Inventor · disambiguated record
Jeffrey R. Levine
Also filed as: LEVINE JEFFREY · LEVINE JEFFREY R
24 granted patents·5 pending applications·292 citations·filing 1989–2019
95Inventor score
Files withUNITED TECHNOLOGIES CORP19LEVINE JEFFREY R6APPLIED CRYOGENICS INC1NADEAU DANIEL C1PEREZ RAFAEL A1
Top patents by PatentIndex Score
29 records- 0191US9279331B2Gas turbine engine airfoil with dirt purge feature and core for making sameLEVINE JEFFREY R·Filed 2012·Granted Mar 8, 2016·6 cites·18 claims
- 0290US7478994B2Airfoil with supplemental cooling channel adjacent leading edgeUNITED TECHNOLOGIES CORP·Filed 2004·Granted Jan 20, 2009·74 cites·31 claims
- 0385US9938837B2Gas turbine engine airfoil trailing edge passage and core for making sameUNITED TECHNOLOGIES CORP·Filed 2013·Granted Apr 10, 2018·4 cites·9 claims
- 0484US7467924B2Turbine blade including revised platformUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 23, 2008·25 cites·16 claims
- 0580US7445432B2Enhanced serpentine cooling with U-shaped divider ribUNITED TECHNOLOGIES CORP·Filed 2006·Granted Nov 4, 2008·20 cites·19 claims
- 0677US9982560B2Cooling feed orificesUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 29, 2018·3 cites·17 claims
- 0777US7452186B2Turbine blade including revised trailing edge coolingUNITED TECHNOLOGIES CORP·Filed 2005·Granted Nov 18, 2008·19 cites·25 claims
- 0875US9157329B2Gas turbine engine airfoil internal cooling featuresNADEAU DANIEL C·Filed 2012·Granted Oct 13, 2015·7 cites·17 claims
- 0973US7632071B2Cooled turbine bladeUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 15, 2009·19 cites·15 claims
- 1071US7665968B2Cooled rotor bladeUNITED TECHNOLOGIES CORP·Filed 2004·Granted Feb 23, 2010·26 cites·4 claims
- 1168US9145775B2Tapered thermal coating for airfoilLEVINE JEFFREY R·Filed 2012·Granted Sep 29, 2015·3 cites·23 claims
- 1267US9995147B2Blade tip cooling arrangementUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 12, 2018·1 cites·13 claims
- 1367US5174122AMethod and means of low temperature treatment of items and materials with cryogenic liquidAPPLIED CRYOGENICS INC·Filed 1989·Granted Dec 29, 1992·41 cites·18 claims
- 1464US10253634B2Gas turbine engine airfoil trailing edge suction side coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 9, 2019·2 cites·15 claims
- 1564US10119407B2Tapered thermal barrier coating on convex and concave trailing edge surfacesUNITED TECHNOLOGIES CORP·Filed 2013·Granted Nov 6, 2018·2 cites·8 claims
- 1662US10428666B2Turbine vane assemblyUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 1, 2019·1 cites·20 claims
- 1762US10294806B2Multiple coating configurationUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 21, 2019·0 cites·16 claims
- 1861US10808546B2Gas turbine engine airfoil trailing edge suction side coolingRAYTHEON TECH CORP·Filed 2019·Granted Oct 20, 2020·0 cites·20 claims
- 1961US9045987B2Cooling for a turbine airfoil trailing edgeLEVINE JEFFREY R·Filed 2012·Granted Jun 2, 2015·2 cites·17 claims
- 2060US8690538B2Leading edge cooling using chevron trip stripsLEVINE JEFFREY R·Filed 2006·Granted Apr 8, 2014·8 cites·6 claims
- 2159US10253635B2Blade tip cooling arrangementUNITED TECHNOLOGIES CORP·Filed 2018·Granted Apr 9, 2019·0 cites·22 claims
- 2259US7150601B2Turbine airfoil cooling passagewayUNITED TECHNOLOGIES CORP·Filed 2004·Granted Dec 19, 2006·17 cites·24 claims
- 2352US7195448B2Cooled rotor bladeUNITED TECHNOLOGIES CORP·Filed 2004·Granted Mar 27, 2007·12 cites·10 claims
- 2443US2014219813A1Gas turbine engine serpentine cooling passagePEREZ RAFAEL A·Filed 2012·Application pending·0 cites
- 2539US10132168B2AirfoilUNITED TECHNOLOGIES CORP·Filed 2016·Granted Nov 20, 2018·0 cites·19 claims
- 2638US2007297916A1Leading edge cooling using wrapped staggered-chevron trip stripsUNITED TECHNOLOGIES CORP·Filed 2006·Application pending·0 cites
- 2738US2017198601A1Internally cooled ni-base superalloy component with spallation-resistant tbc systemUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
- 2838US2012163993A1Leading edge airfoil-to-platform fillet cooling tubeLEVINE JEFFREY R·Filed 2010·Application pending·0 cites
- 2934US2005265840A1Cooled rotor blade with leading edge impingement coolingLEVINE JEFFREY R·Filed 2004·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →