultrashort pulsed lasers, can be used without problems, in particular in thermosetting plastics, and has the advantage here that fewer foreign deposits occur.
For the first time, a method for laser direct structuring is proposed which on the one hand reliably achieves the energy input required for laser activation, but on the other hand limits the heating such that not only significantly fewer ablation products are produced, but also the temperature of the ablation products is so low that the adhesion to the carrier material is very low and can therefore be easily removed.
According to the invention, particularly fine electrically conductive structures can be produced in this way, since the short-circuit risk associated therewith is also prevented by avoiding foreign deposits. Thereby the width of the structures and the distance between the structures can be reduced.
A further highly effective embodiment of the method according to the invention is also achieved in that the number of laser pulses per second (pulse repetition rate) is designed to be so large, for example 2 to 2.5MHz, that successive pulses act with regions of action that overlap one another on the respective additive particles or additive regions to be activated. In this way, a plurality of successive pulses are always applied to each additive particle or each additive region, so that the energy input is correspondingly increased.
This enables precise temperature management, by means of which the following are excluded: the thermal energy coupled into the support material is so low that the temperature is not sufficient to reduce the additives, such as Cu — Cr spinel, to elemental copper, and therefore catalytically active species for the desired metallization are not or cannot be reliably generated, and irregular partial metallizations occur in particular. Furthermore, the overlapping regions of action of the successive pulses also ensure that the temperature during structuring is not too high, so that the flaking products do not heat up compared to the prior art and thus do not adhere to the carrier material in an undesirable manner, so that they cannot be removed again reliably.
By means of this method, a composite structure is produced in which a non-conductive support material contains an additive with catalytically active species formed as a result of the action of laser radiation, wherein the electrically conductive structure is formed by irradiation with pulsed laser radiation, in particular ultrashort pulsed laser light, and by then metallization in a metallization bath. According to the invention, by using pulsed laser radiation, a quasi non-thermal treatment of the carrier material is achieved with the correct selection of the parameters in such a way that the material evaporates directly due to the very high peak intensity, so that no or almost no melt is produced. The pulses are so short that, during the pulse duration, no energy is transferred into the lattice oscillation and thus into the temperature increase. It is therefore believed that the energy introduced by the ultrashort pulse corresponds to the energy required for evaporation of the material, and therefore no other energy is used for thermalization.
Contrary to the above prejudice of the academia, the invention is based on the unexpected recognition that the activation of the metal compounds and the formation of catalytically active nuclei in those regions thus activated by laser light corresponds to a thermal process which requires high temperatures for the decomposition of the additive particles: not the heat energy input but the maximum strength forms the basis and thus creates the cause and necessary prerequisites for the activation of the metal compound.
It has proven particularly advantageous here for the electrically non-conductive support material to comprise at least one inorganic filler with a maximum particle size of 50 μm. Filler materials which are not destroyed or broken apart by the active laser radiation can thus also be used, since these filler materials, because of their small particle size, do not impair or hinder subsequent processing, for example the introduction of recesses such as holes, including through-holes or blind holes. The filler can therefore be selected without restriction according to the desired technical properties of the thermoset, for example with regard to viscosity, CTE (Coefficient of Thermal Expansion) or setting time.
The catalytically active exfoliation products, which in the prior art are particularly disadvantageous with regard to adhesion, are therefore reliably prevented from forming what is known as "beading" in the region of the pores. According to the invention, the cycle time is thus not increased. With ultrashort pulse lasers using picosecond laser sources, significantly less heat is generated upon ablation. This prevents the generation of hot spalling products and formation of a ledge during drilling, even at higher powers. The use of higher power leads to a higher ablation rate, whereby in practice even cycle times can be reduced.
In a particularly advantageous manner, the change from nanosecond pulse to picosecond pulse, with the other parameters remaining unchanged during structuring of the carrier material, and the correspondingly reduced heat input which can lead to inadequate activation of the additive, is compensated by the overlapping region of the individual pulses, which can be achieved by using higher pulse repetition rates, for example in the range between 2 and 2.5 MHz.
Another embodiment which is also very effective is also realized in the following way: the position and/or orientation of at least one electronic component in the carrier material is determined using a contactless measurement method, in particular using electromagnetic radiation, for example roentgen rays, the deviation of the actual position and/or the actual orientation from the target position and/or the target orientation is then determined, and correction values for the subsequent irradiation of the carrier material by means of pulsed laser radiation are derived therefrom, and finally the irradiation is carried out taking into account these correction values. Thereby, in particular when embedding one or more electronic components into the composite mass, the individual positional deviations of the electronic components from the target position are determined. For this purpose, the exact position and the degree of torsion of the electronic components are determined, for example, by means of the roentgen ray method, and the irradiation of the activatable additive or the catalytically active substance is carried out taking into account the correction values. The lines and holes to be structured can be adapted to the actual position and orientation of the electronic components in the carrier material by means of software, thereby avoiding rejects and significantly increasing the reliability.
When, according to a preferred embodiment, the size and/or mass of the individual filler particles contained in the carrier material is significantly greater than the size and/or mass of the individual additive particles contained in the carrier material, the size or mass difference of the filler particles on the one hand and the additive particles on the other hand results in an uneven distribution of the additive and filler particles in an unexpected manner, with the result that, during processing of the carrier material, the relatively large or heavy filler particles are predominantly collected in the inner or middle region of the carrier material, while the relatively small or light additive particles are displaced into the layers of the carrier material close to the edges, relative to this. By increasing the concentration of the additive in the layer close to the edge, the activation process can be significantly improved there, whereby the activation process can be carried out with a low radiation intensity without the total amount of additive added having to be increased for this purpose. At the same time, undesirable changes in the properties of the other materials are avoided by a corresponding reduction in the proportion of additives in the core part of the carrier material. For example, the LDS additive is contained in the support material in an amount of 3 to 15 weight percent, preferably 6 to 12 weight percent.
Claims (6)
1. Method for producing a composite structure by means of laser radiation, the composite structure being made of at least one electrically conductive structure, a carrier and at least one electronic component, the carrier being made of an electrically non-conductive carrier material from a thermosetting plastic, wherein the electrically non-conductive carrier material contains an additive which subsequently forms catalytically active species by irradiation with laser radiation in an electrically current-free metallization bath, wherein the electrically conductive structure is formed by irradiation with pulsed laser radiation having a pulse duration of less than 100 picoseconds and subsequent electrically current-free metallization, and wherein the pulse repetition rate is set such that, in the region of the respective additive or additive region to be activated, pulses which follow one another are deflected onto the additive or additive region one above the other.
2. The method according to claim 1, characterized in that the laser radiation is imaged onto the non-conductive carrier material through a partially transmissive mask.
3. A method according to claim 1 or 2, characterized in that the laser radiation is positioned on the carrier using a polygon scanner.
4. Method according to at least one of the preceding claims, characterized in that a plurality of, in particular four, galvanometer scanners are used to position the laser radiation on the carrier.
5. Method according to at least one of the preceding claims, characterized in that the laser radiation is positioned on the carrier using a resonator mirror.
6. Method according to at least one of the preceding claims, characterized in that the actual position and/or the actual orientation of the electronic component in the carrier material is determined by using a contactless measurement method, in particular by means of roentgen rays, then the deviation of the actual position and/or the actual orientation from a target position and/or a target orientation is determined, and from this a correction value for the subsequent irradiation of the carrier material by means of the pulsed laser radiation is derived, and the irradiation is performed taking into account the correction value.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
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DE102019133955.3 | 2019-12-11 | ||
DE102019133955.3A DE102019133955B4 (en) | 2019-12-11 | 2019-12-11 | Method for producing a composite structure from at least one conductive structure |
PCT/DE2020/100840 WO2021115518A1 (en) | 2019-12-11 | 2020-10-01 | Method for producing an electrically conductive structure |
Publications (1)
Publication Number | Publication Date |
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CN114787417A true CN114787417A (en) | 2022-07-22 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202080085464.0A Pending CN114787417A (en) | 2019-12-11 | 2020-10-01 | Method for producing an electrically conductive structure |
Country Status (7)
Country | Link |
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US (1) | US20230026070A1 (en) |
EP (1) | EP4073286A1 (en) |
JP (1) | JP2023505869A (en) |
KR (1) | KR20220087531A (en) |
CN (1) | CN114787417A (en) |
DE (1) | DE102019133955B4 (en) |
WO (1) | WO2021115518A1 (en) |
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WO2014085324A1 (en) * | 2012-11-27 | 2014-06-05 | President And Fellows Of Harvard College | Crystal growth through irradiation with short laser pulses |
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DE10132092A1 (en) * | 2001-07-05 | 2003-01-23 | Lpkf Laser & Electronics Ag | Track structures and processes for their manufacture |
US20070148420A1 (en) * | 2005-12-28 | 2007-06-28 | Intel Corporation | Method of making a substrate using laser assisted metallization and patterning with electroless plating without electrolytic plating |
JP2007330995A (en) * | 2006-06-15 | 2007-12-27 | Ricoh Co Ltd | Laser beam machining apparatus, laser beam machining method, liquid droplet delivery head machined by the laser beam machining method, and image forming apparatus |
CN102006964B (en) * | 2008-03-21 | 2016-05-25 | Imra美国公司 | Material processing method based on laser and system |
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- 2019-12-11 DE DE102019133955.3A patent/DE102019133955B4/en active Active
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2020
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- 2020-10-01 US US17/784,156 patent/US20230026070A1/en not_active Abandoned
- 2020-10-01 EP EP20792922.5A patent/EP4073286A1/en not_active Withdrawn
- 2020-10-01 CN CN202080085464.0A patent/CN114787417A/en active Pending
- 2020-10-01 WO PCT/DE2020/100840 patent/WO2021115518A1/en unknown
- 2020-10-01 KR KR1020227017515A patent/KR20220087531A/en unknown
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JP2023505869A (en) | 2023-02-13 |
EP4073286A1 (en) | 2022-10-19 |
KR20220087531A (en) | 2022-06-24 |
DE102019133955A1 (en) | 2021-06-17 |
US20230026070A1 (en) | 2023-01-26 |
WO2021115518A1 (en) | 2021-06-17 |
DE102019133955B4 (en) | 2021-08-19 |
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