Inventor · disambiguated record
Jonathan Gilson
Also filed as: GILSON JONATHAN · GILSON JONATHAN D · GILSON JONATHAN DAVID
22 granted patents·6 pending applications·234 citations·filing 2008–2021
95Inventor score
Files withUNITED TECHNOLOGIES CORP14RAYTHEON TECH CORP5GILSON JONATHAN4HALL ANDRE M2GILSON JONATHAN D1
Top patents by PatentIndex Score
28 records- 0197US10655538B2Geared gas turbine engine with reduced fan noiseUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 19, 2020·15 cites·30 claims
- 0297US10301971B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 28, 2019·13 cites·30 claims
- 0397US10066548B2Acoustic liner with varied propertiesUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 4, 2018·34 cites·36 claims
- 0497US9932933B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2013·Granted Apr 3, 2018·33 cites·19 claims
- 0596US10184340B2Geared turbofan engine having a reduced number of fan blades and improved acousticsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 22, 2019·29 cites·13 claims
- 0696US9920653B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2012·Granted Mar 20, 2018·17 cites·20 claims
- 0793US12060834B2Hybrid electric idle and braking for an aircraftRTX CORP·Filed 2021·Granted Aug 13, 2024·3 cites·16 claims
- 0893US9745918B2Gas turbine engine with noise attenuating variable area fan nozzleUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 29, 2017·10 cites·18 claims
- 0991US8997497B2Gas turbine engine with variable area fan nozzleHALL ANDRE M·Filed 2010·Granted Apr 7, 2015·23 cites·16 claims
- 1089US11492967B2Particulate ingestion sensor for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2019·Granted Nov 8, 2022·3 cites·20 claims
- 1189US11118507B2Geared gas turbine engine with reduced fan noiseRAYTHEON TECH CORP·Filed 2020·Granted Sep 14, 2021·2 cites·30 claims
- 1288US8820088B2Variable area fan nozzle with acoustic system for a gas turbine engineGILSON JONATHAN·Filed 2010·Granted Sep 2, 2014·14 cites·20 claims
- 1388US8800261B2Gas turbine engine with noise attenuating variable area fan nozzleHALL ANDRE M·Filed 2010·Granted Aug 12, 2014·16 cites·5 claims
- 1486US11286811B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 29, 2022·2 cites·26 claims
- 1584US10371051B2Gas turbine engine noise reducing nose coneUNITED TECHNOLOGIES CORP·Filed 2014·Granted Aug 6, 2019·8 cites·7 claims
- 1680US11015550B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 25, 2021·2 cites·18 claims
- 1774US8973364B2Gas turbine engine with noise attenuating variable area fan nozzleGILSON JONATHAN·Filed 2008·Granted Mar 10, 2015·10 cites·13 claims
- 1872US11781447B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeRAYTHEON TECH CORP·Filed 2021·Granted Oct 10, 2023·0 cites·30 claims
- 1971US11512631B2Geared gas turbine engine with reduced fan noiseRAYTHEON TECH CORP·Filed 2021·Granted Nov 29, 2022·0 cites·30 claims
- 2069US11781505B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeRAYTHEON TECH CORP·Filed 2021·Granted Oct 10, 2023·0 cites·30 claims
- 2166US2020063603A1Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2254USRE48980EAcoustic liner with varied propertiesRAYTHEON TECH CORP·Filed 2014·Granted Mar 22, 2022·0 cites·64 claims
- 2352US10808648B2Variable area fan nozzle for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 20, 2020·0 cites·24 claims
- 2447US2015126335A1Height adjustable pull-up bar apparatusGILSON JONATHAN D·Filed 2013·Application pending·0 cites
- 2547US2014073491A1Weight training sledGILSON JONATHAN DAVID·Filed 2012·Application pending·0 cites
- 2641US2013219922A1Geared gas turbine engine with reduced fan noiseGILSON JONATHAN·Filed 2012·Application pending·0 cites
- 2741US2016108854A1Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 2839US2013283821A1Gas turbine engine and nacelle noise attenuation structureGILSON JONATHAN·Filed 2012·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →