Inventor · disambiguated record
Derrick Walter Simons
Also filed as: SIMONS DERRICK · SIMONS DERRICK W · SIMONS DERRICK WALTER
23 granted patents·12 pending applications·395 citations·filing 2003–2016
96Inventor score
Files withGEN ELECTRIC23ROMIG BRYAN WESLEY4SIMONS DERRICK WALTER2BERRY JONATHAN DWIGHT1FULLER JASON D1
Top patents by PatentIndex Score
35 records- 0197US7181916B2Method for operating a reduced center burner in multi-burner combustorGEN ELECTRIC·Filed 2006·Granted Feb 27, 2007·36 cites·20 claims
- 0292US8904797B2Sector nozzle mounting systemsBERRY JONATHAN DWIGHT·Filed 2011·Granted Dec 9, 2014·14 cites·20 claims
- 0392US7185494B2Reduced center burner in multi-burner combustor and method for operating the combustorGEN ELECTRIC·Filed 2004·Granted Mar 6, 2007·52 cites·18 claims
- 0491US9388985B2Premixing apparatus for gas turbine systemWU CHUNYANG·Filed 2011·Granted Jul 12, 2016·21 cites·6 claims
- 0590US7389643B2Inboard radial dump venturi for combustion chamber of a gas turbineGEN ELECTRIC·Filed 2005·Granted Jun 24, 2008·35 cites·20 claims
- 0690US7246002B2Method for controlling fuel splits to gas turbine combustorGEN ELECTRIC·Filed 2003·Granted Jul 17, 2007·44 cites·14 claims
- 0786US10480792B2Fuel staging in a gas turbine engineGEN ELECTRIC·Filed 2016·Granted Nov 19, 2019·5 cites·13 claims
- 0886US7320213B2System for identification of hot and cold chambers in a gas turbine combustorGEN ELECTRIC·Filed 2007·Granted Jan 22, 2008·23 cites·20 claims
- 0985US7593803B2Method for controlling fuel splits to gas turbine combustorGEN ELECTRIC·Filed 2007·Granted Sep 22, 2009·15 cites·20 claims
- 1083US9291098B2Turbomachine and staged combustion system of a turbomachineGEN ELECTRIC·Filed 2012·Granted Mar 22, 2016·8 cites·15 claims
- 1183US8474268B2Method of mitigating undesired gas turbine transient response using event based actionsFULLER JASON D·Filed 2007·Granted Jul 2, 2013·28 cites·20 claims
- 1283US7854121B2Independent pilot fuel control in secondary fuel nozzleGEN ELECTRIC·Filed 2005·Granted Dec 21, 2010·10 cites·5 claims
- 1382US7210297B2Method and apparatus for identification of hot and cold chambers in a gas turbine combustorGEN ELECTRIC·Filed 2004·Granted May 1, 2007·39 cites·19 claims
- 1481US8370044B2NOX compliant peak for gas turbineGEN ELECTRIC·Filed 2009·Granted Feb 5, 2013·19 cites·19 claims
- 1579US8959925B2Combustor recovery method and systemROMIG BRYAN WESLEY·Filed 2012·Granted Feb 24, 2015·4 cites·19 claims
- 1676US9140189B2Systems and methods for detecting fuel leaks in gas turbine enginesROMIG BRYAN WESLEY·Filed 2012·Granted Sep 22, 2015·6 cites·16 claims
- 1767US9297315B2Systems and methods for determining a target exhaust temperature for a gas turbineGEN ELECTRIC·Filed 2012·Granted Mar 29, 2016·3 cites·17 claims
- 1867US8997558B2Combustor probe for gas turbineROMIG BRYAN WESLEY·Filed 2011·Granted Apr 7, 2015·2 cites·20 claims
- 1962US7373772B2Turbine combustor transition piece having dilution holesGEN ELECTRIC·Filed 2004·Granted May 20, 2008·23 cites·12 claims
- 2056US2010058767A1Swirl angle of secondary fuel nozzle for turbomachine combustorGEN ELECTRIC·Filed 2008·Application pending·0 cites
- 2152US2015253011A1Annular premixed pilot in fuel nozzleGEN ELECTRIC·Filed 2015·Application pending·0 cites
- 2251US8707704B2Method and apparatus for assembling turbine enginesSIMONS DERRICK WALTER·Filed 2007·Granted Apr 29, 2014·5 cites·14 claims
- 2351US2013219899A1Annular premixed pilot in fuel nozzleUHM JONG HO·Filed 2012·Application pending·0 cites
- 2449US9279369B2Turbomachine with transition piece having dilution holes and fuel injection system coupled to transition pieceGEN ELECTRIC·Filed 2013·Granted Mar 8, 2016·0 cites·20 claims
- 2548US8371101B2Radial inlet guide vanes for a combustorGEN ELECTRIC·Filed 2009·Granted Feb 12, 2013·2 cites·20 claims
- 2648US2009211255A1Gas turbine combustor flame stabilizerGEN ELECTRIC·Filed 2008·Application pending·0 cites
- 2747US7887322B2Mixing 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
- 2843US2013014514A1Systems and methods for bulk temperature variation reduction of a gas turbine through can-to-can fuel temperature modulationROMIG BRYAN WESLEY·Filed 2011·Application pending·0 cites
- 2942US2011225973A1Combustor with Pre-Mixing Primary Fuel-Nozzle AssemblyGEN ELECTRIC·Filed 2010·Application pending·0 cites
- 3041US2010192587A1Combustor assembly for use in a gas turbine engine and method of assembling sameHESSLER WILLIAM KIRK·Filed 2009·Application pending·0 cites
- 3141US2011247340A1Apparatus and method for minimizing and/or eliminating dilution air leakage in a combustion liner assemblyPOPOVIC PREDRAG·Filed 2010·Application pending·0 cites
- 3240US2011162377A1Turbomachine nozzleGEN ELECTRIC·Filed 2010·Application pending·0 cites
- 3339US2009019854A1APPARATUS/METHOD FOR COOLING COMBUSTION CHAMBER/VENTURI IN A LOW NOx COMBUSTORGEN ELECTRIC·Filed 2007·Application pending·0 cites
- 3439US2009053054A1LEAKAGE REDUCING VENTURI FOR DRY LOW NITRIC OXIDES (NOx) COMBUSTORSGEN ELECTRIC·Filed 2007·Application pending·0 cites
- 3531US2010192580A1Combustion System Burner TubeSIMONS DERRICK WALTER·Filed 2009·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →