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ECA Subsurface Crack Detection


SubSurface Crack Detection

Commercial and military aircraft are built by joining overlapping aluminum sheets together with thousands of fasteners. Fatigue cracks on the underlying layers of aluminum are often concealed by the first sheet layer. To guarantee the integrity of any airplane, these hidden flaws must be detected and repaired during regular in-service inspections.

As a part of its series of aerospace solutions, Olympus proposes an innovative fastener and subsurface crack inspection technique, which propels eddy current technology into previously uncharted territory. This new technology provides an incredibly clear image of cracks under the first layer of aluminum aircraft skin, providing efficient and reliable results.

Features

  • Replaces magneto-optical imaging (MOI).
  • The 32-coil probe provides large coverage.
  • Avoids paint removal; simplified process equals time-savings.
  • With continuous mode, the scan imagery reveals inspection results without interruption.
  • Data recording for professional reports.
  • Probe positioning not as critical as a sliding probe.
  • Optimized to detect typical subsurface cracks in aluminum sheets of commercial and military aircraft.

Subsurface Crack Area

Standard_RSTD_10123.psd

Conventional eddy current impedance plane with a 32-channel signal Subsurface Crack Detail Screen Crack orientation on the right
  Crack on both sides of the fastener
  Zipper crack indication
Detailed subsurface crack ECA imagery Crack orientation on the left
  Good fastener indication
   

Olympus IMS
Products used for this application

Performs eddy current array testing inspections. The test configuration supports 32 sensor coils (up to 64 with an external multiplexer) working in bridge or transmit-receive mode. The operating frequency ranges from 20 Hz to 6 MHz with the option of using multiple frequencies in the same acquisition.
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