http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10982553-B2

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filingDate 2018-12-03-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2021-04-20-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_aabd420fbf64cbb86cdc486ca6b0a5fc
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publicationDate 2021-04-20-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-10982553-B2
titleOfInvention Tip rail with cooling structure using three dimensional unit cells
abstract A tip for a turbine component, turbine rotor blade or tip of a blade, is disclosed. The tip includes a tip plate configured to be coupled at a tip end of an airfoil chamber; and a tip rail extending radially from the tip plate, the tip rail disposed near or at a periphery of the tip plate. The trip rail includes a cooling structure constituting at least a portion of the tip rail. The cooling structure is in fluid communication with the airfoil chamber, and includes a plurality of repeating, three dimensional unit cells. Each unit cell defines a flow passage that is in fluid communication with the flow passage of at least one other unit cell. The flow passages of the 3D unit cells create a tortuous cooling passage in at least a portion of the tip rail.
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