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Wire Crimp Termination Verification Using Ultrasonic InspectionThe development of a new ultrasonic measurement technique to quantitatively assess wire crimp terminations is discussed. The amplitude change of a compressional ultrasonic wave propagating through the junction of a crimp termination and wire is shown to correlate with the results of a destructive pull test, which is a standard for assessing crimp wire junction quality. Various crimp junction pathologies such as undercrimping, missing wire strands, incomplete wire insertion, partial insulation removal, and incorrect wire gauge are ultrasonically tested, and their results are correlated with pull tests. Results show that the nondestructive ultrasonic measurement technique consistently (as evidenced with destructive testing) predicts good crimps when ultrasonic transmission is above a certain threshold amplitude level. A physics-based model, solved by finite element analysis, describes the compressional ultrasonic wave propagation through the junction during the crimping process. This model is in agreement within 6% of the ultrasonic measurements. A prototype instrument for applying this technique while wire crimps are installed is also presented. The instrument is based on a two-jaw type crimp tool suitable for butt-splice type connections. Finally, an approach for application to multipin indenter type crimps will be discussed.
Document ID
20070034160
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Perey, Daniel F.
(NASA Langley Research Center Hampton, VA, United States)
Cramer, K. Elliott
(NASA Langley Research Center Hampton, VA, United States)
Yost, William T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
October 22, 2007
Subject Category
Electronics And Electrical Engineering
Meeting Information
Meeting: SAE Aerospace Electrical Interconnect System Symposium (AEISS)
Location: Savannah, GA
Country: United States
Start Date: October 22, 2007
End Date: October 26, 2007
Sponsors: Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: FAA DTFACT-06-X-00003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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