http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-104763479-A

Outgoing Links

Predicate Object
assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_80d21b615b5cbb00bb46fca529dc0ddc
classificationCPCAdditional http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-37
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http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-225
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D9-04
filingDate 2008-01-08-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_cd9f710b929b4fe399807809e1abfb2c
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_7a6e1b31c276dbd62f09894f8b5e8edb
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http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_41ace2b0b0eea7438fb49bb8fa993d8d
publicationDate 2015-07-08-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-104763479-A
titleOfInvention Method of manufacturing turbine diaphragm
abstract The invention relates to a method for manufacturing a turbine diaphragm. The turbine diaphragm (10) comprises an annulus of static blades and an outer diaphragm ring (33) surrounding the annulus of static blades and welded to the outer platforms (32). Each static blade comprises an inner platform (31), an aerofoil (30) and an outer platform (32). The inner platforms (31) serve the function of an inner diaphragm ring, thereby reducing material and manufacturing costs. Furthermore, confronting edges (83(i)) of the inner platforms (31) have an interference fit with each other and the aerofoils (30) are in a state of torsional stress between the inner and outer platforms. The latter two features improve the dynamic characteristics of the diaphragm.
priorityDate 2007-01-12-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

Predicate Subject
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Total number of triples: 19.