Inventor · disambiguated record
Mark F. Zelesky
Also filed as: ZELESKY MARK · ZELESKY MARK F
103 granted patents·14 pending applications·1,374 citations·filing 1992–2024
99Inventor score
Top patents by PatentIndex Score
117 records- 0199US10036258B2Gas turbine engine component having vascular engineered lattice structureUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jul 31, 2018·30 cites·19 claims
- 0298US10202863B2Seal ring for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 12, 2019·21 cites·15 claims
- 0398US9296039B2Gas turbine engine airfoil impingement coolingPROPHETER-HINCKLEY TRACY A·Filed 2012·Granted Mar 29, 2016·36 cites·2 claims
- 0498US5931638ATurbomachinery airfoil with optimized heat transferUNITED TECHNOLOGIES CORP·Filed 1997·Granted Aug 3, 1999·241 cites·17 claims
- 0597US8683813B2Multi-lobed cooling hole and method of manufactureXU JINQUAN·Filed 2012·Granted Apr 1, 2014·32 cites·28 claims
- 0696US9856793B2Intercooled cooling air with improved air flowUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jan 2, 2018·14 cites·19 claims
- 0796US9169739B2Hybrid blade outer air seal for gas turbine engineMIRONETS SERGEY·Filed 2012·Granted Oct 27, 2015·24 cites·17 claims
- 0896US9115590B2Gas turbine engine airfoil cooling circuitUNITED TECHNOLOGIES CORP·Filed 2012·Granted Aug 25, 2015·24 cites·24 claims
- 0995US11536148B2Vane arc segment with thermal insulation elementRAYTHEON TECH CORP·Filed 2020·Granted Dec 27, 2022·3 cites·15 claims
- 1095US10662781B2Gas turbine engine component having vascular engineered lattice structureUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 26, 2020·9 cites·22 claims
- 1195US9850773B2Dual walled seal assemblyUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 26, 2017·11 cites·3 claims
- 1294US10040115B2Additively manufactured casting articles for manufacturing gas turbine engine partsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 7, 2018·5 cites·17 claims
- 1394US8733111B2Cooling hole with asymmetric diffuserGLEINER MATTHEW S·Filed 2012·Granted May 27, 2014·18 cites·20 claims
- 1493US10247419B2Combustor liner panel with a multiple of heat transfer ribs for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 2, 2019·7 cites·13 claims
- 1593US10012088B2Additive manufacturing system utilizing an epitaxy process and method of operationUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 3, 2018·5 cites·20 claims
- 1693US9273560B2Gas turbine engine component with multi-lobed cooling holeGLEINER MATTHEW S·Filed 2012·Granted Mar 1, 2016·19 cites·15 claims
- 1793US8763402B2Multi-lobed cooling hole and method of manufactureXU JINQUAN·Filed 2012·Granted Jul 1, 2014·16 cites·22 claims
- 1893US8584470B2Tri-lobed cooling hole and method of manufactureZELESKY MARK F·Filed 2012·Granted Nov 19, 2013·15 cites·23 claims
- 1993US6234754B1Coolable airfoil structureUNITED TECHNOLOGIES CORP·Filed 1999·Granted May 22, 2001·117 cites·9 claims
- 2092US9957817B2Tip leakage flow directionality controlZELESKY MARK F·Filed 2013·Granted May 1, 2018·13 cites·18 claims
- 2192US9109452B2Vortex generators for improved film effectivenessMARTIN THOMAS J·Filed 2012·Granted Aug 18, 2015·18 cites·18 claims
- 2291US9851105B2Self-cooled orifice structureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 26, 2017·7 cites·20 claims
- 2390US10975723B2Gas turbine engine including seal plate providing increased cooling adjacent contact areaUNITED TECHNOLOGIES CORP·Filed 2019·Granted Apr 13, 2021·4 cites·16 claims
- 2490US10731855B2Combustor panel cooling arrangementsUNITED TECHNOLOGIES CORP·Filed 2017·Granted Aug 4, 2020·5 cites·17 claims
- 2590US10385774B2Split compressor turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 20, 2019·6 cites·21 claims
- 2689US10670273B2Cooling configurations for combustor attachment featuresUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 2, 2020·5 cites·13 claims
- 2789US10329918B2Multiple piece engine componentUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 25, 2019·5 cites·13 claims
- 2889US9777582B2Tip leakage flow directionality controlZELESKY MARK F·Filed 2013·Granted Oct 3, 2017·11 cites·21 claims
- 2989US9260972B2Tip leakage flow directionality controlZELESKY MARK F·Filed 2012·Granted Feb 16, 2016·12 cites·23 claims
- 3089US6241467B1Stator vane for a rotary machineUNITED TECHNOLOGIES CORP·Filed 1999·Granted Jun 5, 2001·101 cites·21 claims
- 3189US5271715ACooled turbine bladeUNITED TECHNOLOGIES CORP·Filed 1992·Granted Dec 21, 1993·64 cites·3 claims
- 3286US12180898B1Regulating core air bled from a turbine engine core flowpathRTX CORP·Filed 2023·Granted Dec 31, 2024·1 cites·19 claims
- 3386US10101029B2Combustor panels and configurations for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 16, 2018·4 cites·19 claims
- 3486US9963982B2Casting optimized to improve suction side cooling shaped hole performanceUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 8, 2018·4 cites·15 claims
- 3586US9091176B2Turbomachinery component cooling schemeMARTIN THOMAS J·Filed 2012·Granted Jul 28, 2015·10 cites·19 claims
- 3686US6179565B1Coolable airfoil structureUNITED TECHNOLOGIES CORP·Filed 1999·Granted Jan 30, 2001·88 cites·13 claims
- 3785US11680531B2Adaptive bleed schedule in a gas turbine engineRAYTHEON TECH CORP·Filed 2022·Granted Jun 20, 2023·1 cites·20 claims
- 3885US10006367B2Self-opening cooling passages for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 26, 2018·8 cites·11 claims
- 3984US10502067B2Dual-fed airfoil tipUNITED TECHNOLOGIES CORP·Filed 2016·Granted Dec 10, 2019·4 cites·15 claims
- 4084US8689568B2Cooling hole with thermo-mechanical fatigue resistanceKOHLI ATUL·Filed 2012·Granted Apr 8, 2014·11 cites·21 claims
- 4182US11125168B2Dirt mitigation in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 21, 2021·3 cites·20 claims
- 4282US10794214B2Tip clearance control for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2017·Granted Oct 6, 2020·3 cites·18 claims
- 4382US10422230B2Cooling hole with curved metering sectionUNITED TECHNOLOGIES CORP·Filed 2016·Granted Sep 24, 2019·3 cites·18 claims
- 4482US9024226B2EDM method for multi-lobed cooling holeLEVASSEUR GLENN·Filed 2012·Granted May 5, 2015·7 cites·22 claims
- 4582US9011087B2Hybrid airfoil for a gas turbine engineMIRONETS SERGEY·Filed 2012·Granted Apr 21, 2015·6 cites·13 claims
- 4682US7779540B2Apparatus and method for quadrail ergonomic assemblyUNITED TECHNOLOGIES CORP·Filed 2005·Granted Aug 24, 2010·26 cites·37 claims
- 4781US11608749B2Airfoil having environmental barrier topcoats that vary in composition by locationUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 21, 2023·2 cites·6 claims
- 4881US11085325B2Turbine engine cooling system with an open loop circuitUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 10, 2021·1 cites·19 claims
- 4981US10690346B2Washer for combustor assemblyUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 23, 2020·3 cites·5 claims
- 5080US11181005B2Gas turbine engine assembly with mid-vane outer platform gapUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 23, 2021·2 cites·20 claims
Showing the top 50 of 117 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →