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The microstructure and properties of rapidly solidified, dispersion-strengthened NiAlAn advanced rapid solidification technology for processing reactive and refractory alloys, utilized to produce large quantities of melt-spun filaments of NiAl, is presented. The melt-spun filaments are pulverized to fine particle sizes, and subsequently consolidated by hot extrusion or hot isostatic pressing. Rapid solidification process gives rise to very fine-grained microstructures. However, exposure to elevated temperature during hot consolidation leads to grain growth. Alloying agents such as borides, carbides, and tungsten can pin the grain boundaries and retard the grain growth. Various alloy compositions are investigated. The eventual goal is to utilize the hot-extruded and forged stock to grow single-crystal NiAl blades for advanced gas-turbine engine applications. Single-crystal NiAl, containing a uniform dispersion of carbide strengthening precipitates, is expected to lead to highly creep-resistant turbine blades, and is of considerable interest to the aerospace propulsion industry.
Document ID
19910028727
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Jha, S. C.
(Texas Instruments, Inc. Dallas, United States)
Ray, R.
(Marko Materials, Inc. North Billerica, MA, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1990
Publication Information
Publication: JOM
Volume: 42
ISSN: 1047-4838
Subject Category
Metallic Materials
Accession Number
91A13350
Funding Number(s)
CONTRACT_GRANT: NAS3-25448
Distribution Limits
Public
Copyright
Other

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