Inventor · name-matched record
CLARK THOMAS E
13 granted patents·7 pending applications·0 citations·filing 2024–2025
80Inventor score
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
20 records- 0168US12540578B2Hybrid electric gas turbine engine two speed transmission for low spool drive power injection and power extractionRTX CORP·Filed 2024·Granted Feb 3, 2026·0 cites·13 claims
- 0264US12570405B1Aircraft with electrically powered engine accessoriesRTX CORP·Filed 2024·Granted Mar 10, 2026·0 cites·20 claims
- 0363US12577910B1Gas turbine engine with compartment anti-icing systemRTX CORP·Filed 2025·Granted Mar 17, 2026·0 cites·15 claims
- 0463US12559246B1Reducing eddy current propagation in electric device housingRTX CORP·Filed 2024·Granted Feb 24, 2026·0 cites·19 claims
- 0562US12560119B1Working fluid system for aircraft powerplantRTX CORP·Filed 2025·Granted Feb 24, 2026·0 cites·15 claims
- 0661US12523161B1Aircraft powerplant gearbox with selectable power couplerRTX CORP·Filed 2024·Granted Jan 13, 2026·0 cites·17 claims
- 0760US12552540B1Aircraft air system with electric boost compressorRTX CORP·Filed 2025·Granted Feb 17, 2026·0 cites·18 claims
- 0859US12553609B2Intercooled combustor nozzle guide vane and secondary air configurationRTX CORP·Filed 2024·Granted Feb 17, 2026·0 cites·18 claims
- 0959US12523177B1Electronic controller cooling for aircraft propulsion systemRTX CORP·Filed 2025·Granted Jan 13, 2026·0 cites·20 claims
- 1058US12560126B2Fan exit guide vane thermal management system for conventional gas turbine enginesRTX CORP·Filed 2024·Granted Feb 24, 2026·0 cites·18 claims
- 1156US2026085633A1High voltage engine-mounted electronics pressurization bleed systemRTX CORP·Filed 2024·Application pending·0 cites
- 1254US12595765B2Bifurcation integrated electrical system for hybrid aircraft propulsion systemRTX CORP·Filed 2024·Granted Apr 7, 2026·0 cites·16 claims
- 1354US12589878B1Hybrid-electric aircraft propulsion systemRTX CORP·Filed 2025·Granted Mar 31, 2026·0 cites·20 claims
- 1454US12584419B1Open rotor gas turbine engine with adaptive turbine clearance control system and methodRTX CORP·Filed 2024·Granted Mar 24, 2026·0 cites·15 claims
- 1554US2026035082A1Low spool electrical machine arrangements for hybrid-electric enginesRTX CORP·Filed 2024·Application pending·0 cites
- 1654US2026001499A1Power feeder cable conduit for hybrid electric gas turbine engines and fan mounted motor controllersRTX CORP·Filed 2024·Application pending·0 cites
- 1754US2026022668A1Gearbox arrangement for dual spool engine accessoriesRTX CORP·Filed 2024·Application pending·0 cites
- 1847US2026092561A1Turbine cooling air throttling valve and system for hybrid electric enginesRTX CORP·Filed 2024·Application pending·0 cites
- 1947US2026098500A1Modulated air flow heat exchanger system in bi-fi ductRTX CORP·Filed 2024·Application pending·0 cites
- 2044US2026005637A1Multi-spool engine electrical load balancing to optimize fuel burn based on ambient and system thermal conditionsHAMILTON SUNDSTRAND CORP·Filed 2024·Application pending·0 cites
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Identity basis: exact name match across USPTO filings. How scoring works →