Inventor · disambiguated record
Shawn J. Gregg
Also filed as: GREGG SHAWN · GREGG SHAWN J
28 granted patents·4 pending applications·513 citations·filing 2003–2017
97Inventor score
Files withUNITED TECHNOLOGIES CORP23GREGG SHAWN J2MALECKI STACY T2BERGMAN RUSSELL J1LEVINE JEFFREY R1
Top patents by PatentIndex Score
32 records- 0198US8961108B2Cooling system for a turbine vaneBERGMAN RUSSELL J·Filed 2012·Granted Feb 24, 2015·51 cites·23 claims
- 0296US9103225B2Blade outer air seal with cored passagesLUTJEN PAUL M·Filed 2012·Granted Aug 11, 2015·31 cites·20 claims
- 0395US8480366B2Recessed metering standoffs for airfoil baffleMALECKI STACY T·Filed 2011·Granted Jul 9, 2013·47 cites·20 claims
- 0491US8807955B2Abrasive airfoil tipWRABEL PETER·Filed 2011·Granted Aug 19, 2014·25 cites·20 claims
- 0590US10196917B2Blade outer air seal with cored passagesUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 5, 2019·6 cites·20 claims
- 0689US10024172B2Gas turbine engine airfoilUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 17, 2018·6 cites·18 claims
- 0788US9222364B2Platform cooling circuit for a gas turbine engine componentPAPPLE MICHAEL LESLIE CLYDE·Filed 2012·Granted Dec 29, 2015·12 cites·8 claims
- 0888US8348613B2Airflow influencing airfoil feature arrayUNITED TECHNOLOGIES CORP·Filed 2009·Granted Jan 8, 2013·29 cites·21 claims
- 0988US8109724B2Recessed metering standoffs for airfoil baffleMALECKI STACY T·Filed 2009·Granted Feb 7, 2012·32 cites·37 claims
- 1087US7125225B2Cooled rotor blade with vibration damping deviceUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 24, 2006·52 cites·19 claims
- 1185US10502075B2Platform cooling circuit for a gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 10, 2019·3 cites·17 claims
- 1284US7467924B2Turbine blade including revised platformUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 23, 2008·25 cites·16 claims
- 1383US10239156B2Multi-density, multi-property turbine componentUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 26, 2019·3 cites·20 claims
- 1481US9476313B2Gas turbine engine including a pre-diffuser heat exchangerUNITED TECHNOLOGIES CORP·Filed 2012·Granted Oct 25, 2016·7 cites·20 claims
- 1578US9334755B2Airfoil with variable trip strip heightUNITED TECHNOLOGIES CORP·Filed 2012·Granted May 10, 2016·6 cites·13 claims
- 1678US6929451B2Cooled rotor blade with vibration damping deviceUNITED TECHNOLOGIES CORP·Filed 2003·Granted Aug 16, 2005·33 cites·15 claims
- 1777US7452186B2Turbine blade including revised trailing edge coolingUNITED TECHNOLOGIES CORP·Filed 2005·Granted Nov 18, 2008·19 cites·25 claims
- 1874US9759072B2Gas turbine engine airfoil cooling circuit arrangementGREGG SHAWN J·Filed 2012·Granted Sep 12, 2017·5 cites·16 claims
- 1973US7632071B2Cooled turbine bladeUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 15, 2009·19 cites·15 claims
- 2071US7665968B2Cooled rotor bladeUNITED TECHNOLOGIES CORP·Filed 2004·Granted Feb 23, 2010·26 cites·4 claims
- 2170US7186082B2Cooled rotor blade and method for cooling a rotor bladeUNITED TECHNOLOGIES CORP·Filed 2004·Granted Mar 6, 2007·26 cites·7 claims
- 2268US9145775B2Tapered thermal coating for airfoilLEVINE JEFFREY R·Filed 2012·Granted Sep 29, 2015·3 cites·23 claims
- 2360US8353668B2Airfoil insert having a tab extending away from the body defining a portion of outlet peripheryUNITED TECHNOLOGIES CORP·Filed 2009·Granted Jan 15, 2013·6 cites·9 claims
- 2457US11377965B2Gas turbine engine airfoil cooling circuit arrangementUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 5, 2022·0 cites·10 claims
- 2556US9080452B2Gas turbine engine airfoil with vane platform cooling passageUNITED TECHNOLOGIES CORP·Filed 2012·Granted Jul 14, 2015·1 cites·14 claims
- 2655US7059825B2Cooled rotor bladeUNITED TECHNOLOGIES CORP·Filed 2004·Granted Jun 13, 2006·16 cites·14 claims
- 2754US7018176B2Cooled turbine airfoilUNITED TECHNOLOGIES CORP·Filed 2004·Granted Mar 28, 2006·15 cites·7 claims
- 2847US7033140B2Cooled rotor blade with vibration damping deviceUNITED TECHNOLOGIES CORP·Filed 2003·Granted Apr 25, 2006·9 cites·19 claims
- 2947US2016003152A1Gas turbine engine multi-vaned stator cooling configurationUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 3046US2014083111A1Gas turbine asymmetric fuel nozzle combustorUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 3136US2014083103A1Gas turbine asymmetric nozzle guide vanesGREGG SHAWN J·Filed 2012·Application pending·0 cites
- 3235US2005265839A1Cooled rotor bladeUNITED TECHNOLOGIES CORP·Filed 2004·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →