http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2015080779-A2

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filingDate 2014-09-10^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_7dd6320b48f494a2a53f386d4ff87298
publicationDate 2015-06-04^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber WO-2015080779-A2
titleOfInvention Large displacement high temperature seal
abstract A seal assembly is provided for a gas turbine engine. This seal assembly includes a tadpole seal with a bulb and a tail, where the tail is directed toward a backwall. The seal assembly also includes a faying extension that at least partially extends into the channel and into contact with the bulb. An exhaust duct is also provided for a gas turbine engine. This exhaust duct includes a seal assembly between a first exhaust duct section and a second exhaust duct section. The seal assembly includes a tadpole seal with a bulb and a tail, where the tail is directed upstream.
priorityDate 2013-09-13^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

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