Integrated Hole and Countersink Inspection of Aircraft Components

Paper #:
  • 2013-01-2147

Published:
  • 2013-09-17
DOI:
  • 10.4271/2013-01-2147
Citation:
Smith, J. and Kochhar-Lindgren, D., "Integrated Hole and Countersink Inspection of Aircraft Components," SAE Technical Paper 2013-01-2147, 2013, doi:10.4271/2013-01-2147.
Pages:
4
Abstract:
Precision hole inspection is often required for automated aircraft assembly. Direct contact measurement has been proven reliable and accurate for over 20 years in production applications. At the core of the hole measurement process tool are high precision optical encoders for measurement of diameter and countersink depth. Mechanical contact within the hole is via standard 2-point split ball tips, and diametric data is collected rapidly and continuously enabling the system to profile the inner surface at 0 and 90 degrees. Hole profile, countersink depth, and grip length data are collected in 6 seconds. Parallel to the active process, auto-calibration is performed to minimize environmental factors such as thermal expansion. Tip assemblies are selected and changed automatically. Optional features include concave countersink and panel position measurement.
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