Inventor · disambiguated record
Nathan L. Messersmith
Also filed as: MESSERSMITH NATHAN L
9 granted patents·1 pending application·50 citations·filing 2004–2023
83Inventor score
Top patents by PatentIndex Score
10 records- 0191US12110839B1Variable area nozzle assembly for an aircraft propulsion systemRTX CORP·Filed 2023·Granted Oct 8, 2024·2 cites·20 claims
- 0288US7775460B2Combustion nozzle fluidic injection assemblyUNITED TECHNOLOGIES CORP·Filed 2006·Granted Aug 17, 2010·32 cites·20 claims
- 0379US10975713B2Hydrostatic seal with aft toothUNITED TECHNOLOGIES CORP·Filed 2019·Granted Apr 13, 2021·2 cites·13 claims
- 0478US10371090B2Variable area exhaust mixer for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·2 cites·8 claims
- 0573US12123309B2After-fan system with electrical motor for gas turbine enginesRTX CORP·Filed 2023·Granted Oct 22, 2024·0 cites·4 claims
- 0661US11846196B2After-fan system with electrical motor for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2020·Granted Dec 19, 2023·0 cites·15 claims
- 0761US2019316544A1Variable area exhaust mixer for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 0855US12065937B1Variable area nozzle assembly for an aircraft propulsion systemRTX CORP·Filed 2023·Granted Aug 20, 2024·0 cites·20 claims
- 0951US7481038B2Yaw vectoring for exhaust nozzleUNITED TECHNOLOGIES CORP·Filed 2004·Granted Jan 27, 2009·12 cites·16 claims
- 1050US11585294B2High bypass ratio engine bypass duct nozzle with controlled nozzle areaRAYTHEON TECH CORP·Filed 2020·Granted Feb 21, 2023·0 cites·16 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →