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Effect of braze processing on the microstructure and mechanical properties of SCS-6/beta21S titanium matrix compositesAn investigation is conducted of the effects of braze processing on the microstructure and tensile properties of SiC fiber-reinforced Ti-15Mo-2.7Nb-3Al-0.25Si-matrix composite (TMC) laminates; the brazing alloy was the commercial Ti-15Cu-15Ni, in both its conventional and metglass forms. Tensile tests conducted at room temperature, 1200 F, and 1500 F showed that the braze processes (1) had little effect on tensile properties, and (2) appeared to degrade neither the reinforcing fibers not the fiber/matrix interfacial bondline.
Document ID
19930038296
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hoffman, Eric K. (NASA Langley Research Center Hampton, VA, United States)
Bird, R. K. (NASA Langley Research Center Hampton, VA, United States)
Dicus, Dennis L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
December 1, 1992
Subject Category
Composite Materials
Report/Patent Number
AIAA PAPER 92-5017
Meeting Information
Meeting: AIAA, International Aerospace Planes Conference
Location: Orlando, FL
Country: United States
Start Date: December 1, 1992
End Date: December 4, 1992
Sponsors: AIAA
Accession Number
93A22293
Distribution Limits
Public
Copyright
Other

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