Inventor · name-matched record
MORTON JEFFREY T
4 granted patents·13 pending applications·0 citations·filing 2024–2025
51Inventor score
Files withRTX CORP17
This identity is grouped by exact name match (no disambiguated inventor record was available for these filings) — it may combine same-named inventors.
Top patents by PatentIndex Score
17 records- 0184US2026015949A1Turbine engine tip clearance control system with thrust bearingRTX CORP·Filed 2025·Application pending·0 cites
- 0274US2026035086A1Open rotor aircraft propulsion system with multi-gear system geartrainRTX CORP·Filed 2025·Application pending·0 cites
- 0361US12565328B2Differential driven open rotor with brakeRTX CORP·Filed 2024·Granted Mar 3, 2026·0 cites·20 claims
- 0460US12553392B2Gas turbine engine with thermal managementRTX CORP·Filed 2024·Granted Feb 17, 2026·0 cites·20 claims
- 0557US12584444B2Suction enabled post shutdown combustor cooling and core ventilationRTX CORP·Filed 2024·Granted Mar 24, 2026·0 cites·18 claims
- 0656US2026091873A1Open rotor propulsion system with exhaust mixer(s)RTX CORP·Filed 2024·Application pending·0 cites
- 0754US12595765B2Bifurcation integrated electrical system for hybrid aircraft propulsion systemRTX CORP·Filed 2024·Granted Apr 7, 2026·0 cites·16 claims
- 0854US2026035082A1Low spool electrical machine arrangements for hybrid-electric enginesRTX CORP·Filed 2024·Application pending·0 cites
- 0954US2026022668A1Gearbox arrangement for dual spool engine accessoriesRTX CORP·Filed 2024·Application pending·0 cites
- 1053US2026092556A1Open rotor propulsion system with forward exhaust outlet(s)RTX CORP·Filed 2024·Application pending·0 cites
- 1153US2026062117A1Adjusting pitch for airfoils of an aircraft propulsion systemRTX CORP·Filed 2024·Application pending·0 cites
- 1252US2026015968A1Open rotor with aerodynamically isolatable free turbineRTX CORP·Filed 2024·Application pending·0 cites
- 1351US2026078904A1Fuel nozzle thermal management systemRTX CORP·Filed 2024·Application pending·0 cites
- 1451US2026063072A1Suction enabled post shutdown combustor cooling and ventilationRTX CORP·Filed 2024·Application pending·0 cites
- 1551US2026063074A1Suction enabled post shutdown combustor cooling and core ventilationRTX CORP·Filed 2024·Application pending·0 cites
- 1650US2026022670A1Open rotor aircraft propulsion system with multi-gear system geartrainRTX CORP·Filed 2024·Application pending·0 cites
- 1743US2026091880A1Open rotor aircraft propulsion system with offset geartrainRTX CORP·Filed 2024·Application pending·0 cites
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Identity basis: exact name match across USPTO filings. How scoring works →