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Engine CoatingsIncreasing the operating temperature of turbine engines reduces fuel consumption and increases engine efficiency. However, engine components must be protected from excessive heat. Lewis Research Center has successfully developed thermal barrier coatings (TBCs), which are deposited on the components. They insulate, offer oxidation and corrosion resistance and increase adherence. Surface temperatures can be reduced by 200 degrees centigrade or more. G. E. Aircraft Engines, a Lewis contractor, now uses a TBC based on the one developed at Lewis, on production engines. The system, which consists of a bond and a top coat extends component life from 1.3 to 2 times. The company is also testing TBCs on components that operate at higher temperatures.
Document ID
20020083266
Acquisition Source
Legacy CDMS
Document Type
Other
Date Acquired
August 20, 2013
Publication Date
January 1, 1992
Publication Information
Publication: Spinoff 1992
ISBN: 0-16-038211-4
Subject Category
Nonmetallic Materials
Report/Patent Number
ISBN: 0-16-038211-4
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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