http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2011208639-A

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filingDate 2011-03-22^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2b7f109a6df1231e7629a77d2c997359
publicationDate 2011-10-20^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber JP-2011208639-A
titleOfInvention Gas turbine blade with serpentine cooled platform and associated method
abstract A cooling circuit for a turbine blade (10) having a body (14), a platform (18), and a blade (12) is provided. The cooling circuit is a first cooling passage (38) extending from an inlet (20) disposed at a radially inner end of the barrel (14), and communicates with a turbine wheel space. And a first cooling passage (38) for supplying cooling air to a serpentine cooling circuit (24) extending across at least one region of the platform (18) when in use. The serpentine cooling circuit (24) connects to a separate internal cooling circuit in the blade (12) so that the cooling air used to cool the platform (18) is reused in the blade cooling circuit. It has become. [Selection] Figure 3
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2017078409-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2017101670-A
priorityDate 2010-03-26^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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