Inventor · disambiguated record
Robert E. Malecki
Also filed as: MALECKI ROBERT E
27 granted patents·5 pending applications·92 citations·filing 2010–2022
95Inventor score
Files withUNITED TECHNOLOGIES CORP23RAYTHEON TECH CORP6MALECKI ROBERT E1MURPHY MICHAEL JOSEPH1SIDELKOVSKIY DMITRIY B1
Top patents by PatentIndex Score
32 records- 0197US10301971B2Low 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
- 0297US9932933B2Low 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
- 0396US9920653B2Low 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
- 0487US11236701B2Convergent divergent exit nozzle for a gas turbine engineRAYTHEON TECH CORP·Filed 2018·Granted Feb 1, 2022·3 cites·8 claims
- 0586US11286811B2Low 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
- 0684US10724541B2Nacelle short inletUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jul 28, 2020·5 cites·17 claims
- 0782US10371092B2Convergent divergent exit nozzle for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·3 cites·13 claims
- 0880US11015550B2Low 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
- 0977US9057286B2Non-circular aft nacelle cowling geometryMURPHY MICHAEL JOSEPH·Filed 2010·Granted Jun 16, 2015·5 cites·13 claims
- 1073US10054059B2Nacelle and compressor inlet arrangementsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 21, 2018·2 cites·10 claims
- 1172US11781447B2Low 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
- 1269US11781505B2Low 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
- 1367US11970974B2Gas turbine engine mounted above wing and with camberRAYTHEON TECH CORP·Filed 2022·Granted Apr 30, 2024·0 cites·12 claims
- 1467US11391216B2Elongated geared turbofan with high bypass ratioRAYTHEON TECH CORP·Filed 2019·Granted Jul 19, 2022·0 cites·16 claims
- 1566US2020063603A1Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 1665US12441475B2Gas turbine engine mounted above wing and with camberRAYTHEON TECH CORP·Filed 2020·Granted Oct 14, 2025·0 cites·19 claims
- 1764US10330047B2Asymmetric fan nozzle in high-BPR separate-flow nacelleUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jun 25, 2019·2 cites·9 claims
- 1862US10479519B2Nacelle short inlet for fan blade removalUNITED TECHNOLOGIES CORP·Filed 2016·Granted Nov 19, 2019·1 cites·19 claims
- 1962US10295420B2Nacelle deflection measurement assemblyUNITED TECHNOLOGIES CORP·Filed 2016·Granted May 21, 2019·1 cites·11 claims
- 2062US9249731B2Nacelle bifurcation for gas turbine engineSIDELKOVSKIY DMITRIY B·Filed 2012·Granted Feb 2, 2016·3 cites·18 claims
- 2157US10294871B2Exhaust nozzle arrangement for geared turbofanUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 21, 2019·0 cites·19 claims
- 2255US10316757B2Exhaust nozzle arrangement for geared turbofanUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 11, 2019·0 cites·20 claims
- 2354US10436120B2Exhaust nozzle for an elongated gear turbofan with high bypass ratioUNITED TECHNOLOGIES CORP·Filed 2013·Granted Oct 8, 2019·0 cites·36 claims
- 2453US10436121B2Elongated geared turbofan with high bypass ratioUNITED TECHNOLOGIES CORP·Filed 2013·Granted Oct 8, 2019·0 cites·30 claims
- 2552US9995180B2Non-circular aft nacelle cowling geometryUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 12, 2018·0 cites·13 claims
- 2647US10450898B2Track fairing assembly for a turbine engine nacelleUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 22, 2019·0 cites·16 claims
- 2747US2016003091A1Nacelle internal and external flow controlUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2846US2016215732A1Bypass duct heat exchanger placementUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2942US10145335B2Turbomachine thrust reverserUNITED TECHNOLOGIES CORP·Filed 2012·Granted Dec 4, 2018·0 cites·17 claims
- 3042US2014216005A1Gas Turbine Engine Assembly Including A Thrust ReverserUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 3141US10006404B2Gas turbine engine thrust reverser systemMALECKI ROBERT E·Filed 2012·Granted Jun 26, 2018·0 cites·20 claims
- 3241US2016108854A1Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →