Inventor · disambiguated record
Ronald James Chila
Also filed as: CHILA RONALD · CHILA RONALD J · CHILA RONALD JAMES
45 granted patents·21 pending applications·409 citations·filing 2001–2023
98Inventor score
Files withGEN ELECTRIC27CHILA RONALD JAMES9BOARDMAN GREGORY ALLEN5MCMAHAN KEVIN WESTON5DAVIS JR LEWIS BERKLEY4
Top patents by PatentIndex Score
66 records- 0196US8307657B2Combustor liner cooling systemCHILA RONALD JAMES·Filed 2009·Granted Nov 13, 2012·47 cites·23 claims
- 0295US9759425B2System and method having multi-tube fuel nozzle with multiple fuel injectorsGEN ELECTRIC·Filed 2013·Granted Sep 12, 2017·14 cites·14 claims
- 0395US9212823B2Systems and methods for suppressing combustion driven pressure fluctuations with a premix combustor having multiple premix timesBOARDMAN GREGORY ALLEN·Filed 2012·Granted Dec 15, 2015·20 cites·17 claims
- 0495US8919127B2System and method for flow control in gas turbine engineMELTON PATRICK BENEDICT·Filed 2011·Granted Dec 30, 2014·20 cites·19 claims
- 0595US8671691B2Hybrid prefilming airblast, prevaporizing, lean-premixing dual-fuel nozzle for gas turbine combustorBOARDMAN GREGORY ALLEN·Filed 2010·Granted Mar 18, 2014·21 cites·16 claims
- 0689US9074773B2Combustor assembly with trapped vortex cavityBOARDMAN GREGORY ALLEN·Filed 2012·Granted Jul 7, 2015·11 cites·13 claims
- 0788US8683804B2Premixing apparatus for fuel injection in a turbine engineBOARDMAN GREGORY ALLEN·Filed 2009·Granted Apr 1, 2014·25 cites·19 claims
- 0886US9217373B2Fuel nozzle for reducing modal coupling of combustion dynamicsGEN ELECTRIC·Filed 2013·Granted Dec 22, 2015·5 cites·18 claims
- 0984US9182123B2Combustor fuel nozzle and method for supplying fuel to a combustorBOARDMAN GREGORY ALLEN·Filed 2012·Granted Nov 10, 2015·8 cites·18 claims
- 1084US9182122B2Combustor and method for supplying flow to a combustorMATTHEWS JOHN M·Filed 2011·Granted Nov 10, 2015·13 cites·20 claims
- 1183US10578306B2Liquid fuel cartridge unit for gas turbine combustor and method of assemblyGEN ELECTRIC·Filed 2017·Granted Mar 3, 2020·3 cites·18 claims
- 1283US9765973B2System and method for tube level air flow conditioningGEN ELECTRIC·Filed 2013·Granted Sep 19, 2017·4 cites·20 claims
- 1382US8438856B2Effusion cooled one-piece can combustorCHILA RONALD JAMES·Filed 2009·Granted May 14, 2013·18 cites·13 claims
- 1482US8387397B2Flow conditioner for use in gas turbine component in which combustion occursCHEN WEI·Filed 2009·Granted Mar 5, 2013·21 cites·6 claims
- 1582US6882068B2Forced air stator ventilation system and stator ventilation method for superconducting synchronous machineGEN ELECTRIC·Filed 2002·Granted Apr 19, 2005·33 cites·22 claims
- 1681US12305860B2Bundled tube fuel nozzle assembly for gas turbine combustorGE INFRASTRUCTURE TECHNOLOGY LLC·Filed 2023·Granted May 20, 2025·0 cites·18 claims
- 1781US8646277B2Combustor liner for a turbine engine with venturi and air deflectorCHILA RONALD JAMES·Filed 2010·Granted Feb 11, 2014·8 cites·19 claims
- 1880US8590314B2Combustor liner helical cooling apparatusMCMAHAN KEVIN WESTON·Filed 2010·Granted Nov 26, 2013·6 cites·20 claims
- 1979US9650959B2Fuel-air mixing system with mixing chambers of various lengths for gas turbine systemGEN ELECTRIC·Filed 2013·Granted May 16, 2017·6 cites·20 claims
- 2079US6680549B2Tapered rotor-stator air gap for superconducting synchronous machineGEN ELECTRIC·Filed 2001·Granted Jan 20, 2004·23 cites·27 claims
- 2178US8353165B2Combustor assembly for use in a turbine engine and methods of fabricating sameGEN ELECTRIC·Filed 2011·Granted Jan 15, 2013·6 cites·20 claims
- 2277US9115808B2Transition piece seal assembly for a turbomachineSIMMONS SCOTT ROBERT·Filed 2012·Granted Aug 25, 2015·4 cites·15 claims
- 2376US10982593B2System and method for combusting liquid fuel in a gas turbine combustor with staged combustionGEN ELECTRIC·Filed 2017·Granted Apr 20, 2021·2 cites·14 claims
