Inventor · disambiguated record
Shankar S. Magge
Also filed as: JANSEN WILLEM · MAGGE SHANKAR S
25 granted patents·6 pending applications·453 citations·filing 1978–2022
96Inventor score
Files withUNITED TECHNOLOGIES CORP13RAYTHEON TECH CORP8ADAMS PAUL R2PRAISNER THOMAS J2SUCIU GABRIEL L2
Top patents by PatentIndex Score
31 records- 0199US10060357B2Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 28, 2018·23 cites·27 claims
- 0298US10371061B2Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 6, 2019·11 cites·33 claims
- 0396US9028200B2Counter rotating low pressure turbine with splitter gear systemSUCIU GABRIEL L·Filed 2012·Granted May 12, 2015·23 cites·21 claims
- 0495US11149650B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2018·Granted Oct 19, 2021·7 cites·30 claims
- 0595US8844265B2Turbine section of high bypass turbofanADAMS PAUL R·Filed 2012·Granted Sep 30, 2014·28 cites·20 claims
- 0695US8105019B23D contoured vane endwall for variable area turbine vane arrangementMCCAFFREY MICHAEL G·Filed 2007·Granted Jan 31, 2012·44 cites·20 claims
- 0794US4212585ACentrifugal compressorNORTHERN RES AND ENGR CORP·Filed 1978·Granted Jul 15, 1980·146 cites·17 claims
- 0893US8424313B1Gas turbine engine mid turbine frame with flow turning featuresPRAISNER THOMAS J·Filed 2012·Granted Apr 23, 2013·16 cites·26 claims
- 0992US11480108B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2021·Granted Oct 25, 2022·2 cites·30 claims
- 1092US8850793B2Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2013·Granted Oct 7, 2014·11 cites·18 claims
- 1191US8561414B1Gas turbine engine mid turbine frame with flow turning featuresUNITED TECHNOLOGIES CORP·Filed 2013·Granted Oct 22, 2013·12 cites·23 claims
- 1290US11242805B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2018·Granted Feb 8, 2022·5 cites·31 claims
- 1390US8935926B2Centrifugal compressor with bleed flow splitter for a gas turbine engineWAGNER JOEL H·Filed 2010·Granted Jan 20, 2015·11 cites·6 claims
- 1487US9010085B2Turbine section of high bypass turbofanADAMS PAUL R·Filed 2012·Granted Apr 21, 2015·8 cites·23 claims
- 1584US11346289B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2020·Granted May 31, 2022·2 cites·14 claims
- 1684US7094034B2Airfoil profile with optimized aerodynamic shapeUNITED TECHNOLOGIES CORP·Filed 2004·Granted Aug 22, 2006·45 cites·8 claims
- 1783US8915090B2Gas turbine engine mid turbine frame with flow turning featuresUNITED TECHNOLOGIES CORP·Filed 2014·Granted Dec 23, 2014·6 cites·28 claims
- 1883US8292570B2Low pressure turbine with counter-rotating drives for single spoolSUCIU GABRIEL L·Filed 2008·Granted Oct 23, 2012·19 cites·7 claims
- 1983US8052388B2Gas turbine engine systems involving mechanically alterable vane throat areasUNITED TECHNOLOGIES CORP·Filed 2007·Granted Nov 8, 2011·20 cites·20 claims
- 2082US11486311B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2021·Granted Nov 1, 2022·1 cites·30 claims
- 2173US11614036B2Turbine section of gas turbine engineRAYTHEON TECH CORP·Filed 2021·Granted Mar 28, 2023·0 cites·30 claims
- 2272US8075259B2Turbine vane airfoil with turning flow and axial/circumferential trailing edge configurationPRAISNER THOMAS J·Filed 2009·Granted Dec 13, 2011·13 cites·25 claims
- 2370US11215123B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2020·Granted Jan 4, 2022·0 cites·30 claims
- 2460US10794293B2Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 6, 2020·0 cites·27 claims
- 2557US10662880B2Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 26, 2020·0 cites·11 claims
- 2656US2015377123A1Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 2745US2023323836A1Turbine section of a gas turbine engineRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 2843US2016222815A1High Efficiency Geared TurbofanUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2940US2015377122A1Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 3038US2012070297A1Aft loaded airfoilESTES MATTHEW B·Filed 2010·Application pending·0 cites
- 3138US2015377124A1Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →