Inventor · disambiguated record
Atul Kohli
Also filed as: KOHLI ATUL
33 granted patents·8 pending applications·334 citations·filing 2001–2021
97Inventor score
Top patents by PatentIndex Score
41 records- 0197US8683813B2Multi-lobed cooling hole and method of manufactureXU JINQUAN·Filed 2012·Granted Apr 1, 2014·32 cites·28 claims
- 0296US10301964B2Baffle with flow augmentation featureUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 28, 2019·10 cites·13 claims
- 0395US9022737B2Airfoil including trench with contoured surfacePIGGUSH JUSTIN D·Filed 2011·Granted May 5, 2015·23 cites·29 claims
- 0494US8733111B2Cooling hole with asymmetric diffuserGLEINER MATTHEW S·Filed 2012·Granted May 27, 2014·18 cites·20 claims
- 0594US8105030B2Cooled airfoils and gas turbine engine systems involving such airfoilsABDEL-MESSEH WILLIAM·Filed 2008·Granted Jan 31, 2012·49 cites·20 claims
- 0693US9273560B2Gas turbine engine component with multi-lobed cooling holeGLEINER MATTHEW S·Filed 2012·Granted Mar 1, 2016·19 cites·15 claims
- 0793US8763402B2Multi-lobed cooling hole and method of manufactureXU JINQUAN·Filed 2012·Granted Jul 1, 2014·16 cites·22 claims
- 0893US8584470B2Tri-lobed cooling hole and method of manufactureZELESKY MARK F·Filed 2012·Granted Nov 19, 2013·15 cites·23 claims
- 0993US6547524B2Film cooled article with improved temperature toleranceUNITED TECHNOLOGIES CORP·Filed 2001·Granted Apr 15, 2003·63 cites·14 claims
- 1089US11459898B2Airfoil cooling holesRAYTHEON TECH CORP·Filed 2021·Granted Oct 4, 2022·3 cites·20 claims
- 1184US9482100B2Multi-lobed cooling holeUNITED TECHNOLOGIES CORP·Filed 2012·Granted Nov 1, 2016·8 cites·20 claims
- 1284US8689568B2Cooling hole with thermo-mechanical fatigue resistanceKOHLI ATUL·Filed 2012·Granted Apr 8, 2014·11 cites·21 claims
- 1383US10711618B2Turbine component with tip film cooling and method of coolingUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 14, 2020·3 cites·20 claims
- 1482US10670275B2Cooling configurations for combustor attachment featuresUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 2, 2020·3 cites·15 claims
- 1582US10280841B2Baffle insert for a gas turbine engine component and method of coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 7, 2019·3 cites·20 claims
- 1681US10690346B2Washer for combustor assemblyUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 23, 2020·3 cites·5 claims
- 1779US8695683B2Cast features for a turbine engine airfoilALBERT JASON EDWARD·Filed 2011·Granted Apr 15, 2014·6 cites·5 claims
- 1877US10337334B2Gas turbine engine component with a baffle insertUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 2, 2019·2 cites·20 claims
- 1976US10731474B2Airfoil with varying wall thicknessUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 4, 2020·3 cites·16 claims
- 2076US10605094B2Internal cooling cavity with trip stripsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 31, 2020·2 cites·15 claims
- 2176US10494939B2Air shredder insertUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 3, 2019·2 cites·18 claims
- 2273US10422233B2Baffle insert for a gas turbine engine component and component with baffle insertUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 24, 2019·2 cites·20 claims
- 2371US8955576B2Cast features for a turbine engine airfoilUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 17, 2015·2 cites·4 claims
- 2470US7980819B2Cast features for a turbine engine airfoilUNITED TECHNOLOGIES CORP·Filed 2007·Granted Jul 19, 2011·9 cites·4 claims
- 2570US7883320B2Article having diffuser holes and method of making sameUNITED TECHNOLOGIES CORP·Filed 2005·Granted Feb 8, 2011·10 cites·7 claims
- 2668US10619489B2Airfoil having end wall contoured pedestalsUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 14, 2020·1 cites·12 claims
- 2767US10577947B2Baffle insert for a gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 3, 2020·1 cites·20 claims
- 2863US11078793B2Gas turbine engine airfoil with large thickness propertiesRAYTHEON TECH CORP·Filed 2019·Granted Aug 3, 2021·0 cites·20 claims
- 2961US10947854B2Internal cooling cavity with trip stripsUNITED TECHNOLOGIES CORP·Filed 2020·Granted Mar 16, 2021·0 cites·17 claims
- 3055US7845907B2Blade cooling passage for a turbine engineUNITED TECHNOLOGIES CORP·Filed 2007·Granted Dec 7, 2010·4 cites·5 claims
- 3153US6932572B2Film cooled article with improved temperature toleranceUNITED TECHNOLOGIES CORP·Filed 2003·Granted Aug 23, 2005·11 cites·2 claims
- 3250US10458252B2Cooling passages for a gas path component of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 29, 2019·0 cites·19 claims
- 3347US2018347919A1Pressure equalizing orifice for baffles in vanesUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 3447US2016222794A1Incidence tolerant engine componentUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 3545US11286787B2Gas turbine engine airfoil with showerhead cooling holes near leading edgeUNITED TECHNOLOGIES CORP·Filed 2016·Granted Mar 29, 2022·0 cites·3 claims
- 3645US2011132876A1Article having diffuser holes and method of making sameUNITED TECHNOLOGIES CORP·Filed 2011·Application pending·0 cites
- 3744US2017022839A1Gas turbine engine component mateface surfacesUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 3843US2019078786A1Cooling configurations for combustor attachment featuresUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 3938US2008003096A1High coverage cooling hole shapeUNITED TECHNOLOGIES CORP·Filed 2006·Application pending·0 cites
- 4037US2016047251A1Cooling hole having unique meter portionUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 4133US2007009358A1Cooled airfoil with reduced internal turn lossesKOHLI ATUL·Filed 2005·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →