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Gas-Phase Combustion Synthesis of Metal and Ceramic NanoparticlesGas-phase combustion (flame) synthesis has been an essential industrial process for producing large quantities of powder materials such as carbon black, titanium dioxide, and silicon dioxide. Flames typically produce simple oxides, with carbon black being the noted exception because the oxides of carbon are gaseous and are easily separated from the particulate matter that is formed during fuel pyrolysis. The powders produced in flames are usually agglomerated, nanometer-sized particles (nanoparticles). This is an acceptable composition and morphology for many applications. However, recently there has been interest in flames for the synthesis of metal and non-oxide ceramic unagglomerated nanoparticles (2 to 100 nm) for advanced materials applications. For these applications nano-powders are consolidated into bulk materials under high temperature and pressure, yielding a solid part whose grains retain the nanometer size of the starting powder. The final nanostructured materials often possess unique mechanical, electrical or magnetic properties compared to their coarse-grained counterparts. The economics of powder processing can also be enhanced with nano-powders vis-a-vis low temperature consolidation and superplastic forming.
Document ID
19970020553
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
R L Axelbaum
(Washington University in St. Louis St Louis, United States)
B H Chao
(University of Hawaii System Honolulu, United States)
Date Acquired
August 17, 2013
Publication Date
May 1, 1997
Publication Information
Publication: Fourth International Microgravity Combustion Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Inorganic, Organic and Physical Chemistry
Report/Patent Number
NASA-CP-10194
Meeting Information
Meeting: Fourth International Microgravity Combustion Workshop
Location: Cleveland, OH
Country: US
Start Date: May 19, 1997
End Date: May 21, 1997
Sponsors: National Aeronautics and Space Administration
Accession Number
97N21826
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
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