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Thick thermal barrier coatings for diesel componentsAn engineered thick thermal barrier coating consisting of multiple layers of zirconia and CoCrAlY with a zirconia top layer and having a system thermal conductance less than 410 w/m(exp 2)K exceeded the 100 hour engine durability goals set forth in this program. The thermal barrier coatings were intact at the test conclusion. Back to back single cylinder research engine tests were conducted with watercooled, metal hardware and oil-cooled, thermal barrier coating insulated hardware to determine apparent heat release and fuel economy. Apparent heat release data revealed that the insulated engine had a shorter ignition delay and a longer combustion duration than the metal engine. The insulated engine fuel economy was approximately two percent worse on average for this series of tests. There was no attempt to optimize engine efficiency of the insulated engine by modifying the engine timing, coating, or other techniques.
Document ID
19940024847
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yonushonis, T. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Subject Category
Urban Technology And Transportation
Report/Patent Number
NAS 1.26:187111
DOE/NASA/0331-1
NASA-CR-187111
Report Number: NAS 1.26:187111
Report Number: DOE/NASA/0331-1
Report Number: NASA-CR-187111
Accession Number
94N29350
Funding Number(s)
CONTRACT_GRANT: DEN3-331
CONTRACT_GRANT: DE-AI01-86CE-50162
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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