Rfid transponder chip modules, elements thereof, and methods
US-2019392283-A1 · Dec 26, 2019 · US
US12318864B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12318864-B2 |
| Application number | US-202017036031-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 29, 2020 |
| Priority date | Sep 30, 2019 |
| Publication date | Jun 3, 2025 |
| Grant date | Jun 3, 2025 |
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A method for welding a flexible film ( 10 ) to a carrier component ( 20 ) having the following steps: 1) pressing the film ( 10 ) on the carrier component ( 20 ) by a volumetric flow of a fluid, and 2) laser welding the film ( 10 ) on the carrier component ( 20 ).
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What is claimed is: 1. A method for welding a flexible film ( 10 ) to a carrier component ( 20 ), having the following steps: 1) Pressing the film ( 10 ) on the carrier component ( 20 ) by a volumetric flow of a fluid, and 2) laser welding the film ( 10 ) on the carrier component ( 20 ), wherein before step 1), a pre-deforming of the film ( 10 ) is performed using a method that does not include the volumetric flow of fluid and is done by means of a negative mold (M), and wherein the method is used for welding a flexible film ( 10 ) in the form of a flexible trace embedded within a flexible circuit board (FPC) to an electrical carrier component ( 20 ) in the form of landing on a rigid circuit board (PCB). 2. The method according to claim 1 , wherein, in step 1), the fluid is a pressurized fluid, and/or wherein, in step 1), the volumetric flow is produced by a nozzle or a nozzle comb. 3. The method according to claim 2 , wherein the pressurized fluid is in the form of compressed air, nitrogen and/or shielding gas. 4. The method according to claim 1 , wherein, in step 2), a laser radiation in the visible wavelength range, or an NIR laser radiation is used, and/or wherein, in step 2), a pulsed laser radiation, a quasi CW laser radiation or a CW laser radiation is used. 5. The method according to claim 4 , wherein the laser in the visible wavelength range is in the green wavelength range and/or in the blue wavelength range. 6. The method according to claim 1 , wherein, in step 2), a laser radiation with at least one of the following parameters is used: a wavelength of 500 nm-600 nm, a focus diameter of 20 μm-1 mm, a power output of 1 W-4000 W, a pulse duration of 0.3 ms-50 ms, a scanning rate of 1 mm/s-1 km/s. 7. The method according to claim 6 , wherein the laser radiation is a quasi CW laser radiation, with at least one of the following parameters: a wavelength of 515 nm, a focus diameter of 150 μm, a power output of 1 200 W-600 W, a pulse duration of 2 ms-6 ms, a scanning rate of 200 mm/s-300 mm/s. 8. The method according to claim 1 , wherein, in step 2), a laser radiation with at least one of the following parameters is used: a wavelength of 1030 nm-1064 nm, a focus diameter of 10 μm-500 μm, a power output of 1 W-2000 W, a frequency of 1 Hz-2000 kHz, a pulse duration of: 1 ns-500 ns, a scanning rate of: 1 mm/s-1 km/s. 9. The method according to claim 8 , wherein the laser radiation is a pulsed laser radiation, with at least one of the following parameters: a wavelength of 1030 nm-1064 nm, a focus diameter of 20 μm-200 μm, a power output of 10 W-500 W, a frequency of 1000 Hz-2000 Hz, a pulse duration of: 120 ns-500 ns, a scanning rate of: 10 mm/s-1000 mm/s. 10. The method according to claim 9 , wherein the laser radiation is a pulsed laser radiation, with at least one of the following parameters: a power output of 20 W-100 W a scanning rate of: 10 mm/s-100 mm/s. 11. The method according to claim 8 , wherein the laser radiation is a pulsed laser radiation. 12. The method according to claim 1 , wherein, after step 2), a testing of a weld seam (N) for conductivity, resistance and/or impedance is performed. 13. The method according to claim 1 , wherein the method is used for welding multiple flexible films ( 10 ) to multiple carrier components ( 20 ) in the same pass. 14. The method according to claim 1 , wherein the method is used for welding a flexible film ( 10 ) of a layer thickness of 20 μm-100 μm, to an electrical carrier component ( 20 ) of a thickness of 50 μm-500 μm. 15. The method according to claim 14 , wherein the method is used for welding a flexible film ( 10 ) of a layer thickness of 35 μm, to an electrical carrier component ( 20 ) of a thickness of 50 μm-140 μm. 16. The method according to claim 15 , wherein the method is used for welding a flexible film ( 10 ) of a layer thickness of 35 μm, to an electrical carrier component ( 20 ) of a thickness of 135 μm. 17. The method according to claim 1 , wherein the metal is copper. 18. The method according to claim 1 , wherein the pre-deforming of the film ( 10 ) includes using a punch(S). 19. The method according to claim 18 , wherein the punch(S) is an embossing punch(S) that cooperates with the negative mold (M). 20. The method according to claim 1 , wherein the pre-deforming of the film ( 10 ) includes deep drawing the film ( 10 ). 21. The method according to claim 1 , wherein the pre-deforming of the film ( 10 ) includes microdeforming the film ( 10 ).
in an atmosphere of particular gases · CPC title
Printed circuits · CPC title
Copper or alloys thereof · CPC title
Preliminary treatment · CPC title
Scanning systems, i.e. devices involving movement of the laser beam relative to the laser head · CPC title
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