Inventor · disambiguated record
Carey Clum
Also filed as: CLUM CAREY · CLUM CAREY J
68 granted patents·10 pending applications·117 citations·filing 2015–2025
98Inventor score
Top patents by PatentIndex Score
78 records- 0198US10801345B2Chevron trip stripUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 13, 2020·17 cites·20 claims
- 0297US10077664B2Gas turbine engine component having engineered vascular structureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 18, 2018·14 cites·21 claims
- 0396US9845731B2Self-modulated cooling on turbine componentsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 19, 2017·11 cites·20 claims
- 0496US9752447B2Angled rail holesUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 5, 2017·15 cites·16 claims
- 0590US10731855B2Combustor panel cooling arrangementsUNITED TECHNOLOGIES CORP·Filed 2017·Granted Aug 4, 2020·5 cites·17 claims
- 0688US10202864B2Chevron trip stripUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 12, 2019·5 cites·15 claims
- 0787US10767490B2Hot section engine components having segment gap discharge holesUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 8, 2020·4 cites·19 claims
- 0887US10563521B2Aft flowing serpentine cavities and cores for airfoils of gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 18, 2020·4 cites·19 claims
- 0986US10590779B2Double wall turbine gas turbine engine blade cooling configurationUNITED TECHNOLOGIES CORP·Filed 2017·Granted Mar 17, 2020·4 cites·17 claims
- 1086US10233842B2Tangential on-board injectors for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2016·Granted Mar 19, 2019·4 cites·18 claims
- 1185US10626734B2Airfoil having internal hybrid cooling cavitiesUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 21, 2020·1 cites·16 claims
- 1285US10480333B2Turbine blade including balanced mateface conditionUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 19, 2019·4 cites·16 claims
- 1384US11371703B2Apparatus and method for mitigating particulate accumulation on a component of a gas turbineUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jun 28, 2022·3 cites·17 claims
- 1480US10465529B2Leading edge hybrid cavities and cores for airfoils of gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Nov 5, 2019·2 cites·9 claims
- 1579US10519782B2Airfoil having serpentine core resupply flow controlUNITED TECHNOLOGIES CORP·Filed 2017·Granted Dec 31, 2019·3 cites·19 claims
- 1679US10422229B2Airfoil coolingUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 24, 2019·2 cites·17 claims
- 1779US10196902B2Cooling for gas turbine engine componentsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 5, 2019·3 cites·14 claims
- 1878US11098653B2Apparatus and method for mitigating particulate accumulation on a component of a gas turbineUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 24, 2021·2 cites·10 claims
- 1978US11092339B2Apparatus and method for mitigating particulate accumulation on a component of a gas turbineUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 17, 2021·2 cites·16 claims
- 2074US10830049B2Leading edge hybrid cavities and cores for airfoils of gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 10, 2020·2 cites·14 claims
- 2174US2024247613A1Apparatus and method for mitigating airflow separation around engine combustorRTX CORP·Filed 2024·Application pending·0 cites
- 2273US11988145B2Apparatus and method for mitigating airflow separation around engine combustorRTX CORP·Filed 2019·Granted May 21, 2024·1 cites·13 claims
- 2371US10626735B2Double wall turbine gas turbine engine blade cooling configurationUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 21, 2020·1 cites·18 claims
- 2471US10526898B2Airfoil cooling circuitUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jan 7, 2020·1 cites·17 claims
- 2570US2022316705A1Apparatus and method for mitigating particulate accumulation on a component of a gas turbineRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 2669US11143401B2Apparatus and method for mitigating particulate accumulation on a component of a gas turbineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 12, 2021·1 cites·11 claims
- 2769US2022381434A1Apparatus and method for mitigating particulate accumulation on a component of a gas turbineRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 2869US2025389193A1Variable thickness coating controlRTX CORP·Filed 2025·Application pending·0 cites
- 2968US11719439B2Panel burn through tolerant shell designRAYTHEON TECH CORP·Filed 2021·Granted Aug 8, 2023·0 cites·6 claims
- 3068US11187413B2Dirt collector systemUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 30, 2021·1 cites·10 claims
- 3168US10767509B2Trip strip and film cooling hole for gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 8, 2020·1 cites·20 claims
- 3267US10808548B2Double wall turbine gas turbine engine blade cooling configurationRAYTHEON TECH CORP·Filed 2017·Granted Oct 20, 2020·1 cites·17 claims
- 3367US10641105B2Airfoil having forward flowing serpentine flowUNITED TECHNOLOGIES CORP·Filed 2017·Granted May 5, 2020·1 cites·16 claims
- 3465US10989056B2Integrated squealer pocket tip and tip shelf with hybrid and tip flag coreUNITED TECHNOLOGIES CORP·Filed 2016·Granted Apr 27, 2021·1 cites·12 claims
- 3564US11492912B2Trailing edge pressure and flow regulatorRAYTHEON TECH CORP·Filed 2020·Granted Nov 8, 2022·0 cites·15 claims
- 3664US9957810B2Film hole with protruding flow accumulatorUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 1, 2018·1 cites·16 claims
- 3763US11649731B2Airfoil having internal hybrid cooling cavitiesRAYTHEON TECH CORP·Filed 2020·Granted May 16, 2023·0 cites·9 claims
- 3862US11725521B2Leading edge hybrid cavities for airfoils of gas turbine engineRAYTHEON TECH CORP·Filed 2019·Granted Aug 15, 2023·0 cites·16 claims
- 3962US10968753B1Airfoil having impingement leading edgeUNITED TECHNOLOGIES CORP·Filed 2019·Granted Apr 6, 2021·0 cites·20 claims
- 4061US11359810B2Apparatus and method for mitigating particulate accumulation on a component of a gas turbineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jun 14, 2022·0 cites·14 claims
- 4161US11098899B2Panel burn through tolerant shell designUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 24, 2021·0 cites·15 claims
- 4260US11415319B2Apparatus and method for mitigating particulate accumulation on a component of a gas turbineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 16, 2022·0 cites·10 claims
- 4357US10822959B2Blade tip coolingUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 3, 2020·0 cites·2 claims
- 4457US10584593B2Airfoil having impingement leading edgeUNITED TECHNOLOGIES CORP·Filed 2017·Granted Mar 10, 2020·0 cites·20 claims
- 4556US11319839B2Component having a dirt tolerant passage turnUNITED TECHNOLOGIES CORP·Filed 2019·Granted May 3, 2022·0 cites·17 claims
- 4656US10612390B2Trailing edge pressure and flow regulatorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 7, 2020·0 cites·20 claims
- 4755US10563512B2Gas turbine engine airfoilUNITED TECHNOLOGIES CORP·Filed 2017·Granted Feb 18, 2020·0 cites·18 claims
- 4854US11015454B2Coriolis optimized U-channel with root flagUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 25, 2021·0 cites·20 claims
- 4953US11274559B2Turbine blade tip dirt removal featureUNITED TECHNOLOGIES CORP·Filed 2020·Granted Mar 15, 2022·0 cites·13 claims
- 5052US10890074B2Coriolis optimized u-channel with platform coreUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jan 12, 2021·0 cites·21 claims
Showing the top 50 of 78 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →