Inventor · disambiguated record
Juan Enrique Portillo Bilbao
Also filed as: PORTILLO BILBAO JUAN E · PORTILLO BILBAO JUAN ENRIQUE
11 granted patents·12 pending applications·20 citations·filing 2010–2018
84Inventor score
Files withSIEMENS ENERGY INC10SIEMENS AG7PORTILLO BILBAO JUAN ENRIQUE2PENT JARED M1PORTILLO BILBAO JUAN E1
Top patents by PatentIndex Score
23 records- 0186US10222066B2Ducting arrangement with injector assemblies arranged in an expanding cross-sectional area of a downstream combustion stage in a gas turbine engineSIEMENS ENERGY INC·Filed 2016·Granted Mar 5, 2019·6 cites·12 claims
- 0276US11248795B2Finely distributed combustion system for a gas turbine engineSIEMENS ENERGY GLOBAL GMBH & CO KG·Filed 2018·Granted Feb 15, 2022·2 cites·11 claims
- 0376US10139111B2Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine engineSIEMENS ENERGY INC·Filed 2014·Granted Nov 27, 2018·5 cites·2 claims
- 0474US10095218B2Method and computer-readable model for additively manufacturing ducting arrangement with injector assemblies forming a shielding flow of airSIEMENS AG·Filed 2016·Granted Oct 9, 2018·2 cites·17 claims
- 0560US10215038B2Method and computer-readable model for additively manufacturing ducting arrangement for a gas turbine engineSIEMENS ENERGY INC·Filed 2016·Granted Feb 26, 2019·1 cites·13 claims
- 0657US10309655B2Cooling system for fuel nozzles within combustor in a turbine engineSIEMENS ENERGY INC·Filed 2014·Granted Jun 4, 2019·1 cites·16 claims
- 0757US9366438B2Flow sleeve inlet assembly in a gas turbine engineRAJARAM RAJESH·Filed 2013·Granted Jun 14, 2016·2 cites·18 claims
- 0851US11029030B2Ducting arrangement with injector assemblies configured to form a shielding flow of air injected into a combustion stage in a gas turbine engineSIEMENS AG·Filed 2016·Granted Jun 8, 2021·0 cites·18 claims
- 0950US10775043B2Combustor and method for damping vibrational modes under high-frequency combustion dynamicsSIEMENS AG·Filed 2014·Granted Sep 15, 2020·0 cites·13 claims
- 1048US2017114717A1Axial stage combustion system with exhaust gas recirculationSIEMENS ENERGY INC·Filed 2014·Application pending·0 cites
- 1147US2017328568A1Fuel lance with means for interacting with a flow of air and improve breakage of an ejected liquid jet of fuelSIEMENS AG·Filed 2014·Application pending·0 cites
- 1245US9400108B2Acoustic damping system for a combustor of a gas turbine enginePORTILLO BILBAO JUAN ENRIQUE·Filed 2013·Granted Jul 26, 2016·1 cites·8 claims
- 1342US2017261964A1Method and computer-readable model for additively manufacturing ducting arrangement for a combustion system in a gas turbine engineSIEMENS ENERGY INC·Filed 2016·Application pending·0 cites
- 1442US2015167980A1Axial stage injection dual frequency resonator for a combustor of a gas turbine enginePENT JARED M·Filed 2013·Application pending·0 cites
- 1541US2017260866A1Ducting arrangement in a combustion system of a gas turbine engineSIEMENS ENERGY INC·Filed 2016·Application pending·0 cites
- 1640US2014123649A1Acoustic damping system for a combustor of a gas turbine enginePORTILLO BILBAO JUAN E·Filed 2012·Application pending·0 cites
- 1740US2017284676A1Method and computer-readable model for additively manufacturing injector assembly or ducting arrangement including such injector assembliesSIEMENS ENERGY INC·Filed 2016·Application pending·0 cites
- 1839US2019301738A1Combustion system with injector assemblies arranged to recapture cooling air from a transition duct to form a shielding flow of air in a combustion stageSIEMENS AG·Filed 2016·Application pending·0 cites
- 1938US10054313B2Air biasing system in a gas turbine combustorPORTILLO BILBAO JUAN ENRIQUE·Filed 2010·Granted Aug 21, 2018·0 cites·19 claims
- 2037US2018187563A1Gas turbine transition duct with late lean injection having reduced combustion residence timeSIEMENS AG·Filed 2015·Application pending·0 cites
- 2137US2017284675A1Injector assembly and ducting arrangement including such injector assemblies in a combustion system for a gas turbine engineSIEMENS ENERGY INC·Filed 2016·Application pending·0 cites
- 2236US2018313535A1Combustion system with injector assembly including aerodynamically-shaped body and/or ejection orificesSIEMENS ENERGY INC·Filed 2015·Application pending·0 cites
- 2336US2018230956A1Method and apparatus with arrangement of fuel ejection orifices configured for mitigating combustion dynamics in a combustion turbine engineSIEMENS AG·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →