Inventor · disambiguated record
Timothy A. Fox
Also filed as: FOX TIMOTHY · FOX TIMOTHY A
27 granted patents·15 pending applications·311 citations·filing 2008–2022
96Inventor score
Top patents by PatentIndex Score
42 records- 0198US9016066B2Combustor assembly in a gas turbine engineWIEBE DAVID J·Filed 2012·Granted Apr 28, 2015·29 cites·19 claims
- 0297US8375726B2Combustor assembly in a gas turbine engineSIEMENS ENERGY INC·Filed 2009·Granted Feb 19, 2013·53 cites·16 claims
- 0396US8752386B2Air/fuel supply system for use in a gas turbine engineFOX TIMOTHY A·Filed 2010·Granted Jun 17, 2014·64 cites·20 claims
- 0495US10704786B2Fuel injector including a lobed mixer and vanes for injecting alternate fuels in a gas turbineSIEMENS ENERGY INC·Filed 2015·Granted Jul 7, 2020·11 cites·14 claims
- 0592US8511087B2Fuel injector and swirler assembly with lobed mixerFOX TIMOTHY A·Filed 2011·Granted Aug 20, 2013·39 cites·20 claims
- 0689US8661779B2Flex-fuel injector for gas turbinesLASTER WALTER R·Filed 2009·Granted Mar 4, 2014·27 cites·20 claims
- 0785US8272218B2Spiral cooled fuel nozzleFOX TIMOTHY·Filed 2008·Granted Sep 25, 2012·32 cites·17 claims
- 0883US9395082B2Combustor resonator section with an internal thermal barrier coating and method of fabricating the sameSIEMENS ENERGY INC·Filed 2012·Granted Jul 19, 2016·9 cites·14 claims
- 0978US8769955B2Self-regulating fuel staging port for turbine combustorVAN NIEUWENHUIZEN WILLIAM F·Filed 2010·Granted Jul 8, 2014·11 cites·15 claims
- 1076US10139111B2Dual 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
- 1175US9163841B2Cast manifold for dry low NOx gas turbine engineSIEMENS ENERGY INC·Filed 2012·Granted Oct 20, 2015·5 cites·17 claims
- 1274US10095218B2Method 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
- 1372US8955328B2Burner arrangementBöttcher Andreas·Filed 2011·Granted Feb 17, 2015·2 cites·12 claims
- 1470US10443855B2Flexible fuel combustion system for turbine enginesSIEMENS AG·Filed 2014·Granted Oct 15, 2019·2 cites·14 claims
- 1570US10359194B2Film cooling hole arrangement for acoustic resonators in gas turbine enginesSIEMENS ENERGY INC·Filed 2014·Granted Jul 23, 2019·3 cites·16 claims
- 1667US8991192B2Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engineWIEBE DAVID J·Filed 2009·Granted Mar 31, 2015·9 cites·17 claims
- 1758US9562692B2Nozzle with multi-tube fuel passageway for gas turbine enginesSIEMENS AG·Filed 2014·Granted Feb 7, 2017·1 cites·19 claims
- 1858US8549859B2Combustor apparatus in a gas turbine engineFOX TIMOTHY A·Filed 2008·Granted Oct 8, 2013·6 cites·20 claims
- 1957US10309655B2Cooling system for fuel nozzles within combustor in a turbine engineSIEMENS ENERGY INC·Filed 2014·Granted Jun 4, 2019·1 cites·16 claims
- 2052US2014208757A1Air/Fuel Supply System for Use in a Gas Turbine EngineMIKRO SYSTEMS INC·Filed 2014·Application pending·0 cites
- 2151US11029030B2Ducting 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
- 2251US2017198913A1Fuel injection system for a turbine engineSIEMENS AG·Filed 2014·Application pending·0 cites
- 2343US9291102B2Interface ring for gas turbine fuel nozzle assembliesFOX TIMOTHY A·Filed 2011·Granted Mar 22, 2016·0 cites·19 claims
- 2443US2010071377A1Combustor Apparatus for Use in a Gas Turbine EngineFOX TIMOTHY A·Filed 2009·Application pending·0 cites
- 2542US9488105B2Gas turbine assembly and method thereforBöttcher Andreas·Filed 2011·Granted Nov 8, 2016·0 cites·17 claims
- 2642US2012260666A1Multi-fuel combustion systemBARVE VINAYAK V·Filed 2010·Application pending·0 cites
- 2742US2017314405A1Transition duct exit frame with insertSIEMENS AG·Filed 2014·Application pending·0 cites
- 2841US9151171B2Stepped inlet ring for a transition downstream from combustor basket in a combustion turbine engineSUTCU MUZAFFER·Filed 2010·Granted Oct 6, 2015·0 cites·18 claims
- 2941US2024151150A1Transition with uneven surfaceSIEMENS ENERGY GLOBAL GMBH & CO KG·Filed 2022·Application pending·0 cites
- 3040US9746185B2Circumferential biasing and profiling of fuel injection in distribution ringRITLAND DAVID M·Filed 2010·Granted Aug 29, 2017·0 cites·20 claims
- 3139US11149949B2Converging duct with elongated and hexagonal cooling featuresSIEMENS AG·Filed 2016·Granted Oct 19, 2021·0 cites·16 claims
- 3239US11092338B2Method for constructing impingement/effusion cooling features in a component of a combustion turbine engineSIEMENS AG·Filed 2018·Granted Aug 17, 2021·0 cites·13 claims
- 3339US2019301738A1Combustion 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
- 3439US2011091829A1Multi-fuel combustion systemBARVE VINAYAK·Filed 2009·Application pending·0 cites
- 3539US2013327045A1Gas turbine combustion chamber with fuel nozzle, burner with such a fuel nozzle and fuel nozzleFOX TIMOTHY A·Filed 2011·Application pending·0 cites
- 3638US9157370B2Burner assemblyBöttcher Andreas·Filed 2010·Granted Oct 13, 2015·0 cites·16 claims
- 3738US2018258778A1Non-axially symmetric transition ducts for combustorsSIEMENS AG·Filed 2015·Application pending·0 cites
- 3838US2012137691A1Gas turbine assembly and method thereforBOTTCHER ANDREAS·Filed 2010·Application pending·0 cites
- 3937US2018187563A1Gas turbine transition duct with late lean injection having reduced combustion residence timeSIEMENS AG·Filed 2015·Application pending·0 cites
- 4037US2013104554A1Burner assemblyBODE SIEGFRIED·Filed 2011·Application pending·0 cites
- 4135US2018163550A1Transition ducts of a gas turbine combustorSIEMENS AG·Filed 2015·Application pending·0 cites
- 4234US2018179905A1Component having impingement cooled pockets formed by raised ribs and a cover sheet diffusion bonded to the raised ribsSIEMENS AG·Filed 2015·Application pending·0 cites
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