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In-service health monitoring of composite structuresThe aerospace industry is witnessing a vast utilization of composites in critical structural applications and anticipates even more use of them in future aircraft. Therefore, a definite need exists for a composite health monitoring expert system to meet today's current needs and tomorrow's future demands. The primary goal for this conceptual health monitoring system is functional reliably for in-service operation in the environments of various composite structures. The underlying philosophy of this system is to utilize proven vibration techniques to assess the structural integrity of a fibrous composite. Statistical methods are used to determine if the variances in the measured data are acceptable for making a reliable decision on the health status of the composite. The flexible system allows for algorithms describing any composite fatigue or damage behavior characteristic to be provided as an input to the system. Alert thresholds and variances can also be provided as an input to this system and may be updated to allow for future changes/refinements in the composite's structural integrity behavior.
Document ID
19910067303
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pinto, Gino A.
(Technology Integration and Development Group, Inc. Billerica, MA, United States)
Ventres, C. S.
(Technology Integration and Development Group, Inc. Billerica, MA, United States)
Ginty, Carol A.
(Technology Integration and Development Group, Inc. Billerica, MA, United States)
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Quality Assurance And Reliability
Accession Number
91A51926
Distribution Limits
Public
Copyright
Other

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