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Improved silicon nitride for advanced heat enginesThe results of a four year program to improve the strength and reliability of injection-molded silicon nitride are summarized. Statistically designed processing experiments were performed to identify and optimize critical processing parameters and compositions. Process improvements were monitored by strength testing at room and elevated temperatures, and microstructural characterization by optical, scanning electron microscopes, and scanning transmission electron microscope. Processing modifications resulted in a 20 percent strength and 72 percent Weibull slope improvement of the baseline material. Additional sintering aids screening and optimization experiments succeeded in developing a new composition (GN-10) capable of 581.2 MPa at 1399 C. A SiC whisker toughened composite using this material as a matrix achieved a room temperature toughness of 6.9 MPa m(exp .5) by the Chevron notched bar technique. Exploratory experiments were conducted on injection molding of turbocharger rotors.
Document ID
19930020262
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yeh, Harry C.
(Allied-Signal Aerospace Co. Torrance, CA, United States)
Fang, Ho T.
(Allied-Signal Aerospace Co. Torrance, CA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1991
Subject Category
Composite Materials
Report/Patent Number
REPT-88-61608
NAS 1.26:182193
NASA-CR-182193
Report Number: REPT-88-61608
Report Number: NAS 1.26:182193
Report Number: NASA-CR-182193
Accession Number
93N29451
Funding Number(s)
CONTRACT_GRANT: NAS3-24385
PROJECT: RTOP 533-05-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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