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Hot corrosion of ceramic engine materialsA number of commercially available SiC and Si3N4 materials were exposed to 1000 C in a high velocity, pressurized burner rig as a simulation of a turbine engine environment. Sodium impurities added to the burner flame resulted in molten Na2SO4 deposition, attack of the SiC and Si4N4 and formation of substantial Na2O-x(SiO2) corrosion product. Room temperature strength of the materials decreased. This was a result of the formation of corrosion pits in SiC, and grain boundary dissolution and pitting in Si3N4. Corrosion regimes for such Si-based ceramics have been predicted using thermodynamics and verified in rig tests of SiO2 coupons. Protective mullite coatings are being investigated as a solution to the corrosion problem for SiC and Si3N4. Limited corrosion occurred to cordierite (Mg2Al4Si5O18) but some cracking of the substrate occurred.
Document ID
19890006694
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Fox, Dennis S.
(NASA Lewis Research Center Cleveland, OH, United States)
Jacobson, Nathan S.
(NASA Lewis Research Center Cleveland, OH, United States)
Smialek, James L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Nonmetallic Materials
Report/Patent Number
NAS 1.15:101439
DOE/NASA/50111-2
E-4544
NASA-TM-101439
Meeting Information
Meeting: Automotive Technology Development Contractors Coordination Meeting
Location: Dearborn, MI
Country: United States
Start Date: October 24, 1988
End Date: October 27, 1988
Sponsors: DOE
Accession Number
89N16065
Funding Number(s)
PROJECT: RTOP 778-32-11
CONTRACT_GRANT: DE-AI01-85CE-50111
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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