Inventor · disambiguated record
Nagaraja Rudrapatna
Also filed as: RUDRAPATNA NAGARAJA · RUDRAPATNA NAGARAJA S
30 granted patents·8 pending applications·225 citations·filing 2006–2023
96Inventor score
Files withHONEYWELL INT INC20PRATT & WHITNEY CANADA5RUDRAPATNA NAGARAJA S5RUDRAPATNA NAGARAJA3PATEL BHAWAN2
Top patents by PatentIndex Score
38 records- 0195US9765968B2Combustors with complex shaped effusion holesHONEYWELL INT INC·Filed 2013·Granted Sep 19, 2017·21 cites·13 claims
- 0293US7559142B2Method of manufacturing a heat shield for a fuel manifoldPRATT & WHITNEY CANADA·Filed 2006·Granted Jul 14, 2009·25 cites·8 claims
- 0392US9625156B2Gas turbine engines having fuel injector shrouds with interior ribsHONEYWELL INT INC·Filed 2013·Granted Apr 18, 2017·15 cites·17 claims
- 0492US9038395B2Combustors with quench insertsRUDRAPATNA NAGARAJA S·Filed 2012·Granted May 26, 2015·22 cites·13 claims
- 0591US11519604B2Plug resistant effusion holes for gas turbine engineHONEYWELL INT INC·Filed 2021·Granted Dec 6, 2022·2 cites·20 claims
- 0691US11085641B2Plug resistant effusion holes for gas turbine engineHONEYWELL INT INC·Filed 2018·Granted Aug 10, 2021·6 cites·13 claims
- 0788US12085279B1Gas turbine combustor with enhanced cooling featuresHONEYWELL INT INC·Filed 2023·Granted Sep 10, 2024·2 cites·20 claims
- 0888US9062884B2Combustors with quench insertsRUDRAPATNA NAGARAJA S·Filed 2011·Granted Jun 23, 2015·18 cites·7 claims
- 0987US7926286B2Heat shield for a fuel manifoldPRATT & WHITNEY CANADA·Filed 2006·Granted Apr 19, 2011·15 cites·19 claims
- 1084US9021812B2Combustor dome and heat-shield assemblyPARDINGTON RONALD B·Filed 2012·Granted May 5, 2015·14 cites·16 claims
- 1184US9010123B2Combustors with quench insertsRUDRAPATNA NAGARAJA S·Filed 2010·Granted Apr 21, 2015·12 cites·6 claims
- 1279US11022308B2Double wall combustors with strain isolated insertsHONEYWELL INT INC·Filed 2018·Granted Jun 1, 2021·2 cites·18 claims
- 1378US8726631B2Dual walled combustors with impingement cooled ignitersRUDRAPATNA NAGARAJA S·Filed 2009·Granted May 20, 2014·18 cites·16 claims
- 1475US11162383B2System and method for cleaning cooling passages of a combustion chamberHONEYWELL INT INC·Filed 2019·Granted Nov 2, 2021·1 cites·14 claims
- 1572US8196410B2Stress reduction feature to improve fuel nozzle sheath durabilityPATEL BHAWAN·Filed 2007·Granted Jun 12, 2012·6 cites·14 claims
- 1672US8033113B2Fuel injection system for a gas turbine enginePRATT & WHITNEY CANADA·Filed 2007·Granted Oct 11, 2011·13 cites·18 claims
- 1770US11306659B2Plug resistant effusion holes for gas turbine engineHONEYWELL INT INC·Filed 2019·Granted Apr 19, 2022·1 cites·20 claims
- 1870US8171634B2Method of producing effusion holesRUDRAPATNA NAGARAJA·Filed 2007·Granted May 8, 2012·5 cites·10 claims
- 1966US7703289B2Internal fuel manifold having temperature reduction featurePRATT & WHITNEY CANADA·Filed 2006·Granted Apr 27, 2010·10 cites·22 claims
- 2065US11326781B2Liner for a combustor with strain isolated insertsHONEYWELL INT INC·Filed 2020·Granted May 10, 2022·0 cites·19 claims
- 2159US8555649B2Fuel nozzle swirler assemblyPATEL BHAWAN B·Filed 2009·Granted Oct 15, 2013·6 cites·6 claims
- 2256US10900377B2System and method for monitoring for sand plugging in gas turbine enginesHONEYWELL INT INC·Filed 2018·Granted Jan 26, 2021·0 cites·18 claims
- 2355US10519868B2System and method for cleaning cooling passages of a combustion chamberHONEYWELL INT INC·Filed 2017·Granted Dec 31, 2019·0 cites·11 claims
- 2453US8429916B2Dual walled combustors with improved liner sealsRUDRAPATNA NAGARAJA S·Filed 2009·Granted Apr 30, 2013·5 cites·16 claims
- 2552US2010209633A1Curved test specimenHONEYWELL INT INC·Filed 2009·Application pending·0 cites
- 2650US11674686B2Coating occlusion resistant effusion cooling holes for gas turbine engineHONEYWELL INT INC·Filed 2021·Granted Jun 13, 2023·0 cites·18 claims
- 2750US9897320B2Effusion cooled dual wall gas turbine combustorsBRONSON THOMAS J·Filed 2009·Granted Feb 20, 2018·3 cites·20 claims
- 2849US8794005B2Combustor constructionRUDRAPATNA NAGARAJA·Filed 2006·Granted Aug 5, 2014·3 cites·10 claims
- 2948US8935925B2Stress reduction feature to improve fuel nozzle sheath durabilityPATEL BHAWAN·Filed 2012·Granted Jan 20, 2015·0 cites·3 claims
- 3046US8695217B2Hole producing systemRUDRAPATNA NAGARAJA·Filed 2012·Granted Apr 15, 2014·0 cites·9 claims
- 3143US2022213797A1Turbomachine with low leakage seal assembly for combustor-turbine interfaceHONEYWELL INT INC·Filed 2021·Application pending·0 cites
- 3242US2010095679A1Dual wall structure for use in a combustor of a gas turbine engineHONEYWELL INT INC·Filed 2008·Application pending·0 cites
- 3341US2011185739A1Gas turbine combustors with dual walled linersHONEYWELL INT INC·Filed 2010·Application pending·0 cites
- 3440US11988386B2Gas turbine engine injector module with thermally coupled fuel lines having respective outletsHONEYWELL INT INC·Filed 2021·Granted May 21, 2024·0 cites·16 claims
- 3540US2022213796A1Turbomachine with low leakage seal assembly for combustor-turbine interfaceHONEYWELL INT INC·Filed 2021·Application pending·0 cites
- 3640US2010212324A1Dual walled combustors with impingement cooled ignitersHONEYWELL INT INC·Filed 2009·Application pending·0 cites
- 3739US2008053096A1Fuel injection system and method of assemblyPRATT & WHITNEY CANADA·Filed 2006·Application pending·0 cites
- 3838US2010095680A1Dual wall structure for use in a combustor of a gas turbine engineHONEYWELL INT INC·Filed 2008·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →