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Evaluation of bonded boron/epoxy doublers for commercial aircraft aluminum structuresAn 18 month laboratory test and stress analysis program was conducted to evaluate bonded boron/epoxy doublers for repairing cracks on aluminum aircraft structures. The objective was to obtain a core body of substantiating data which will support approval for use on commercial transports of a technology that is being widely used by the military. The data showed that the doublers had excellent performance.
Document ID
19950008043
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Belason, Bruce (Textron Specialty Materials Lowell, MA, United States)
Rutherford, Paul (Textron Specialty Materials Lowell, MA, United States)
Miller, Matthew (Textron Specialty Materials Lowell, MA, United States)
Raj, Shreeram (Textron Specialty Materials Lowell, MA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1994
Publication Information
Publication: NASA. Langley Research Center, FAA(NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance
Subject Category
Structural Mechanics
Accession Number
95N14457
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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