Title of article :
Tensile creep of directionally solidified NiAl–9Mo in situ composites
Author/Authors :
L. Hu، نويسنده , , G. Zhang، نويسنده , , W. Hu، نويسنده , , G. Gottstein، نويسنده , , S. Bogner، نويسنده , , A. Bührig-Polaczek، نويسنده ,
Issue Information :
دوهفته نامه با شماره پیاپی سال 2013
Pages :
11
From page :
7155
To page :
7165
Abstract :
Well-aligned Mo fiber-reinforced NiAl in situ composites were produced by specially controlled directional solidification. The creep behavior parallel to the growth direction was studied in static tensile tests at temperatures between 900 °C and 1200 °C. A steady-state creep rate of 10−6 s−1 was measured at 1100 °C under an initial applied tensile stress of 150 MPa. Compared to binary NiAl and previously investigated NiAl–Mo eutectics with irregularly oriented Mo fibers, this value demonstrates a remarkably improved creep resistance in NiAl–Mo with well-aligned unidirectional Mo fibers. A high-resolution transmission electron microscope investigation of the NiAl/Mo interface revealed a clean semi-coherent boundary between NiAl and Mo, which enabled an effective load transfer from the NiAl matrix to the Mo fibers, and thus leads to the remarkably increased creep strength. The stress exponent, n, was found to be between 3.5 and 5, dependent on temperature. The activation energy for creep, Qc, was measured to be 291 ± 19 kJ mol–1, which is close to the value for self-diffusion in binary NiAl. Transmission electron microscopy observations substantiated that creep occurred by dislocation climb in the NiAl matrix. The Mo fiber was found to behave in a quasi-rigid manner during creep. A creep model for fiber-reinforced metal matrix composites was applied for an in-depth understanding of the mechanical behavior of the individual components and their contribution to the creep strength of the composite.
Keywords :
Creep resistance , Interface , Fiber reinforced composite
Journal title :
ACTA Materialia
Serial Year :
2013
Journal title :
ACTA Materialia
Record number :
1147321
Link To Document :
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