http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9482114-B2

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filingDate 2011-05-31-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2016-11-01-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1058f1707ec9eb5f64cae89c7449ca81
publicationDate 2016-11-01-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-9482114-B2
titleOfInvention Compressor case lining
abstract A lining for a compressor case in use with a gas turbine engine compressor is provided. The compressor includes a compressor casing, which is generally comprised of a first and second half. Inside the casing is a plurality of vanes attached to a plurality of vane bands. The vane bands are affixed to the interior of the compressor casing. A lining, comprising a carbon fiber reinforced-type material is applied to the interior of the compressor casing over the vane bands. The lining allows a minimal clearance to be between the lining and wheel blade tips spinning within the compressor casing. The carbon fiber in the lining allows the lining to withstand a high number of temperature cycles due to the use of the compressor and the gas turbine engine.
priorityDate 2010-05-31-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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