ISSN:
1662-9752
Source:
Scientific.Net: Materials Science & Technology / Trans Tech Publications Archiv 1984-2008
Topics:
Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
Notes:
NiAl-based alloy is a promising material applied in the fields of aeronautic and astronauticinstruments. In the paper the compression deformation behavior and microstructure evolution ofNiAl-Cr(Mo)-Hf alloy at elevated temperature were studied. The results demonstrate that the alloybehaves good formability in the temperature ranging from 1320°C to 1360°C, in which the maximuminitial strain rate is about 8.3×10-4s-1 and the maximum deformation resistance is lower than 40MPa.During compression at temperature between 1250°C and 1300°C the flow stress increased sharplywith the increasing of the deformation degree. When compression deformation at 1320°C~1360°C,the flow stress decreased obviously and the flow stress decreased slightly after reached the maximumvalue. By analyzing the microstructure evolution during compression it can be concluded thatas-casting microstructure was improved in deformation. The grains were refined and the brittle phasesof lamellar Cr(Mo) existing at NiAl matrix were broken. The porosities in as-casting material wereeliminated during compression and the density of the material increased. The fracture toughness ofthe alloy increased from 6.4MPa·m1/2 to 9.8MPa·m1/2 after compression
Type of Medium:
Electronic Resource
URL:
http://www.tib-hannover.de/fulltexts/2011/0528/02/16/transtech_doi~10.4028%252Fwww.scientific.net%252FMSF.551-552.457.pdf
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