Inventor · disambiguated record
Eric A. Grover
Also filed as: GROVER ERIC A
32 granted patents·5 pending applications·306 citations·filing 2004–2022
97Inventor score
Files withUNITED TECHNOLOGIES CORP25GROVER ERIC A3ALLEN-BRADLEY EUNICE2PRAISNER THOMAS J2RAYTHEON TECH CORP2
Top patents by PatentIndex Score
37 records- 0196US10995861B2Cantilevered hydrostatic advanced low leakage sealUNITED TECHNOLOGIES CORP·Filed 2019·Granted May 4, 2021·13 cites·14 claims
- 0295US11359726B2Non-contact seal assembly with multiple axially spaced spring elementsRAYTHEON TECH CORP·Filed 2020·Granted Jun 14, 2022·4 cites·20 claims
- 0395US8356975B2Gas turbine engine with non-axisymmetric surface contoured vane platformUNITED TECHNOLOGIES CORP·Filed 2010·Granted Jan 22, 2013·21 cites·18 claims
- 0494US9140128B2Endwall contouringUNITED TECHNOLOGIES CORP·Filed 2012·Granted Sep 22, 2015·18 cites·18 claims
- 0593US7887297B2Airfoil array with an endwall protrusion and components of the arrayUNITED TECHNOLOGIES CORP·Filed 2006·Granted Feb 15, 2011·46 cites·30 claims
- 0689US8105037B2Endwall with leading-edge humpGROVER ERIC A·Filed 2009·Granted Jan 31, 2012·41 cites·18 claims
- 0789US7251592B1Boundary layer transition modelUNITED TECHNOLOGIES CORP·Filed 2004·Granted Jul 31, 2007·57 cites·20 claims
- 0887US11473434B2Gas turbine engine airfoilUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 18, 2022·4 cites·20 claims
- 0985US10982770B2Hydrostatic seal with extended housingUNITED TECHNOLOGIES CORP·Filed 2019·Granted Apr 20, 2021·3 cites·16 claims
- 1082US9976433B2Gas turbine engine with non-axisymmetric surface contoured rotor blade platformPRAISNER THOMAS J·Filed 2010·Granted May 22, 2018·8 cites·23 claims
- 1181US11378187B2Articulating cantilevered hydrostatic sealUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jul 5, 2022·2 cites·20 claims
- 1280US10961858B2Hydrostatic seal with enhanced maneuver responseUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 30, 2021·2 cites·16 claims
- 1379US10975713B2Hydrostatic seal with aft toothUNITED TECHNOLOGIES CORP·Filed 2019·Granted Apr 13, 2021·2 cites·13 claims
- 1479US9951638B2Shaped rim cavity wing surfaceUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 24, 2018·2 cites·20 claims
- 1579US8511978B2Airfoil array with an endwall depression and components of the arrayALLEN-BRADLEY EUNICE·Filed 2006·Granted Aug 20, 2013·18 cites·20 claims
- 1678US8678740B2Turbomachine flow path having circumferentially varying outer peripheryPRAISNER THOMAS J·Filed 2011·Granted Mar 25, 2014·6 cites·18 claims
- 1778US8240121B2Retrofit dirt separator for gas turbine engineHAZZARD ROBERT L·Filed 2007·Granted Aug 14, 2012·23 cites·13 claims
- 1877US12140229B2Non-contact seal assembly with multiple spaced spring elementsRTX CORP·Filed 2022·Granted Nov 12, 2024·0 cites·20 claims
- 1973US7686567B2Airfoil embodying mixed loading conventionsUNITED TECHNOLOGIES CORP·Filed 2005·Granted Mar 30, 2010·9 cites·27 claims
- 2072US9212558B2Endwall contouringUNITED TECHNOLOGIES CORP·Filed 2012·Granted Dec 15, 2015·4 cites·20 claims
- 2171US11028717B2Bearing assembly for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 8, 2021·1 cites·21 claims
- 2267US11118471B2Variable area vane endwall treatmentsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 14, 2021·3 cites·19 claims
- 2365US10385728B2Airfoil contour for low-loss on-boarding of cooling air through an articulating spindleUNITED TECHNOLOGIES CORP·Filed 2014·Granted Aug 20, 2019·2 cites·22 claims
- 2464US9926806B2Turbomachine flow path having circumferentially varying outer peripheryUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 27, 2018·1 cites·15 claims
- 2564US9181815B2Shaped rim cavity wing surfaceGROVER ERIC A·Filed 2012·Granted Nov 10, 2015·2 cites·5 claims
- 2664US8366399B2Blade or vane with a laterally enlarged baseUNITED TECHNOLOGIES CORP·Filed 2006·Granted Feb 5, 2013·8 cites·20 claims
- 2763US2020024984A1Endwall ControuringUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 2860US8517686B2Flow passage for gas turbine engineALLEN-BRADLEY EUNICE·Filed 2009·Granted Aug 27, 2013·6 cites·17 claims
- 2953US2014154068A1Endwall ControuringUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 3052US10519796B2Variable area turbine vane row assemblyUNITED TECHNOLOGIES CORP·Filed 2014·Granted Dec 31, 2019·0 cites·11 claims
- 3147US9382807B2Non-axisymmetric rim cavity features to improve sealing efficienciesGROVER ERIC A·Filed 2012·Granted Jul 5, 2016·0 cites·5 claims
- 3246US12410723B2Non-contact seal for rotational equipment with radial through-holeUNITED TECHNOLOGIES CORP·Filed 2020·Granted Sep 9, 2025·0 cites·17 claims
- 3346US11619309B2Non-contact seal for rotational equipment with axially expended seal shoesRAYTHEON TECH CORP·Filed 2020·Granted Apr 4, 2023·0 cites·13 claims
- 3446US2020362714A1Brush secondary seal for cantilevered hydrostatic advanced low leakage sealUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 3541US9957801B2Airfoil design having localized suction side curvaturesAGGARWALA ANDREW S·Filed 2012·Granted May 1, 2018·0 cites·16 claims
- 3639US2019078450A1Inlet guide vane having a varied trailing edge geometryUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 3736US2017335712A1Variable area vane having minimized end gap lossesUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →