Eddy current detection of short cracks under installed fasteners

Materials Evaluation

Volumn 55, Issue 1, 1997, Pages 25-30

  Hagemaier, Don ^a   Kark, Greg ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CRACK DETECTION; AIRCRAFT MATERIALS; COMPUTER SIMULATION; CRACKS; EDDY CURRENT TESTING; FATIGUE OF MATERIALS;

EDDY CURRENT DETECTION; SHORT-CRACKS;

EDDY CURRENT TESTING; FUSELAGES;

ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES; SHORT CRACKS;

EID: 0030844227     PISSN: 00255327     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (5)

1. Buckley, J., and J. Calvert, Improved Eddy Current Techniques for the Aerospace Industry. Hocking NDT Ltd., St Albans, England, 1995.
2. Gibbs, M., Pulsed Eddy Current vs Other Eddy Current Methods for Inspection of Aircraft Structure, Staveley Instruments, Inc., Kennewick, WA. Sep 1990.
3. Sheppard, W. WL-TR-94-4006: Bddy Current for Detecting Second Layer Cracks Under Installed Fasteners, Wright Patterson Air Force Base, OH, 1994.
4. Sheppaid. W, AFWAL-TR-85-4095: Manufacturing Technology for Advanced Second Layer NDE System Producibility, Wright Patterson Air Force Base, OH, 1985.
5. Spencer, F., and D. Schurman, Reliability Assessment at Airline Inspection Facilities, Vol. III, DOT/FAA/CT-92/12, III, FAA Technical Center, Atlantic City, NJ,1995.