http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-102203308-B

Outgoing Links

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_43e68f0500fafcd32413257a81de6ad7
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classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C22F1-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C22C14-00
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C22F1-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C22C14-00
filingDate 2009-11-06-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2014-05-07-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1380f32d1632094088b78cce5fdf0121
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_93c2a2831ceef56d2b63b2691ece52d3
publicationDate 2014-05-07-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-102203308-B
titleOfInvention Methods for the manufacture of a titanium alloy for use in combustion engine exhaust systems
abstract Methods for the manufacture of the above-mentioned titanium alloy for use in combustion engine exhaust systems are disclosed herein. An exemplary method of the disclosed subject matter for the manufacture of titanium alloy for use in a high temperature and high stress environment includes performing a first heat treatment of the titanium alloy at a first temperature, rolling the titanium alloy to a desired thickness, performing a second heat treatment of the titanium alloy at a second temperature, and performing a third heat treatment of the titanium alloy at a third temperature. In some embodiments, the first temperature is selected such that recrystallization and softening of the titanium alloy is optimized without substantial coarsening of second phase particles and can be approximately 1500-1600 DEG F. In some embodiments, the rolling of the titanium alloy reduces the thickness of the titanium alloy by at least than 65%.
priorityDate 2008-11-06-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

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http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419578708

Total number of triples: 18.