http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CH-707021-A2

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filingDate 2013-09-16-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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publicationDate 2014-03-31-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CH-707021-A2
titleOfInvention Blade tip insert for a turbomachine.
abstract The invention relates to a blade tip of a turbomachine. The blade tip includes a top corner tape insert (66) having a retained portion (80) adapted to be held within a pocket (68) of a turbine blade (22), and a protruding portion (82) A dynamic seal having a stationary structural component surrounding the turbine blade (22).
priorityDate 2012-09-20-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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