Inventor · disambiguated record
Matthew R. Feulner
Also filed as: FEULNER MATTHEW R
28 granted patents·6 pending applications·340 citations·filing 1996–2023
96Inventor score
Top patents by PatentIndex Score
34 records- 0196US10125691B2Bowed rotor start using a variable position starter valveUNITED TECHNOLOGIES CORP·Filed 2016·Granted Nov 13, 2018·13 cites·19 claims
- 0294US11674407B2Systems and methods for controlling blade tip clearancesRAYTHEON TECH CORP·Filed 2022·Granted Jun 13, 2023·2 cites·17 claims
- 0394US10457401B2Dual-use air turbine system for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 29, 2019·14 cites·16 claims
- 0494US10040577B2Modified start sequence of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 7, 2018·17 cites·8 claims
- 0593US10774788B2Particle extraction system for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Sep 15, 2020·8 cites·15 claims
- 0693US9540944B2Real time model based compressor controlUNITED TECHNOLOGIES CORP·Filed 2012·Granted Jan 10, 2017·24 cites·18 claims
- 0791US9909497B2Combined stability and customer bleed with dirt, water and ice rejectionUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 6, 2018·6 cites·13 claims
- 0890US6195982B1Apparatus and method of active flutter controlUNITED TECHNOLOGIES CORP·Filed 1998·Granted Mar 6, 2001·78 cites·37 claims
- 0984US10625881B2Modified start sequence of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Apr 21, 2020·3 cites·11 claims
- 1084US10293951B2Takeoff power management system and method for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2016·Granted May 21, 2019·4 cites·18 claims
- 1184US6059522ACompressor stall diagnostics and avoidanceUNITED TECHNOLOGIES CORP·Filed 1996·Granted May 9, 2000·62 cites·13 claims
- 1276US6574965B1Rotor tip bleed in gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 1998·Granted Jun 10, 2003·50 cites·16 claims
- 1373US12098681B2High and low spool configuration for a gas turbine engineRTX CORP·Filed 2023·Granted Sep 24, 2024·0 cites·16 claims
- 1472US11339678B2Systems and methods for controlling blade tip clearancesUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 24, 2022·1 cites·11 claims
- 1572US6010303AApparatus and method of predicting aerodynamic and aeromechanical instabilities in turbofan enginesUNITED TECHNOLOGIES CORP·Filed 1998·Granted Jan 4, 2000·48 cites·13 claims
- 1672US2023258192A1Compressor arrangement for a gas turbine engineRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 1770US11473510B2Active multi-effector control of high pressure turbine clearancesUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 18, 2022·1 cites·17 claims
- 1870US9291064B2Anti-icing core inlet stator assembly for a gas turbine engineFEULNER MATTHEW R·Filed 2012·Granted Mar 22, 2016·6 cites·3 claims
- 1966US11719245B2Compressor arrangement for a gas turbine engineRAYTHEON TECH CORP·Filed 2021·Granted Aug 8, 2023·0 cites·8 claims
- 2065US11754000B2High and low spool configuration for a gas turbine engineRAYTHEON TECH CORP·Filed 2021·Granted Sep 12, 2023·0 cites·12 claims
- 2161US10060284B2Engine inlet total air temperature sensorUNITED TECHNOLOGIES CORP·Filed 2013·Granted Aug 28, 2018·1 cites·19 claims
- 2258US10787277B2Modified start sequence of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 29, 2020·0 cites·16 claims
- 2357US10495006B2Variable geometry gas turbine engine for use in inclement weatherUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 3, 2019·1 cites·6 claims
- 2454US11459946B2Gas turbine engine spool couplingUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 4, 2022·0 cites·18 claims
- 2551US10167783B2Low pressure compressor variable vane control for two-spool turbofan or turboprop engineCOLLOPY GARY·Filed 2012·Granted Jan 1, 2019·1 cites·20 claims
- 2651US9982689B2Apparatus and method for water and ice flow management in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 29, 2018·0 cites·16 claims
- 2750US10330010B2Compressor core inner diameter coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 25, 2019·0 cites·18 claims
- 2849US11391205B2Anti-icing core inlet stator assembly for a gas turbine engineRAYTHEON TECH CORP·Filed 2015·Granted Jul 19, 2022·0 cites·5 claims
- 2949US10718272B2Variable-geometry boundary layer diverterUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 21, 2020·0 cites·13 claims
- 3044US2023027726A1High and low spool configuration for a gas turbine engineRAYTHEON TECH CORP·Filed 2021·Application pending·0 cites
- 3144US2014090392A1Model based fuel-air ratio controlUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 3240US2017342913A1Gas turbine engine inlet temperature sensor configurationUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
- 3339US2017241340A1Turbocompressor for aircraft environmental control systemUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
- 3436US2023026997A1Gas 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 →