http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CA-2070521-A1

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filingDate 1992-06-04-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_db0ea592960f22fa051adbf1d4a46bcd
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publicationDate 1993-01-10-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CA-2070521-A1
titleOfInvention Heat shield for a compressor/stator structure
abstract ABSTRACT OF THE DISCLOSURE A heat shield mechanism for thermally protecting a casing located in a turbine engine having a plurality of honeycomb cells which are connected to a support plate. A spring in contact with the support plate and in contact with a vane liner exerts a force on the support plate which causes at least one of the plurality of honeycomb cells to be pressed against the casing.
priorityDate 1991-07-09-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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Total number of triples: 27.