Inventor · disambiguated record
Predrag Popovic
Also filed as: POPOVIC PREDRAG · POPOVIC PREDRAG PEJA
17 granted patents·19 pending applications·161 citations·filing 2006–2017
93Inventor score
Top patents by PatentIndex Score
36 records- 0196US8205455B2Power plant and method of operationPOPOVIC PREDRAG·Filed 2011·Granted Jun 26, 2012·84 cites·6 claims
- 0291US9377202B2System and method for fuel blending and control in gas turbinesGEN ELECTRIC·Filed 2013·Granted Jun 28, 2016·12 cites·20 claims
- 0384US9010082B2Turbine engine and method for flowing air in a turbine engineSTOIA LUCAS JOHN·Filed 2012·Granted Apr 21, 2015·8 cites·17 claims
- 0484US8955329B2Diffusion nozzles for low-oxygen fuel nozzle assembly and methodPOPOVIC PREDRAG·Filed 2011·Granted Feb 17, 2015·8 cites·18 claims
- 0578US8522554B2Fuel nozzle for a turbine engine with a passive purge air passagewayINTILE JOHN·Filed 2010·Granted Sep 3, 2013·5 cites·11 claims
- 0678US8028529B2Low emissions gas turbine combustorGEN ELECTRIC·Filed 2008·Granted Oct 4, 2011·16 cites·18 claims
- 0770US8365534B2Gas turbine combustor having a fuel nozzle for flame anchoringGEN ELECTRIC·Filed 2011·Granted Feb 5, 2013·4 cites·18 claims
- 0867US9382850B2System and method for controlled fuel blending in gas turbinesGEN ELECTRIC·Filed 2013·Granted Jul 5, 2016·3 cites·21 claims
- 0967US9347376B2Liquified fuel backup fuel supply for a gas turbineGEN ELECTRIC·Filed 2013·Granted May 24, 2016·3 cites·18 claims
- 1067US9297315B2Systems and methods for determining a target exhaust temperature for a gas turbineGEN ELECTRIC·Filed 2012·Granted Mar 29, 2016·3 cites·17 claims
- 1157US8020385B2Centerbody cap for a turbomachine combustor and methodGEN ELECTRIC·Filed 2008·Granted Sep 20, 2011·5 cites·10 claims
- 1253US2017184310A1System for Injecting a Liquid Fuel into a Combustion Gas Flow FieldGEN ELECTRIC·Filed 2017·Application pending·0 cites
- 1352US2016068777A1Gas turbine fuel blending using inferred fuel compositionsGEN ELECTRIC·Filed 2014·Application pending·0 cites
- 1450US8397512B2Flow device for turbine engine and method of assembling sameHESSLER WILLIAM KIRK·Filed 2008·Granted Mar 19, 2013·4 cites·20 claims
- 1550US2015047360A1System for injecting a liquid fuel into a combustion gas flow fieldGEN ELECTRIC·Filed 2013·Application pending·0 cites
- 1647US7887322B2Mixing hole arrangement and method for improving homogeneity of an air and fuel mixture in a combustorGEN ELECTRIC·Filed 2006·Granted Feb 15, 2011·1 cites·26 claims
- 1745US8096133B2Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interfaceHESSLER WILLIAM K·Filed 2008·Granted Jan 17, 2012·4 cites·18 claims
- 1843US9181876B2Method and apparatus for operating a gas turbine enginePOPOVIC PREDRAG·Filed 2012·Granted Nov 10, 2015·0 cites·19 claims
- 1943US8156743B2Method and arrangement for expanding a primary and secondary flame in a combustorHESSLER WILLIAM KIRK·Filed 2006·Granted Apr 17, 2012·1 cites·13 claims
- 2043US2014260302A1DIFFUSION COMBUSTOR FUEL NOZZLE FOR LIMITING NOx EMISSIONSGEN ELECTRIC·Filed 2013·Application pending·0 cites
- 2143US2012204571A1Combustor and method for introducing a secondary fluid into a fuel nozzleKRAEMER GILBERT OTTO·Filed 2011·Application pending·0 cites
- 2242US2013276450A1Combustor apparatus for stoichiometric combustionBARUAH ABINASH·Filed 2012·Application pending·0 cites
- 2341US2009260340A1Combustor of a Turbine, a Method of Retro-Fitting a Combustor of a Turbine and a Method of Building a Combustor of a TurbineGEN ELECTRIC·Filed 2008·Application pending·0 cites
- 2441US2011247340A1Apparatus and method for minimizing and/or eliminating dilution air leakage in a combustion liner assemblyPOPOVIC PREDRAG·Filed 2010·Application pending·0 cites
- 2540US2010205970A1Systems, Methods, and Apparatus Providing a Secondary Fuel Nozzle AssemblyGEN ELECTRIC·Filed 2009·Application pending·0 cites
- 2640US2013263605A1Diffusion Combustor Fuel NozzleBARUAH ABINASH·Filed 2012·Application pending·0 cites
- 2740US2012102967A1Method and system for preventing combustion instabilities during transient operationsKIRZHNER JOSEPH·Filed 2010·Application pending·0 cites
- 2840US2012036863A1Method, apparatus and system for delivery of wide range of turbine fuels for combustionKIRZHNER JOSEPH·Filed 2010·Application pending·0 cites
- 2939US2010018211A1Gas turbine transition piece having dilution holesGEN ELECTRIC·Filed 2008·Application pending·0 cites
- 3038US9500369B2Fuel nozzle and method for operating a combustorPOPOVIC PREDRAG·Filed 2012·Granted Nov 22, 2016·0 cites·20 claims
- 3138US2013074504A1System for injecting fuel in a gas turbine engineBARUAH ABINASH·Filed 2011·Application pending·0 cites
- 3237US2011041507A1Integral Liner and Venturi for Eliminating Air LeakageHESSLER WILLIAM KIRK·Filed 2009·Application pending·0 cites
- 3336US2012210717A1Apparatus for injecting fluid into a combustion chamber of a combustorBARUAH ABINASH·Filed 2011·Application pending·0 cites
- 3436US2015135723A1Combustor nozzle and method of supplying fuel to a combustorBELYAEV VLADIMIR VASILYEVICH·Filed 2012·Application pending·0 cites
- 3535US2012102914A1Systems, methods, and apparatus for compensating fuel composition variations in a gas turbineKIRZHNER JOSEPH·Filed 2010·Application pending·0 cites
- 3635US2013025253A1Reduction of co and o2 emissions in oxyfuel hydrocarbon combustion systems using oh radical formation with hydrogen fuel staging and diluent additionAKULA RAJANI KUMAR·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →