Inventor · disambiguated record
Nicholas M. Loricco
Also filed as: LORICCO NICHOLAS · LORICCO NICHOLAS M
38 granted patents·5 pending applications·66 citations·filing 2013–2024
95Inventor score
Top patents by PatentIndex Score
43 records- 0195US11346230B1Turbine blade cooling hole arrangementRAYTHEON TECH CORP·Filed 2020·Granted May 31, 2022·9 cites·20 claims
- 0295US9714580B2Trough seal for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jul 25, 2017·24 cites·18 claims
- 0389US10662780B2Double wall turbine gas turbine engine vane platform cooling configuration with baffle impingementUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 26, 2020·5 cites·15 claims
- 0487US11506129B2Feather seal mateface cooling pocketsRAYTHEON TECH CORP·Filed 2020·Granted Nov 22, 2022·2 cites·13 claims
- 0581US9718708B2Acoustophoretic enhanced system for use in tanksFLODESIGN SONICS INC·Filed 2013·Granted Aug 1, 2017·4 cites·27 claims
- 0679US10196902B2Cooling for gas turbine engine componentsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 5, 2019·3 cites·14 claims
- 0778US10557375B2Segregated cooling air passages for turbine vaneUNITED TECHNOLOGIES CORP·Filed 2018·Granted Feb 11, 2020·2 cites·12 claims
- 0878US10273820B2Turbine vane cooling arrangementUNITED TECHNOLOGIES CORP·Filed 2016·Granted Apr 30, 2019·2 cites·10 claims
- 0978US10259039B2Gas turbine engine component cooling passage and space casting coreUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 16, 2019·1 cites·5 claims
- 1076US10704396B2Dual-wall impingement cavity for components of gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jul 7, 2020·2 cites·8 claims
- 1175US10648363B2Turbine vane cooling arrangementUNITED TECHNOLOGIES CORP·Filed 2017·Granted May 12, 2020·2 cites·11 claims
- 1274US11143037B1Turbine blade cooling hole arrangementUNITED TECHNOLOGIES CORP·Filed 2020·Granted Oct 12, 2021·1 cites·20 claims
- 1374US10533425B2Doublet vane assembly for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jan 14, 2020·2 cites·16 claims
- 1470US10724381B2Cooling passage with structural rib and film cooling slotUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jul 28, 2020·1 cites·20 claims
- 1567US10697307B2Hybrid cooling schemes for airfoils of gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jun 30, 2020·1 cites·20 claims
- 1667US10006371B2Film hole with in-wall accumulatorUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 26, 2018·1 cites·19 claims
- 1765US10954815B2Divided baffle for components of gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 23, 2021·0 cites·20 claims
- 1864US10364683B2Gas turbine engine component cooling passage turbulatorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jul 30, 2019·2 cites·11 claims
- 1964US9957810B2Film hole with protruding flow accumulatorUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 1, 2018·1 cites·16 claims
- 2061US11814979B1Systems and methods of hybrid blade tip repairRAYTHEON TECH CORP·Filed 2022·Granted Nov 14, 2023·0 cites·14 claims
- 2161US10954800B2Fluidic machining method and systemUNITED TECHNOLOGIES CORP·Filed 2018·Granted Mar 23, 2021·0 cites·12 claims
- 2261US10465530B2Gas turbine engine component cooling cavity with vortex promoting featuresUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 5, 2019·1 cites·9 claims
- 2361US10166601B2Die cast tip cover and method of managing radial deflection of die cast tipUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jan 1, 2019·0 cites·19 claims
- 2461US2020011187A1Gas turbine engine component cooling cavity with vortex promoting featuresUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2560US10480347B2Divided baffle for components of gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 19, 2019·0 cites·20 claims
- 2660US2025345872A1Method of diffusion braze repair of cooling holes and cracksRTX CORP·Filed 2024·Application pending·0 cites
- 2759US2019176228A1Gas turbine engine component cooling passage and space eating coreUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2858US2023241699A1Edm electrode with enriched surface regionRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 2954US11243158B2Determining presence of internal corrosion within a rotor blade by measuring magnetic characteristic(s)UNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 8, 2022·0 cites·19 claims
- 3052US10107110B2Fluidic machining method and systemUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 23, 2018·0 cites·12 claims
- 3151US11661852B2Turbine blade trailing edge cooling feedRAYTHEON TECH CORP·Filed 2020·Granted May 30, 2023·0 cites·21 claims
- 3251US10914178B2Airfoils having tapered tip flag cavity and cores for forming the sameUNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 9, 2021·0 cites·18 claims
- 3351US10801344B2Double wall turbine gas turbine engine vane with discrete opposing skin core cooling configurationUNITED TECHNOLOGIES CORP·Filed 2017·Granted Oct 13, 2020·0 cites·18 claims
- 3450US10415394B2Gas turbine engine blade with ceramic tip and cooling arrangementUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 17, 2019·0 cites·16 claims
- 3549US2024263557A1Systems and methods of blade tip repair and manufacturing using field assisted sinteringRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 3647US11261739B2Airfoil with rib communicationUNITED TECHNOLOGIES CORP·Filed 2018·Granted Mar 1, 2022·0 cites·18 claims
- 3747US10746026B2Gas turbine engine airfoil with cooling pathUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 18, 2020·0 cites·13 claims
- 3846US12472590B2Systems and methods of blade leading edge repair using field assisted sintering technologyRAYTHEON TECH CORP·Filed 2022·Granted Nov 18, 2025·0 cites·12 claims
- 3946US10443401B2Cooled turbine vane with alternately orientated film cooling hole rowsUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 15, 2019·0 cites·20 claims
- 4045US10982552B2Gas turbine engine component with film cooling holeUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 20, 2021·0 cites·20 claims
- 4144US10648343B2Double wall turbine gas turbine engine vane platform cooling configuration with main core resupplyUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 12, 2020·0 cites·12 claims
- 4244US9957814B2Gas turbine engine component with film cooling hole with accumulatorUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 1, 2018·0 cites·15 claims
- 4340US11248481B2Turbine vane having dual source coolingRAYTHEON TECH CORP·Filed 2020·Granted Feb 15, 2022·0 cites·19 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →