Inventor · disambiguated record
Jeffrey T. Morton
Also filed as: MORTON JEFFREY · MORTON JEFFREY T
39 granted patents·13 pending applications·55 citations·filing 2015–2024
95Inventor score
Files withUNITED TECHNOLOGIES CORP25RTX CORP21RAYTHEON TECH CORP5Primetals Technologies Austria GmbH1
Top patents by PatentIndex Score
52 records- 0195US11346230B1Turbine blade cooling hole arrangementRAYTHEON TECH CORP·Filed 2020·Granted May 31, 2022·9 cites·20 claims
- 0295US10718521B2Combustor liner panel end rail cooling interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 21, 2020·10 cites·15 claims
- 0393US10473331B2Combustor panel endrail interfaceUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 12, 2019·8 cites·17 claims
- 0492US10370976B2Directional cooling arrangement for airfoilsUNITED TECHNOLOGIES CORP·Filed 2017·Granted Aug 6, 2019·7 cites·20 claims
- 0590US12203385B1Telescoping guide vane for aircraft propulsion systemRTX CORP·Filed 2024·Granted Jan 21, 2025·2 cites·17 claims
- 0690US12018587B1Turbine airfoil having cooling hole arrangementRTX CORP·Filed 2023·Granted Jun 25, 2024·2 cites·20 claims
- 0788US10801325B2Turbine blade with tip vortex control and tip shelfUNITED TECHNOLOGIES CORP·Filed 2017·Granted Oct 13, 2020·5 cites·19 claims
- 0885US12503241B2Thermal management assembly for an aircraft propulsion systemRTX CORP·Filed 2024·Granted Dec 23, 2025·1 cites·16 claims
- 0985US10279390B2Apparatus and method for production of long metal productsPrimetals Technologies Austria GmbH·Filed 2015·Granted May 7, 2019·2 cites·13 claims
- 1081US10344607B2Internally cooled engine componentsUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 9, 2019·3 cites·20 claims
- 1174US11143037B1Turbine blade cooling hole arrangementUNITED TECHNOLOGIES CORP·Filed 2020·Granted Oct 12, 2021·1 cites·20 claims
- 1274US10267520B2Float wall combustor panels having airflow distribution featuresUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 23, 2019·2 cites·16 claims
- 1373US12466544B1SRV open rotor with core inlet forward of rotorRTX CORP·Filed 2024·Granted Nov 11, 2025·0 cites·19 claims
- 1472US12421863B2Turbine engine tip clearance control system with thrust bearingRAYTHEON TECH CORP·Filed 2023·Granted Sep 23, 2025·0 cites·15 claims
- 1572US11098612B2Blade outer air seal including cooling trenchUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 24, 2021·1 cites·15 claims
- 1671US12497905B1Non-uniform and bi-tri stator spacing for swirl recovery vane (SRV) open rotor enginesRTX CORP·Filed 2024·Granted Dec 16, 2025·0 cites·18 claims
- 1771US12467384B1Translatable guide vanes for aircraft propulsion systemRTX CORP·Filed 2024·Granted Nov 11, 2025·0 cites·20 claims
- 1871US12352185B1Open rotor variable pitch blade with retracting inboard trailing edgeRTX CORP·Filed 2024·Granted Jul 8, 2025·0 cites·20 claims
- 1971US10551066B2Combustor liner panel and rail with diffused interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Feb 4, 2020·1 cites·23 claims
- 2068US10830434B2Combustor liner panel end rail with curved interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 10, 2020·1 cites·4 claims
- 2167US12448901B1Thermal management system for gas turbine engine with open propulsorRTX CORP·Filed 2024·Granted Oct 21, 2025·0 cites·20 claims
- 2265US12460577B2AFT gear based engine with heat recovery systemRTX CORP·Filed 2024·Granted Nov 4, 2025·0 cites·16 claims
- 2364US12352287B1Variable guide vane for aircraft propulsion systemRTX CORP·Filed 2024·Granted Jul 8, 2025·0 cites·19 claims
- 2463US12492711B1Open rotor with fixed guide vane/statorRTX CORP·Filed 2024·Granted Dec 9, 2025·0 cites·11 claims
- 2563US11156359B2Combustor liner panel end rail with diffused interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 26, 2021·0 cites·13 claims
- 2663US2025369825A1Actuatable inspection probe for non-destructive inspectionRTX CORP·Filed 2024·Application pending·0 cites
- 2762US2025236408A1Framed heat exchanger for aircraft propulsion systemRTX CORP·Filed 2024·Application pending·0 cites
- 2861US11255197B2Impingement cooling arrangement for airfoilsUNITED TECHNOLOGIES CORP·Filed 2020·Granted Feb 22, 2022·0 cites·21 claims
- 2961US10633978B2Directional cooling arrangement for airfoilsUNITED TECHNOLOGIES CORP·Filed 2019·Granted Apr 28, 2020·0 cites·20 claims
- 3059US2025214703A1Blended wing body aircraft systemRTX CORP·Filed 2024·Application pending·0 cites
- 3158US12397924B2Open rotor aircraft propulsion system with bypass flowpathRTX CORP·Filed 2024·Granted Aug 26, 2025·0 cites·19 claims
- 3258US11098591B1Turbine blade with contoured filletUNITED TECHNOLOGIES CORP·Filed 2020·Granted Aug 24, 2021·0 cites·12 claims
- 3355US12404812B1Open rotor aircraft propulsion system with bypass flowpathRTX CORP·Filed 2024·Granted Sep 2, 2025·0 cites·17 claims
- 3455US10570748B2Impingement cooling arrangement for airfoilsUNITED TECHNOLOGIES CORP·Filed 2018·Granted Feb 25, 2020·0 cites·22 claims
- 3553US11384654B2Mateface for blade outer air seals in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jul 12, 2022·0 cites·16 claims
- 3652US10677462B2Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 9, 2020·0 cites·15 claims
- 3752US2025326491A1Thermal management assembly for a hybrid-electric aircraft propulsion systemRTX CORP·Filed 2024·Application pending·0 cites
- 3851US12460819B2Continuous flow fuel systemRTX CORP·Filed 2024·Granted Nov 4, 2025·0 cites·13 claims
- 3951US11661852B2Turbine blade trailing edge cooling feedRAYTHEON TECH CORP·Filed 2020·Granted May 30, 2023·0 cites·21 claims
- 4051US10914178B2Airfoils having tapered tip flag cavity and cores for forming the sameUNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 9, 2021·0 cites·18 claims
- 4151US10823411B2Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 3, 2020·0 cites·12 claims
- 4249US2025154906A1Turbine engine accessory system with multiple gearboxesRTX CORP·Filed 2023·Application pending·0 cites
- 4349US2025297579A1Open pusher rotor with remote exhaustRTX CORP·Filed 2024·Application pending·0 cites
- 4448US2025197013A1Open rotor aircraft propulsion system with anti-icing systemRTX CORP·Filed 2023·Application pending·0 cites
- 4547US10815792B2Gas turbine engine component with a cooling circuit having a flared baseUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 27, 2020·0 cites·11 claims
- 4647US2024410284A1Turbine vane baffle chimneyRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 4747US2024426245A1Water actuated tip clearance control system for turbine engineRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 4842US10731477B2Woven skin cores for turbine airfoilsUNITED TECHNOLOGIES CORP·Filed 2017·Granted Aug 4, 2020·0 cites·20 claims
- 4941US2018306113A1Combustor liner panel end rail matching heat transfer featuresUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 5041US2018335212A1Redundant endrail for combustor panelUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
Showing the top 50 of 52 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →