Accession Number : AD0757063
Title : Fiber Reinforced Ceramic Matrix Composites.
Descriptive Note : Final rept. 15 Jan 72-15 Jan 73,
Corporate Author : UNITED AIRCRAFT RESEARCH LABS EAST HARTFORD CONN
Personal Author(s) : Brennan,J. J. ; De Crescente,M. A.
Report Date : 15 JAN 1973
Pagination or Media Count : 73
Abstract : Tungsten reinforced silicon nitride was found to increase the elevated temperature (1300C) Charpy impact strength by a factor of nine over monolithic Si3N4, primarily due to the energy absorbing mechanism of fiber pullout. However, the room temperature Charpy impact strength of tungsten reinforced Si3N4 is not increased over that of monolithic Si3N4 due to the brittle nature of the silicide reaction product at the Si3N4-W interface and the notch sensitivity of tungsten. Tantalum wire reinforced Si3N4 was found to increase the room temperature Charpy impact strength of Si3N4 by a factor of 30 (0.5 ft-lbs to 14.8 ft-lbs) and also to affect the mode of failure such that interfacial splitting along with ductile fiber elongation occurs, resulting in very small fragments of matrix breaking off upon impact. This mode of fracture is desirable for use in gas turbine engines. (Author Modified Abstract)
Descriptors : (*COMPOSITE MATERIALS, CERAMIC MATERIALS), SILICON COMPOUNDS, NITRIDES, TUNGSTEN, TANTALUM, FIBERS, REINFORCING MATERIALS, GAS TURBINES, IMPACT SHOCK, SHOCK RESISTANCE, OXIDATION, RUPTURE
Subject Categories : Laminates and Composite Materials
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE