http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8844262-B2

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filingDate 2010-12-21^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2014-09-30^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1d9b49aca11f371adfdd4f2f1aec943a
publicationDate 2014-09-30^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-8844262-B2
titleOfInvention Exhaust for a gas turbine engine
abstract A gas turbine engine is provided having an offtake passage that in one form is capable of extracting a bypass flow from the engine. The airflow traversing the offtake passage is introduced to an exhaust flow of the gas turbine engine through an offtake outlet. The offtake outlet includes an airflow member that is moveable. A nozzle is also provided for exhaust from the gas turbine engine. In one form the nozzle includes moveable duct members. Flows exiting the offtake outlet and the nozzle can be combined after passing the airflow member and the moveable duct members, respectively.
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http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9964035-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10436073-B2
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http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9874143-B2
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http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9970354-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10584615-B2
priorityDate 2009-12-29^^<http://www.w3.org/2001/XMLSchema#date>
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