http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102006016703-A1

Outgoing Links

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_1ce17db423b2712f70a3001a199ec58e
classificationCPCAdditional http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T29-49318
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classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-005
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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D5-12
filingDate 2006-04-08-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_3f5f256d8c2bb67d3788cb7633fe94f2
publicationDate 2007-10-11-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber DE-102006016703-A1
titleOfInvention Method of repairing a vane segment
abstract methodnfor repairing a guide vane segment of a gas turbine, whereinnthe vane segment at least two vanes and an innernand an outer shroudnwherein at least one vane is irreparably damaged,nis separated from the vane segment, and the vane segmentnby joiningnat least one spare bucket is added. If one, irreparablenVane itself outsidenthe circumferential center of the vane segment is located in a segment half,nor if the multiple, irreparable vanes are in the samensegment halfnbe located firstnthe - matchingn- Number of vanes to be separated from the segment and thento join the segmentnReplacement blades determined. Then the determined number of spare bladesnjoined to the vane segment.nFinallynwill be the same number of vanes including thenat least one irreparable vane from the vane segmentnseparated.
priorityDate 2006-04-08-04:00^^<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.