Inventor · disambiguated record
Thomas G. Tillman
Also filed as: TILLMAN THOMAS G · TILLMAN THOMAS GREGORY
18 granted patents·4 pending applications·898 citations·filing 2000–2022
95Inventor score
Files withUNITED TECHNOLOGIES CORP15HAMILTON SUNDSTRAND CORP2CORDATOS HARALAMBOS1GIERAS JACEK F1HERRING NEAL R1
Top patents by PatentIndex Score
22 records- 0196US6939392B2System and method for thermal managementUNITED TECHNOLOGIES CORP·Filed 2003·Granted Sep 6, 2005·134 cites·57 claims
- 0296US6334753B1Streamlined bodies with counter-flow fluid injectionUNITED TECHNOLOGIES CORP·Filed 2000·Granted Jan 1, 2002·91 cites·5 claims
- 0396US6318070B1Variable area nozzle for gas turbine engines driven by shape memory alloy actuatorsUNITED TECHNOLOGIES CORP·Filed 2000·Granted Nov 20, 2001·447 cites·19 claims
- 0493US7569099B2Fuel deoxygenation system with non-metallic fuel plate assemblyUNITED TECHNOLOGIES CORP·Filed 2006·Granted Aug 4, 2009·46 cites·17 claims
- 0591US7393388B2Spiral wound fuel stabilization unit for fuel de-oxygenationUNITED TECHNOLOGIES CORP·Filed 2005·Granted Jul 1, 2008·28 cites·17 claims
- 0690US11964772B2Boundary layer ducted fan propulsion systemRAYTHEON TECH CORP·Filed 2022·Granted Apr 23, 2024·2 cites·20 claims
- 0789US7004047B2Variable area nozzle for gas turbine engines driven by shape memory alloy actuatorsUNITED TECHNOLOGIES CORP·Filed 2004·Granted Feb 28, 2006·50 cites·3 claims
- 0888US6735936B2Variable area nozzle for gas turbine engines driven by shape memory alloy actuatorsUNITED TECHNOLOGIES CORP·Filed 2001·Granted May 18, 2004·50 cites·7 claims
- 0983US8741029B2Fuel deoxygenation using surface-modified porous membranesCORDATOS HARALAMBOS·Filed 2011·Granted Jun 3, 2014·7 cites·20 claims
- 1083US7601203B2Hybrid vacuum system for fuel deoxygenationUNITED TECHNOLOGIES CORP·Filed 2006·Granted Oct 13, 2009·12 cites·12 claims
- 1180US7435283B2Modular fuel stabilization systemUNITED TECHNOLOGIES CORP·Filed 2005·Granted Oct 14, 2008·11 cites·20 claims
- 1273US9688395B2Boundary layer ingesting bladeSIKORSKY AIRCRAFT CORP·Filed 2013·Granted Jun 27, 2017·6 cites·16 claims
- 1370US9909530B2Non-axisymmetric fixed or variable fan nozzle for boundary layer ingestion propulsionUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 6, 2018·3 cites·8 claims
- 1469US11498660B2Embedded engines in hybrid blended wing bodyUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 15, 2022·2 cites·17 claims
- 1564US8147600B2Pressure-based dissolved gas removal systemHERRING NEAL R·Filed 2009·Granted Apr 3, 2012·4 cites·7 claims
- 1660US9789972B2Fuel and thermal management systemHAMILTON SUNDSTRAND CORP·Filed 2014·Granted Oct 17, 2017·3 cites·15 claims
- 1759US10415505B2Non-axisymmetric fan flow pathUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 17, 2019·2 cites·12 claims
- 1855US8465266B2Vacuum pressure systemsGIERAS JACEK F·Filed 2007·Granted Jun 18, 2013·0 cites·19 claims
- 1947US2005150223A1Shape memory alloy bundles and actuatorsUNITED TECHNOLOGIES CORP·Filed 2005·Application pending·0 cites
- 2045US2016122005A1Embedded engines in hybrid blended wing bodyUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2140US2015044052A1Geared Turbofan With Fan Blades Designed To Achieve Laminar FlowUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
- 2233US2016221664A1Boundary layer control assembly for an aircraft airfoil and method of controlling a boundary layerHAMILTON SUNDSTRAND CORP·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →