http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2013064658-A1

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classificationCPCAdditional http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D11-122
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08G59-686
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08L63-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D25-24
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D25-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08L63-00
filingDate 2011-05-31-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1058f1707ec9eb5f64cae89c7449ca81
publicationDate 2013-03-14-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-2013064658-A1
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.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10030540-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10107134-B2
priorityDate 2010-05-31-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4208777-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2009004453-A1
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Total number of triples: 29.