http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2303155-C2

Outgoing Links

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_2b052a6a4de1db4b8efa5c1eb28ae72e
classificationCPCAdditional http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2230-90
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2300-5024
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2300-50212
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-64
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-64
filingDate 2003-05-28-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2007-07-20-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c5a3fd67610421435ebf21f8a6cf3d45
publicationDate 2007-07-20-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber RU-2303155-C2
titleOfInvention Web construction and member of space vehicle jet engine
abstract FIELD: space vehicle jet engine. n SUBSTANCE: web(2) subjected to the action of thermal loads has at least the first layer (5) and the second layer (6), which is positioned closer than the first layer to the heat source and through which the heat is transferred to the first layer. The offered web is featured by the fact that the first and second layers (5, 6) cam perceive the considerable part of the load acting on the web, the second layer (6) features a greater heat conduction and/or lower thermal expansion as compared with the first layer (5). n EFFECT: reduced thermal deformations arising in the web (2) under the action of heat load. n 2 cl, 3 dwg
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-185328-U1
priorityDate 2002-05-28-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

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Total number of triples: 19.