In the automobile and aviation industries, composite materials are the key to lightweight efficiency. Composites containing carbon fibre reinforcements are of particular interest due to their supreme stiffness-to-weight-ratio, but the machining of this material class is still a challenge in production, rework, and repair. Laser technology presents a powerful solution to this obstacle.

Laser ablation is a technique that can be utilised for repair preparation of composites. However, for largescale industrial acceptance laser processes must incorporate a high degree of automation. In this paper, an approach to fully automatic control of the laser-based repair preparation is presented. It features two process monitoring techniques: Fibre orientation detection and short coherent interferometry. Both techniques aim to support the material ablation process by enabling homogeneous material removal to a specific material layer or specified depth.

Between laser scanning cycles, a camera-based system scans the processed surface and measures the fibre orientation in each pixel with regard to an adjustable tolerance. When scarfing composite parts made from non-crimped carbon fibres, this technique can be used to detect the transition between two consecutive layers. Areas in the scarfing zone that reveal fibres of the next layer will be excluded from further laser scanning until the current fibre layer is completely ablated.

Composite parts reinforced by crimped fabrics are similarly processed, but since single material layers are not easily identified, the ablation process is not controlled by fibre orientation measurements. Instead short coherent interferometry is used to detect the ablated depth and compare it to the part’s ideal layer thickness. Areas in the scarf zone that have reached the desired depth are excluded from further laser scanning. This technique is also applicable for non-crimped fabrics.

The results show, when the laser-based repair preparation is controlled by these techniques that precise scarfings can be achieved.

1.
Dittmar
,
H.
,
Gäbler
,
F.
,
Stute
,
U.
,
2013
.
UV-laser ablation of fibre reinforced composites with ns-pulses
.
Physics Procedia
41
, pp.
266
275
.
2.
Wolynski
,
A.
,
Herrmann
,
T.
,
Mucha
,
P.
,
Haloui
,
H.
,
L’huillier
,
J.
,
2011
.
Laser ablation of CFRP using picosecond laser pulses at different wavelengths from UV to IR
,
Physics Procedia
12
, pp.
292
301
.
3.
Zahedi
,
E.
,
Freitag
,
C.
,
Wiedenmann
,
M.
,
Onuseit
,
V.
,
Weber
,
R.
,
Graf
,
T.
,
2015
.
High Ablation Rate Laser Processing of CFRP for Repair Purpose
. In:
Proceedings of ICALEO 2015
.
International Congress on Applications of Lasers & Electro-Optics.
Atlanta
. 18th-22nd October.
4.
Dittmar
,
H.
,
Bluemel
,
S.
,
Jaeschke
,
P.
,
Suttmann
,
O.
,
Overmeyer
,
L.
,
2017
.
High-power laser surface processing for fast, reliable repair preparation of CFRP
. In:
Proceedings of Lasers in Manufacturing Conference (LiM
).
Munich
.
5.
Boley
,
S.
,
Holder
,
D.
,
Onuseit
,
V.
,
Graf
,
T.
,
Buser
,
M.
,
Schönleber
,
M.
,
2017
.
Distance controlled laser ablation of CFRP
. In:
Proceedings of Lasers in Manufacturing Conference (LiM
).
Munich
.
6.
Dittmar
,
H.
,
Jaeschke
,
P.
,
Suttmann
,
O.
,
Kaierle
,
S.
,
Overmeyer
,
L.
,
2018
.
Online laser-based repair preparation of CFRP supported by short coherent interferometry
. In:
Proceedings of 10th CIRP Conference on Photonic Technologies (LANE
). Fürth. https://www.lane-conference.org/industrial-contributions-2018
7.
Zambal
,
S.
,
Palfinger
,
W.
,
Stöger
,
M.
,
Eitzinger
,
C.
,
2015
.
Accurate fibre orientation measurement for carbon fibre surfaces
.
Pattern Recognition
48
, Issue
11
, pp.
3324
3332
.
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