PROCESS FOR PRODUCING A LINE OF WEAKNESS IN A COVER ELEMENT THROUGH REMOVAL OF MATERIAL

• US 20150352670A1
• Filed: 06/09/2015
• Published: 12/10/2015
• Est. Priority Date: 06/10/2014
• Status: Active Grant

• Current Assignee: Jenoptik Automatisierungstechnik Gmbh (Jenoptik AG)
• Original Assignee: Jenoptik Automatisierungstechnik Gmbh (Jenoptik AG)
• Inventors: LUTZE, Walter, GRIEBEL, Martin, WEISSER, Juergen
• Granted Patent: US 9,676,062 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B23K 2103/30 Organic material
• CPC Class Codes: B23K 2103/50 Inorganic material, e.g. metals, not provided for in B23K2103/02 – B23K2103/26
• CPC Class Codes: B23K 26/032 using optical means
• CPC Class Codes: B23K 26/0622 by shaping pulses
• CPC Class Codes: B23K 26/082 Scanning systems, i.e. devices involving movement of the laser beam relative to the laser head
• CPC Class Codes: B23K 26/364 for making a groove or trench, e.g. for scribing a break initiation groove
• CPC Class Codes: B23K 26/402 involving non-metallic material, e.g. isolators

Abstract

Process for producing a line of weakness in a cover element comprising at least one slit. This slit is produced through a plurality of machining cycles in which a pulsed laser beam is guided in each instance over the cover element along an imaginary line so that the energy of the laser pulses is introduced into the cover element. The slits are produced in two segments. More energy is introduced over the machining cycles in the first, comparatively short segments than in the second, comparatively long segments. The residual wall below the slits decreases with each machining cycle until the first residual wall segment thickness in the first segment is so small that energy portions transmit through the first residual wall segment and are detected by a sensor arrangement arranged downstream. Accordingly, the first residual wall segment thickness is detected, and inferences can be drawn from this about the second residual wall segment thickness.

Claims

1. Process for producing a line of weakness by removal of material in a cover element having a visible side and aback side opposite the visible side, comprising directing laser pulses with an energy determined by a pulse amplitude and a pulse length to said back side and introducing said energy into said cover element repeatedly along an imaginary line at a forward feed speed in a machining cycle so that the line of weakness is formed as a result of removal of material through at least one slit having a slit length and a residual wall thickness of a residual wall adjoining said visible side below said at least one slit, steadily decreasing said residual wall thickness with each machining cycle so that said residual wall thickness becomes sufficiently small that energy portions of the laser pulses which transmit through the residual wall are detected by a sensor arrangement thereby detecting said residual wall thickness, introducing energy point by point along the at least one slit along said imaginary line, said introduced energy being greater in at least one first segment with a first length than in at least one second segment with a second length such that, in each instance, a first residual wall segment thickness of a first residual wall segment of the residual wall along the at least one first segment decreases more slowly than a second residual wall segment thickness of a second residual wall segment of the residual wall along the at least one second segment so that, in each instance, the first residual wall segment thickness of the first residual wall segment along the at least one first segment is detected before the second residual wall segment thickness for the second residual wall segment along the at least one second segment can be detected, and drawing inferences about the second residual wall segment thickness of the second residual wall segment along the at least one second segment without detecting this second residual wall segment thickness.

2. The process according to claim 1, wherein said energy input per slit along the first length of the at least one first segment at least in the first of the machining cycles is carried out by means of at least one of the laser pulses which has a pulse length shorter than a pulse length in a subsequent machining cycle, and the energy input in further machining cycles along the slit length of the slit is carried out by means of one of the laser pulses which has a long pulse length compared to the pulse length in a previous machining cycle.

3. The process according to claim 2, wherein a pulse amplitude of the laser pulses is the same at least over one of the machining cycles.

4. The process according to claim 1, wherein the energy input per slit and per machining cycle is carried out in each instance with at least one same laser pulse which is amplitude-modulated over its pulse length with a comparatively large pulse amplitude for the energy input along the first length of the at least one first segment and a comparatively small pulse amplitude for the energy input along the second length of the at least one second segment.

5. The process according to claim 1, wherein the energy input per slit and per machining cycle is carried out with a same sequence of laser pulses in which at least one of the laser pulses has a comparatively large pulse amplitude for the energy input along the first length of the at least one first segment and a plurality of the laser pulses follow one another directly and have a comparatively small pulse amplitude for the energy input along the second length of the at least one second segment.

6. The process according to claim 1, wherein the energy input per slit and per machining cycle is carried out with a same sequence of laser pulses in which at least one of the laser pulses has a comparatively long pulse length for the energy input along the first length of the at least one first segment and a plurality of the laser pulses follow one another directly and have a comparatively small pulse amplitude for the energy input along the second length of the at least one second segment, and the pulse amplitude of the laser pulses with the comparatively long pulse length is not larger than the pulse amplitude of the laser pulses with the comparatively short pulse length.

7. The process according to claim 1, wherein the energy input per slit along the first length of the at least one first segment is carried out at least in the first of the machining cycles by means of at least one of the laser pulses, and along the slit length of the slit in further machining cycles the energy input is carried out with a same sequence of laser pulses, wherein the sequence of laser pulses comprises a larger quantity of laser pulses than laser pulses participating in the energy input per slit in the at least first machining cycle of the machining cycles, and the pulse length and the pulse amplitude of all of the laser pulses are constant at least over one of the machining cycles.

8. The process according to claim 1, further comprising machining of said second segments carried out subsequent to said machining cycles.