4.6 Article

Active Thermography for the Detection of Sub-Surface Defects on a Curved and Coated GFRP-Structure

Journal

APPLIED SCIENCES-BASEL
Volume 11, Issue 20, Pages -

Publisher

MDPI
DOI: 10.3390/app11209545

Keywords

active thermography; sub-surface defects; defect visualization; automatic defect detection; leading edge; wind turbine rotor blade; coated and curved surface; GFRP-structure

Funding

  1. Bundesministerium fuer Wirtschaft und Energie (BMWI) [20794 N/2]
  2. Arbeitsgemeinschaft industrieller Forschung (AIF)

Ask authors/readers for more resources

This study utilized long-pulse thermography for the first time to detect sub-surface defects on a curved and coated test specimen, successfully detecting defects with a depth-to-diameter ratio of up to 1.04. Additionally, defects were detectable from a non-perpendicular viewing angle, showing promising potential for on-site application during the inspection of rotor blade leading edges.
Initial defects, for example, those occurring during the production of a rotor blade, encourage early damages such as rain erosion at the leading edge of wind turbine rotor blades. To investigate the potential that initial defects have for early damage, long-pulse thermography as a non-destructive and contactless measurement technique is applied to a strongly curved and coated test specimen for the first time. This specimen is similar in structural size and design to a rotor blade leading edge and introduced with sub-surface defects whose diameters range between 2mm and 3.5mm at depths between 1.5mm and 2.5mm below the surface. On the curved and coated test specimen, sub-surface defects with a depth-to-diameter ratio of up to 1.04 are successfully detected. In particular, defects are also detectable when being observed from a non-perpendicular viewing angle, where the intensity of the defects decreases with increasing viewing angle due to the strong surface curvature. In conclusion, long-pulse thermography is suitable for the detection of sub-surface defects on coated and curved components and is therefore a promising technique for the on-site application during inspection of rotor blade leading edges.

Authors

I am an author on this paper
Click your name to claim this paper and add it to your profile.

Reviews

Primary Rating

4.6
Not enough ratings

Secondary Ratings

Novelty
-
Significance
-
Scientific rigor
-
Rate this paper

Recommended

No Data Available
No Data Available