- 2476US8082739B2Combustor exit temperature profile control via fuel staging and related methodCHILA RONALD JAMES·Filed 2010·Granted Dec 27, 2011·5 cites·13 claims
- 2575US9249679B2Impingement sleeve and methods for designing and forming impingement sleeveBERKEBILE MATTHEW PAUL·Filed 2012·Granted Feb 2, 2016·5 cites·20 claims
- 2674US8245515B2Transition duct aft end frame cooling and related methodDAVIS JR LEWIS B·Filed 2008·Granted Aug 21, 2012·15 cites·12 claims
- 2772US8915087B2Methods and systems for transferring heat from a transition nozzleMCMAHAN KEVIN WESTON·Filed 2011·Granted Dec 23, 2014·4 cites·20 claims
- 2871US8826667B2System and method for flow control in gas turbine engineMELTON PATRICK BENEDICT·Filed 2011·Granted Sep 9, 2014·4 cites·22 claims
- 2970US8646276B2Combustor assembly for a turbine engine with enhanced coolingDAVIS JR LEWIS BERKLEY·Filed 2009·Granted Feb 11, 2014·10 cites·14 claims
- 3069US10684016B2Aft frame assembly for gas turbine transition pieceGEN ELECTRIC·Filed 2017·Granted Jun 16, 2020·1 cites·17 claims
- 3169US9671112B2Air diffuser for a head end of a combustorGEN ELECTRIC·Filed 2013·Granted Jun 6, 2017·3 cites·20 claims
- 3267US8322976B2High temperature seal for a turbine engineCHILA RONALD JAMES·Filed 2008·Granted Dec 4, 2012·10 cites·20 claims
- 3367US8186167B2Combustor transition piece aft end cooling and related methodCHILA RONALD J·Filed 2008·Granted May 29, 2012·11 cites·13 claims
- 3465US8813501B2Combustor assemblies for use in turbine engines and methods of assembling sameCIHLAR DAVID WILLIAM·Filed 2011·Granted Aug 26, 2014·3 cites·20 claims
- 3563US9243506B2Methods and systems for cooling a transition nozzleMCMAHAN KEVIN WESTON·Filed 2012·Granted Jan 26, 2016·2 cites·11 claims
- 3662US8887508B2Impingement sleeve and methods for designing and forming impingement sleeveBROWN JEROME DAVID·Filed 2011·Granted Nov 18, 2014·3 cites·20 claims
- 3759US8966910B2Methods and systems for cooling a transition nozzleMCMAHAN KEVIN WESTON·Filed 2011·Granted Mar 3, 2015·1 cites·18 claims
- 3859US8359867B2Combustor having a flow sleeveGEN ELECTRIC·Filed 2010·Granted Jan 29, 2013·3 cites·14 claims
- 3953US8448416B2Combustor linerDAVIS JR LEWIS BERKLEY·Filed 2009·Granted May 28, 2013·3 cites·16 claims
- 4052US9822649B2Integrated combustor and stage 1 nozzle in a gas turbine and methodDAVIS JR LEWIS BERKLEY·Filed 2008·Granted Nov 21, 2017·3 cites·11 claims
- 4152US2013036742A1Combustor liner cooling systemGEN ELECTRIC·Filed 2012·Application pending·0 cites
- 4251US8695322B2Thermally decoupled can-annular transition pieceDAVIS JR LEWIS BERKLEY·Filed 2009·Granted Apr 15, 2014·3 cites·14 claims
- 4350US8904802B2Turbomachine combustor assembly including a vortex modification systemKODUKULLA SRIDHAR VENKAT·Filed 2011·Granted Dec 9, 2014·1 cites·17 claims
- 4448US11859818B2Systems and methods for variable microchannel combustor liner coolingGEN ELECTRIC·Filed 2019·Granted Jan 2, 2024·0 cites·16 claims
- 4547US2014338340A1System and method for tube level air flow conditioningGEN ELECTRIC·Filed 2013·Application pending·0 cites
- 4645US8307655B2System for cooling turbine combustor transition pieceCHILA RONALD JAMES·Filed 2010·Granted Nov 13, 2012·0 cites·24 claims
- 4745US2013236301A1Apparatus And System For Directing Hot GasCHEN WEI·Filed 2012·Application pending·0 cites
- 4844US2012324898A1Combustor assembly for use in a turbine engine and methods of assembling sameMCMAHAN KEVIN WESTON·Filed 2011·Application pending·0 cites
- 4944US2010257863A1Combined convection/effusion cooled one-piece can combustorGEN ELECTRIC·Filed 2009·Application pending·0 cites
- 5044US2013086915A1Film cooled combustion liner assemblyCIHLAR DAVID WILLIAM·Filed 2011·Application pending·0 cites
Showing the top 50 of 66 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →