Inventor · disambiguated record
Dominic J. Mongillo
Also filed as: KULAK LEGAL REPRESENTATIVE EUG · MONGILLO DOMINIC · MONGILLO DOMINIC J · MONGILLO DOMINIC J JR
181 granted patents·21 pending applications·1,455 citations·filing 1997–2024
99Inventor score
Files withUNITED TECHNOLOGIES CORP138RAYTHEON TECH CORP31RTX CORP14MONGILLO JR DOMINIC J2PROPHETER-HINCKLEY TRACY A2
Top patents by PatentIndex Score
202 records- 0199US10107128B2Cooling channels for gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 23, 2018·29 cites·18 claims
- 0299US10036258B2Gas turbine engine component having vascular engineered lattice structureUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jul 31, 2018·30 cites·19 claims
- 0398US10801345B2Chevron trip stripUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 13, 2020·17 cites·20 claims
- 0498US9296039B2Gas turbine engine airfoil impingement coolingPROPHETER-HINCKLEY TRACY A·Filed 2012·Granted Mar 29, 2016·36 cites·2 claims
- 0598US5931638ATurbomachinery airfoil with optimized heat transferUNITED TECHNOLOGIES CORP·Filed 1997·Granted Aug 3, 1999·241 cites·17 claims
- 0697US11603769B2Forming lined cooling aperture(s) in a turbine engine componentRAYTHEON TECH CORP·Filed 2021·Granted Mar 14, 2023·6 cites·17 claims
- 0797US9976743B2Dilution hole assemblyUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 22, 2018·11 cites·19 claims
- 0896US8850828B2Cooling hole with curved metering sectionMONGILLO JR DOMINIC J·Filed 2012·Granted Oct 7, 2014·25 cites·18 claims
- 0995US11459897B2Cooling schemes for airfoils for gas turbine enginesRAYTHEON TECH CORP·Filed 2020·Granted Oct 4, 2022·4 cites·20 claims
- 1095US10774657B2Baffle assembly for gas turbine engine componentsUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 15, 2020·8 cites·20 claims
- 1195US10662781B2Gas turbine engine component having vascular engineered lattice structureUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 26, 2020·9 cites·22 claims
- 1295US9926799B2Gas turbine engine components, blade outer air seal assemblies, and blade outer air seal segments thereofUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 27, 2018·9 cites·18 claims
- 1395US9284845B2Turbine airfoil tip shelf and squealer pocket coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 15, 2016·19 cites·13 claims
- 1493US7837441B2Impingement skin core cooling for gas turbine engine bladeUNITED TECHNOLOGIES CORP·Filed 2007·Granted Nov 23, 2010·21 cites·16 claims
- 1593US6234754B1Coolable airfoil structureUNITED TECHNOLOGIES CORP·Filed 1999·Granted May 22, 2001·117 cites·9 claims
- 1692US7131818B2Airfoil with three-pass serpentine cooling channel and microcircuitUNITED TECHNOLOGIES CORP·Filed 2004·Granted Nov 7, 2006·66 cites·32 claims
- 1791US12203388B1Dual tip flagRTX CORP·Filed 2023·Granted Jan 21, 2025·1 cites·20 claims
- 1891US11898459B1Turbine blade cooling hole arrangementRAYTHEON TECH CORP·Filed 2022·Granted Feb 13, 2024·2 cites·20 claims
- 1991US11898465B2Forming lined cooling aperture(s) in a turbine engine componentRAYTHEON TECH CORP·Filed 2021·Granted Feb 13, 2024·2 cites·20 claims
- 2091US11781434B2Components for gas turbine enginesRTX CORP·Filed 2023·Granted Oct 10, 2023·2 cites·20 claims
- 2191US11137140B2Dilution holes with ridge feature for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2017·Granted Oct 5, 2021·6 cites·14 claims
- 2291US10408453B2Dilution holes for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 10, 2019·5 cites·14 claims
- 2391US10006295B2Gas turbine engine component having trip stripsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 26, 2018·12 cites·21 claims
- 2491US9995165B2Blade outer air seal having partial coatingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 12, 2018·6 cites·19 claims
- 2591US9851105B2Self-cooled orifice structureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 26, 2017·7 cites·20 claims
- 2691US7021893B2Fanned trailing edge teardrop arrayUNITED TECHNOLOGIES CORP·Filed 2004·Granted Apr 4, 2006·27 cites·13 claims
- 2790US8083485B2Angled tripped airfoil peanut cavityCHON YOUNG H·Filed 2007·Granted Dec 27, 2011·36 cites·21 claims
- 2890US7478994B2Airfoil with supplemental cooling channel adjacent leading edgeUNITED TECHNOLOGIES CORP·Filed 2004·Granted Jan 20, 2009·74 cites·31 claims
- 2989US11459898B2Airfoil cooling holesRAYTHEON TECH CORP·Filed 2021·Granted Oct 4, 2022·3 cites·20 claims
- 3089US10662780B2Double wall turbine gas turbine engine vane platform cooling configuration with baffle impingementUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 26, 2020·5 cites·15 claims
- 3188US10801325B2Turbine blade with tip vortex control and tip shelfUNITED TECHNOLOGIES CORP·Filed 2017·Granted Oct 13, 2020·5 cites·19 claims
- 3288US10669861B2Airfoil cooling structureUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 2, 2020·5 cites·19 claims
- 3388US10202864B2Chevron trip stripUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 12, 2019·5 cites·15 claims
- 3488US10018052B2Gas turbine engine component having engineered vascular structureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 10, 2018·4 cites·22 claims
- 3588US9222364B2Platform cooling circuit for a gas turbine engine componentPAPPLE MICHAEL LESLIE CLYDE·Filed 2012·Granted Dec 29, 2015·12 cites·8 claims
- 3687US10767490B2Hot section engine components having segment gap discharge holesUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 8, 2020·4 cites·19 claims
- 3787US10563521B2Aft flowing serpentine cavities and cores for airfoils of gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 18, 2020·4 cites·19 claims
- 3887US9429027B2Turbine airfoil tip shelf and squealer pocket coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 30, 2016·5 cites·16 claims
- 3986US11813706B2Methods for forming cooling apertures in a turbine engine componentRAYTHEON TECH CORP·Filed 2021·Granted Nov 14, 2023·1 cites·19 claims
- 4086US10731473B2Gas turbine engine component having engineered vascular structureUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 4, 2020·3 cites·22 claims
- 4186US10590779B2Double wall turbine gas turbine engine blade cooling configurationUNITED TECHNOLOGIES CORP·Filed 2017·Granted Mar 17, 2020·4 cites·17 claims
- 4286US10458264B2Seal arrangement for turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 29, 2019·4 cites·13 claims
- 4386US10101029B2Combustor panels and configurations for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 16, 2018·4 cites·19 claims
- 4486US9228442B2Turbine airfoil tip shelf and squealer pocket coolingMONGILLO JR DOMINIC J·Filed 2012·Granted Jan 5, 2016·10 cites·20 claims
- 4586US6179565B1Coolable airfoil structureUNITED TECHNOLOGIES CORP·Filed 1999·Granted Jan 30, 2001·88 cites·13 claims
- 4685US12460818B2Dilution holes with ridge feature for gas turbine enginesRTX CORP·Filed 2024·Granted Nov 4, 2025·0 cites·17 claims
- 4785US11434768B2Multi-walled airfoil coreRAYTHEON TECH CORP·Filed 2021·Granted Sep 6, 2022·1 cites·20 claims
- 4885US11396819B2Components for gas turbine enginesRAYTHEON TECH CORP·Filed 2020·Granted Jul 26, 2022·2 cites·20 claims
- 4985US10502075B2Platform cooling circuit for a gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 10, 2019·3 cites·17 claims
- 5085US10480329B2Airfoil turn caps in gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 19, 2019·4 cites·12 claims
Showing the top 50 of 202 patent records by PatentIndex Score.
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