Inventor · disambiguated record
Morris G. Anderson
Also filed as: ANDERSON MORRIS · ANDERSON MORRIS G
37 granted patents·7 pending applications·530 citations·filing 2002–2024
97Inventor score
Top patents by PatentIndex Score
44 records- 0196US9664542B2Systems and methods for additive manufacturing for air data probesHONEYWELL INT INC·Filed 2015·Granted May 30, 2017·34 cites·11 claims
- 0295US10197588B2Thin film heating systems for air data probesHONEYWELL INT INC·Filed 2016·Granted Feb 5, 2019·16 cites·11 claims
- 0395US9856027B2Air data probe with double helical coil heater cableHONEYWELL INT INC·Filed 2015·Granted Jan 2, 2018·18 cites·19 claims
- 0494US11649056B2Thermally isolated sensor for gas turbine engineHONEYWELL INT INC·Filed 2020·Granted May 16, 2023·4 cites·16 claims
- 0594US7506501B2Compact mixer with trimmable open centerbodyHONEYWELL INT INC·Filed 2005·Granted Mar 24, 2009·81 cites·10 claims
- 0693US10384787B2Forming an air data probe from a porous cover and brazing materialHONEYWELL INT INC·Filed 2016·Granted Aug 20, 2019·16 cites·9 claims
- 0793US10126320B2Arrangement of dams in air data probeHONEYWELL INT INC·Filed 2017·Granted Nov 13, 2018·14 cites·20 claims
- 0893US7927408B2Inlet particle separator systems and methodsHONEYWELL INT INC·Filed 2007·Granted Apr 19, 2011·47 cites·19 claims
- 0992US10436649B2Icing resistance total temperature probe with integrated ejectorHONEYWELL INT INC·Filed 2017·Granted Oct 8, 2019·8 cites·20 claims
- 1092US10221765B2Anti-icing exhaust systemHONEYWELL INT INC·Filed 2016·Granted Mar 5, 2019·9 cites·20 claims
- 1192US9950799B2Shielded anti-icing system and methodsHONEYWELL INT INC·Filed 2016·Granted Apr 24, 2018·10 cites·20 claims
- 1291US9791304B2Air data probe heater utilizing low melting point metalHONEYWELL INT INC·Filed 2015·Granted Oct 17, 2017·12 cites·20 claims
- 1389US7856824B2Cooling systems for use on aircraftHONEYWELL INT INC·Filed 2007·Granted Dec 28, 2010·43 cites·20 claims
- 1488US9045998B2System for directing air flow to a plurality of plenaLO CHARLES·Filed 2011·Granted Jun 2, 2015·20 cites·14 claims
- 1588US8024935B2Flush inlet scoop design for aircraft bleed air systemHONEYWELL INT INC·Filed 2008·Granted Sep 27, 2011·35 cites·20 claims
- 1688US7882696B2Integrated support and mixer for turbo machineryHONEYWELL INT INC·Filed 2007·Granted Feb 8, 2011·24 cites·20 claims
- 1785US10179654B2Architecture for air data probe power supply controlHONEYWELL INT INC·Filed 2015·Granted Jan 15, 2019·6 cites·18 claims
- 1885US6701715B2Variable geometry ejector for a bleed air system using integral ejector exit pressure feedbackHONEYWELL INT INC·Filed 2002·Granted Mar 9, 2004·70 cites·30 claims
- 1984US11560968B2Bleed valve with reduced noiseHONEYWELL INT INC·Filed 2020·Granted Jan 24, 2023·2 cites·18 claims
- 2084US10337454B2Thrust reverser with asymmetric vane geometryHONEYWELL INT INC·Filed 2016·Granted Jul 2, 2019·4 cites·8 claims
- 2183US10648426B2Single row vane assembly for a thrust reverserHONEYWELL INT INC·Filed 2016·Granted May 12, 2020·4 cites·6 claims
- 2282US11105691B2Self-regulating heating system for a total air temperature probeHONEYWELL INT INC·Filed 2018·Granted Aug 31, 2021·3 cites·20 claims
- 2379US11002222B2Systems and methods for thrust reverser with temperature and fluid managementHONEYWELL INT INC·Filed 2018·Granted May 11, 2021·2 cites·10 claims
- 2478US10401229B2Systems and methods for icing resistant total air temperature probesHONEYWELL INT INC·Filed 2016·Granted Sep 3, 2019·2 cites·16 claims
- 2577US11215631B2Multi-function air data probe having multi-hole ports used for determining angle of attack, total and static pressure valuesHONEYWELL INT INC·Filed 2020·Granted Jan 4, 2022·1 cites·13 claims
- 2676US10337931B2Systems and methods for icing resistant total air temperature probes with air jetsHONEYWELL INT INC·Filed 2017·Granted Jul 2, 2019·2 cites·11 claims
- 2767US11609243B2Method of health management and assessment for a multi-function air data probeHONEYWELL INT INC·Filed 2021·Granted Mar 21, 2023·0 cites·10 claims
- 2863US9969500B2Bifurcated ducts including plenums for stabilizing flow therethrough and exhaust systems including the sameHONEYWELL INT INC·Filed 2014·Granted May 15, 2018·3 cites·11 claims
- 2962US12410750B1Shielded swirl gas turbine engine inlet anti-icing systemHONEYWELL INT INC·Filed 2024·Granted Sep 9, 2025·0 cites·14 claims
- 3062US7146816B2Effusion momentum controlHONEYWELL INT INC·Filed 2004·Granted Dec 12, 2006·24 cites·14 claims
- 3161US10578638B2Arrangement of dams in air data probeHONEYWELL INT INC·Filed 2018·Granted Mar 3, 2020·0 cites·10 claims
- 3259US2021285399A1Systems for thrust reverser with temperature and fluid managementHONEYWELL INT INC·Filed 2021·Application pending·0 cites
- 3356US11422153B2Air data probe replacement determination systemHONEYWELL INT INC·Filed 2020·Granted Aug 23, 2022·0 cites·20 claims
- 3453US7389635B2Twisted mixer with open center bodyHONEYWELL INT INC·Filed 2004·Granted Jun 24, 2008·12 cites·31 claims
- 3549US7500353B2Eductor swirl busterHONEYWELL INT INC·Filed 2005·Granted Mar 10, 2009·2 cites·16 claims
- 3649US2022275733A1Ejector driven scavenge system for particle separator associated with gas turbine engineHONEYWELL INT INC·Filed 2022·Application pending·0 cites
- 3748US11859523B2MufflerHONEYWELL INT INC·Filed 2022·Granted Jan 2, 2024·0 cites·19 claims
- 3848US11674527B2Compressor ported shroud with particle separatorHONEYWELL INT INC·Filed 2020·Granted Jun 13, 2023·0 cites·20 claims
- 3943US2011126512A1Turbofan gas turbine engine aerodynamic mixerHONEYWELL INT INC·Filed 2009·Application pending·0 cites
- 4040US2008203218A1Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second AreaHONEYWELL INT INC·Filed 2007·Application pending·0 cites
- 4138US2017074167A1Turbofan engine mounted precooler systemHONEYWELL INT INC·Filed 2015·Application pending·0 cites
- 4237US7464535B2Rocket motor nozzle throat area control system and methodHONEYWELL INT INC·Filed 2004·Granted Dec 16, 2008·2 cites·22 claims
- 4336US2017204808A1Translating cowl thrust reverser having a pressure imbalance that reduces overall structural loadHONEYWELL INT INC·Filed 2016·Application pending·0 cites
- 4433US2006150612A1Thrust vector controlHONEYWELL INT INC·Filed 2005·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →