http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102005042272-A1

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filingDate 2005-09-06-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e9f25c0869c2fac1d45c506fce91e5dd
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publicationDate 2007-03-08-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber DE-102005042272-A1
titleOfInvention Turbomachine and sealing element for a turbomachine
abstract ThenInvention relates to a turbomachine,nin particular a gas turbine, with several in the axial direction of thenflow machinenalternately successively arranged blade rings (10,n11) and vane ringsn(12), wherein each blade ring (10, 11) more on a rotor base body (14)nmounted rotor blades (13), each rotor main body (14)nin the transition areanto the blades (13) forms a platform (15), which in the axial directionnthe turbomachinenacross fromnprojecting the blades (13), and wherein each vane ringn(12) a plurality of guide vanes (19) with a radially innernCovering (20). According to the invention is on the radially innernShroud (20) of at least one vane ring (12) at leastna flexible sealing element (22, 23) mounted, wherein sealing body (24)nthe or each flexible sealing element (22, 23) on each onenPlatform (15) of a rotor base bodyn(14) one upstreamnand / or downstreamnof the vane ring (12) positioned blade ringn(10, 11) abut.
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priorityDate 2005-09-06-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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