Inventor · disambiguated record
Robert L. Gukeisen
Also filed as: GUKEISEN ROBERT · GUKEISEN ROBERT L
18 granted patents·6 pending applications·216 citations·filing 1997–2021
94Inventor score
Files withUNITED TECHNOLOGIES CORP13CLOFT THOMAS G4GUKEISEN ROBERT L2RAYTHEON TECH CORP2MARSHALL RICHARD M1
Top patents by PatentIndex Score
24 records- 0192US8104261B2Tri-body variable area fan nozzle and thrust reverserMARSHALL RICHARD M·Filed 2006·Granted Jan 31, 2012·37 cites·18 claims
- 0289US9540113B2De-couple geared turbo-fan engine and aircraftUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 10, 2017·14 cites·11 claims
- 0389US9297314B2Gas turbine engine with accessory gear boxUNITED TECHNOLOGIES CORP·Filed 2012·Granted Mar 29, 2016·10 cites·11 claims
- 0489US8869507B2Translatable cascade thrust reverserCLOFT THOMAS G·Filed 2010·Granted Oct 28, 2014·14 cites·19 claims
- 0585US9126691B2Access door for gas turbine engine componentsCLOFT THOMAS G·Filed 2007·Granted Sep 8, 2015·24 cites·18 claims
- 0683US6048171ABleed valve systemUNITED TECHNOLOGIES CORP·Filed 1997·Granted Apr 11, 2000·59 cites·11 claims
- 0778US7434405B2Bleed diffuser for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2005·Granted Oct 14, 2008·10 cites·12 claims
- 0874US10179653B2Pylon shape with geared turbofan for structural stiffnessUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jan 15, 2019·4 cites·17 claims
- 0972US7975465B2Hybrid engine accessory power systemUNITED TECHNOLOGIES CORP·Filed 2003·Granted Jul 12, 2011·29 cites·9 claims
- 1068US10221809B2Thrust reverser sliding door assemblyUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 5, 2019·4 cites·11 claims
- 1166US2021197976A1Pylon shape with geared turbofan for structural stiffnessRAYTHEON TECH CORP·Filed 2021·Application pending·0 cites
- 1256US11021257B2Pylon shape with geared turbofan for structural stiffnessRAYTHEON TECH CORP·Filed 2019·Granted Jun 1, 2021·0 cites·14 claims
- 1356US8800918B2Hybrid engine accessory power systemMORRIS TIMOTHY M·Filed 2009·Granted Aug 12, 2014·6 cites·21 claims
- 1455US10519898B2Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation systemUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 31, 2019·0 cites·8 claims
- 1555US8312728B2Generator with separate oil system for improved nacelle performanceCLOFT THOMAS G·Filed 2007·Granted Nov 20, 2012·4 cites·27 claims
- 1654US10184404B2Geared gas turbine engine accessory gearboxUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jan 22, 2019·1 cites·10 claims
- 1753US2016186598A1Gas Turbine Engine With Accessory Gear BoxUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
- 1847US10641181B2Gas turbine engine accessory gearboxUNITED TECHNOLOGIES CORP·Filed 2013·Granted May 5, 2020·0 cites·18 claims
- 1945US2014090386A1Geared turbofan with fan and core mounted accessory gearboxesCLOFT THOMAS G·Filed 2012·Application pending·0 cites
- 2044US2018327231A1Motorized transport systemSHAGBARK LLC·Filed 2017·Application pending·0 cites
- 2142US10145335B2Turbomachine thrust reverserUNITED TECHNOLOGIES CORP·Filed 2012·Granted Dec 4, 2018·0 cites·17 claims
- 2239US2016230702A1Extended thrust reverser cascadeUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2335US9194328B2Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation systemGUKEISEN ROBERT L·Filed 2006·Granted Nov 24, 2015·0 cites·16 claims
- 2432US2008258016A1Nacelle assembly without lower bi-fi splitterGUKEISEN ROBERT L·Filed 2007·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →