Inventor · disambiguated record
Nagendra Somanath
Also filed as: SOMANATH NAGENDRA
24 granted patents·3 pending applications·562 citations·filing 2006–2019
96Inventor score
Top patents by PatentIndex Score
27 records- 0198US7632064B2Variable geometry guide vane for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2006·Granted Dec 15, 2009·206 cites·18 claims
- 0297US7594404B2Embedded mount for mid-turbine frameUNITED TECHNOLOGIES CORP·Filed 2006·Granted Sep 29, 2009·71 cites·8 claims
- 0396US7815417B2Guide vane for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2006·Granted Oct 19, 2010·60 cites·5 claims
- 0494US10160550B1Ice detection and real time ice estimation using innovative sensor data learning approachesUNITED TECHNOLOGIES CORP·Filed 2017·Granted Dec 25, 2018·20 cites·18 claims
- 0594US7610763B2Tailorable design configuration topologies for aircraft engine mid-turbine framesUNITED TECHNOLOGIES CORP·Filed 2006·Granted Nov 3, 2009·38 cites·6 claims
- 0691US7797946B2Double U design for mid-turbine frame strutsUNITED TECHNOLOGIES CORP·Filed 2006·Granted Sep 21, 2010·34 cites·17 claims
- 0789US7677047B2Inverted stiffened shell panel torque transmission for loaded struts and mid-turbine framesUNITED TECHNOLOGIES CORP·Filed 2006·Granted Mar 16, 2010·27 cites·2 claims
- 0887US7594405B2Catenary mid-turbine frame designUNITED TECHNOLOGIES CORP·Filed 2008·Granted Sep 29, 2009·20 cites·11 claims
- 0985US11230948B2Work recovery system for a gas turbine engine utilizing an overexpanded, recuperated supercritical CO2 bottoming cycleUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jan 25, 2022·5 cites·22 claims
- 1085US8113768B2Actuated variable geometry mid-turbine frame designSOMANATH NAGENDRA·Filed 2008·Granted Feb 14, 2012·15 cites·16 claims
- 1184US11447271B2Aircraft component repair scheduling system and processUNITED TECHNOLOGIES CORP·Filed 2019·Granted Sep 20, 2022·4 cites·22 claims
- 1284US8388306B2Method for varying the geometry of a mid-turbine frameSOMANATH NAGENDRA·Filed 2012·Granted Mar 5, 2013·7 cites·7 claims
- 1384US7775049B2Integrated strut design for mid-turbine frames with U-baseUNITED TECHNOLOGIES CORP·Filed 2006·Granted Aug 17, 2010·18 cites·9 claims
- 1482US8181467B2Mid-turbine frame torque box having a concave surfaceKUMAR KESHAVA B·Filed 2010·Granted May 22, 2012·7 cites·4 claims
- 1579US8181466B2Mid-turbine frameKUMAR KESHAVA B·Filed 2010·Granted May 22, 2012·6 cites·12 claims
- 1673US7762087B2Rotatable integrated segmented mid-turbine framesUNITED TECHNOLOGIES CORP·Filed 2006·Granted Jul 27, 2010·13 cites·18 claims
- 1765US8001791B2Turbine engine frame having an actuated equilibrating caseUNITED TECHNOLOGIES CORP·Filed 2007·Granted Aug 23, 2011·9 cites·19 claims
- 1854US11676009B2Machine learning based rotor alloy design systemUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jun 13, 2023·0 cites·17 claims
- 1950US11248989B2System and method for analyzing engine test data in real timeUNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 15, 2022·0 cites·19 claims
- 2049US8707710B2Tailorable design configuration topologies for aircraft engine mid-turbine framesSOMANATH NAGENDRA·Filed 2009·Granted Apr 29, 2014·2 cites·12 claims
- 2148US11397134B2Intelligent learning device for part state detection and identificationUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jul 26, 2022·0 cites·14 claims
- 2248US2020224590A1Work recovery system for a gas turbine engine utilizing a recuperated supercritical co2 cycle driven by cooled cooling air waste heatUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2348US2020224557A1Work recovery system for a gas turbine engine utilizing an overexpanded, recuperated supercritical co2 cycle driven by cooled cooling air waste heatUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2447US11485520B2Material selection and optimization process for component manufacturingUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 1, 2022·0 cites·20 claims
- 2544US12162627B2Aircraft component repair system and processUNITED TECHNOLOGIES CORP·Filed 2019·Granted Dec 10, 2024·0 cites·20 claims
- 2642US2020224588A1Work recovery system for a gas turbine engine utilizing a recuperated supercritical co2 bottoming cycleUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2741US8568083B2Spool support structure for a multi-spool gas turbine engineSOMANATH NAGENDRA·Filed 2009·Granted Oct 29, 2013·0 cites·17 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →