Inventor · disambiguated record
Andrew S. Aggarwala
Also filed as: AGGARWALA ANDREW S
23 granted patents·4 pending applications·368 citations·filing 2001–2018
95Inventor score
Files withUNITED TECHNOLOGIES CORP17ZELESKY MARK F4AGGARWALA ANDREW S3NASH TIMOTHY CHARLES1O'HEARN JASON L1
Top patents by PatentIndex Score
27 records- 0195US6669445B2Endwall shape for use in turbomachineryUNITED TECHNOLOGIES CORP·Filed 2002·Granted Dec 30, 2003·108 cites·7 claims
- 0294US9140128B2Endwall contouringUNITED TECHNOLOGIES CORP·Filed 2012·Granted Sep 22, 2015·18 cites·18 claims
- 0393US6547524B2Film cooled article with improved temperature toleranceUNITED TECHNOLOGIES CORP·Filed 2001·Granted Apr 15, 2003·63 cites·14 claims
- 0492US9957817B2Tip leakage flow directionality controlZELESKY MARK F·Filed 2013·Granted May 1, 2018·13 cites·18 claims
- 0591US9803559B2Variable vane and seal arrangementUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 31, 2017·6 cites·18 claims
- 0689US10830073B2Vane assembly of a gas turbine engineRAYTHEON TECH CORP·Filed 2018·Granted Nov 10, 2020·4 cites·12 claims
- 0789US9777582B2Tip leakage flow directionality controlZELESKY MARK F·Filed 2013·Granted Oct 3, 2017·11 cites·21 claims
- 0889US9260972B2Tip leakage flow directionality controlZELESKY MARK F·Filed 2012·Granted Feb 16, 2016·12 cites·23 claims
- 0988US10648353B2Low loss airfoil platform rim seal assemblyUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 12, 2020·5 cites·10 claims
- 1088US7195456B2Turbine engine guide vane and arrays thereofUNITED TECHNOLOGIES CORP·Filed 2004·Granted Mar 27, 2007·59 cites·16 claims
- 1185US9175567B2Low loss airfoil platform trailing edgeAGGARWALA ANDREW S·Filed 2012·Granted Nov 3, 2015·10 cites·25 claims
- 1283US7581930B2High lift transonic turbine bladeUNITED TECHNOLOGIES CORP·Filed 2006·Granted Sep 1, 2009·24 cites·11 claims
- 1376US8360731B2Tip vortex controlUNITED TECHNOLOGIES CORP·Filed 2009·Granted Jan 29, 2013·15 cites·10 claims
- 1474US10774659B2Tip leakage flow directionality controlUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 15, 2020·1 cites·8 claims
- 1573US10815790B2Tip leakage flow directionality controlUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 27, 2020·1 cites·17 claims
- 1672US9212558B2Endwall contouringUNITED TECHNOLOGIES CORP·Filed 2012·Granted Dec 15, 2015·4 cites·20 claims
- 1765US10287901B2Vane assembly of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 14, 2019·1 cites·8 claims
- 1863US2020024984A1Endwall ControuringUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 1962US10844739B2Platforms with leading edge featuresUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 24, 2020·0 cites·18 claims
- 2062US9004861B2Blade tip having a recessed areaNASH TIMOTHY CHARLES·Filed 2012·Granted Apr 14, 2015·2 cites·18 claims
- 2153US9951629B2Tip leakage flow directionality controlZELESKY MARK F·Filed 2013·Granted Apr 24, 2018·0 cites·25 claims
- 2253US6932572B2Film cooled article with improved temperature toleranceUNITED TECHNOLOGIES CORP·Filed 2003·Granted Aug 23, 2005·11 cites·2 claims
- 2353US2014154068A1Endwall ControuringUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 2444US2016312654A1Turbine airfoil coolingUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2541US9957801B2Airfoil design having localized suction side curvaturesAGGARWALA ANDREW S·Filed 2012·Granted May 1, 2018·0 cites·16 claims
- 2640US2013315745A1Airfoil mateface sealingAGGARWALA ANDREW S·Filed 2012·Application pending·0 cites
- 2736US8439644B2Airfoil leading edge shape tailoring to reduce heat loadO'HEARN JASON L·Filed 2007·Granted May 14, 2013·0 cites·12 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →