Inventor · disambiguated record
Stephen G. Pixton
Also filed as: PIXTON STEPHEN G
15 granted patents·4 pending applications·14 citations·filing 2009–2024
86Inventor score
Top patents by PatentIndex Score
19 records- 0195US11454129B1CMC component flow discourager flangesRAYTHEON TECH CORP·Filed 2021·Granted Sep 27, 2022·7 cites·7 claims
- 0290US12203385B1Telescoping guide vane for aircraft propulsion systemRTX CORP·Filed 2024·Granted Jan 21, 2025·2 cites·17 claims
- 0388US11814968B2Gas turbine engine with idle thrust ratioRAYTHEON TECH CORP·Filed 2021·Granted Nov 14, 2023·2 cites·22 claims
- 0486US11808154B2CMC component flow discourager flangesRAYTHEON TECH CORP·Filed 2022·Granted Nov 7, 2023·1 cites·19 claims
- 0573US12098681B2High and low spool configuration for a gas turbine engineRTX CORP·Filed 2023·Granted Sep 24, 2024·0 cites·16 claims
- 0672US2023258192A1Compressor arrangement for a gas turbine engineRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 0771US12123310B2Gas turbine engine with idle thrust ratioRTX CORP·Filed 2023·Granted Oct 22, 2024·0 cites·21 claims
- 0866US11719245B2Compressor arrangement for a gas turbine engineRAYTHEON TECH CORP·Filed 2021·Granted Aug 8, 2023·0 cites·8 claims
- 0965US11754000B2High and low spool configuration for a gas turbine engineRAYTHEON TECH CORP·Filed 2021·Granted Sep 12, 2023·0 cites·12 claims
- 1064US12352287B1Variable guide vane for aircraft propulsion systemRTX CORP·Filed 2024·Granted Jul 8, 2025·0 cites·19 claims
- 1164US9897001B2Compressor areas for high overall pressure ratio gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 20, 2018·1 cites·20 claims
- 1258US9771863B2Gas turbine engine with embedded distributed fansUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 26, 2017·1 cites·5 claims
- 1357US2009194459A1Fuel processing of feedstocks having components harmful to hydrodesulfurizationVINCITORE ANTONIO M·Filed 2009·Application pending·0 cites
- 1445US9745526B2Fuel processing of feedstocks having components harmful to hydrodesulfurizationVINCITORE ANTONIO M·Filed 2012·Granted Aug 29, 2017·0 cites·2 claims
- 1544US12392280B2Gas turbine engine with high low spool power extraction ratioRAYTHEON TECH CORP·Filed 2021·Granted Aug 19, 2025·0 cites·2 claims
- 1644US12123356B2Gas turbine engine with higher low spool torque-to-thrust ratioRAYTHEON TECH CORP·Filed 2021·Granted Oct 22, 2024·0 cites·10 claims
- 1744US2023027726A1High and low spool configuration for a gas turbine engineRAYTHEON TECH CORP·Filed 2021·Application pending·0 cites
- 1841US10472071B2Hybrid compressor bleed air for aircraft useUNITED TECHNOLOGIES CORP·Filed 2015·Granted Nov 12, 2019·0 cites·19 claims
- 1936US2023026997A1Gas turbine engine compressor arrangementRAYTHEON TECH CORP·Filed 2021·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →