Inventor · disambiguated record
John Charles Intile
Also filed as: INTILE JOHN · INTILE JOHN C · INTILE JOHN CHARLES
15 granted patents·5 pending applications·363 citations·filing 2004–2015
93Inventor score
Top patents by PatentIndex Score
20 records- 0198US7493767B2Method and apparatus for cooling combustor liner and transition piece of a gas turbineGEN ELECTRIC·Filed 2005·Granted Feb 24, 2009·66 cites·20 claims
- 0297US7010921B2Method and apparatus for cooling combustor liner and transition piece of a gas turbineGEN ELECTRIC·Filed 2004·Granted Mar 14, 2006·190 cites·24 claims
- 0393US7628062B2Method and system to determine composition of fuel entering combustorGEN ELECTRIC·Filed 2007·Granted Dec 8, 2009·31 cites·9 claims
- 0487US9968991B2Method and assembly for forming components having internal passages using a lattice structureGEN ELECTRIC·Filed 2015·Granted May 15, 2018·2 cites·22 claims
- 0586US8677753B2System for supplying a working fluid to a combustorMELTON PATRICK BENEDICT·Filed 2012·Granted Mar 25, 2014·9 cites·17 claims
- 0684US9334803B2Method of recovering energy in a steam-cooled gas turbineGEN ELECTRIC·Filed 2013·Granted May 10, 2016·8 cites·20 claims
- 0782US8024964B2Method and system to determine composition of fuel entering combustorGEN ELECTRIC·Filed 2009·Granted Sep 27, 2011·11 cites·9 claims
- 0878US8522554B2Fuel nozzle for a turbine engine with a passive purge air passagewayINTILE JOHN·Filed 2010·Granted Sep 3, 2013·5 cites·11 claims
- 0973US7970570B2Methods and systems for analysis of combustion dynamics in the time domainGEN ELECTRIC·Filed 2006·Granted Jun 28, 2011·9 cites·20 claims
- 1066US8818684B2Systems, methods, and apparatus for detecting failure in gas turbine hardwareJOHN JUSTIN V·Filed 2010·Granted Aug 26, 2014·4 cites·17 claims
- 1166US7757492B2Method and apparatus to facilitate cooling turbine enginesGEN ELECTRIC·Filed 2007·Granted Jul 20, 2010·10 cites·18 claims
- 1265US8087228B2Segmented combustor capMCMAHAN KEVIN WESTON·Filed 2008·Granted Jan 3, 2012·10 cites·9 claims
- 1362US8365532B2Apparatus and method for a gas turbine nozzleGEN ELECTRIC·Filed 2009·Granted Feb 5, 2013·0 cites·18 claims
- 1459US8402763B2Combustor headend guide vanes to reduce flow maldistribution into multi-nozzle arrangementMULHERIN JASON·Filed 2009·Granted Mar 26, 2013·8 cites·12 claims
- 1543US2013160456A1System and method for controlling oxygen emissions from a gas turbineSNOOK DANIEL DAVID·Filed 2011·Application pending·0 cites
- 1642US2010011770A1Gas Turbine Premixer with Cratered Fuel Injection SitesCHILA RONALD JAMES·Filed 2008·Application pending·0 cites
- 1739US8322141B2Power generation system including afirst turbine stage structurally incorporating a combustorINTILE JOHN CHARLES·Filed 2011·Granted Dec 4, 2012·0 cites·21 claims
- 1839US2009056336A1Gas turbine premixer with radially staged flow passages and method for mixing air and gas in a gas turbineGEN ELECTRIC·Filed 2007·Application pending·0 cites
- 1936US2010319353A1Multiple Fuel Circuits for Syngas/NG DLN in a Premixed NozzleINTILE JOHN CHARLES·Filed 2009·Application pending·0 cites
- 2034US2006010874A1Cooling aft end of a combustion linerINTILE JOHN C·Filed 2004·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →