Inventor · disambiguated record
Thomas N. Slavens
Also filed as: SLAVENS JR THOMAS N · SLAVENS THOMAS N
91 granted patents·21 pending applications·272 citations·filing 2012–2025
99Inventor score
Top patents by PatentIndex Score
112 records- 0199US10036258B2Gas turbine engine component having vascular engineered lattice structureUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jul 31, 2018·30 cites·19 claims
- 0296US9713843B2Method for additively constructing internal channelsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 25, 2017·14 cites·15 claims
- 0395US10662781B2Gas turbine engine component having vascular engineered lattice structureUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 26, 2020·9 cites·22 claims
- 0495US9988923B2Seal for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 5, 2018·24 cites·15 claims
- 0595US9932841B2Workpiece manufactured from an additive manufacturing system having a particle separator and method of operationUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 3, 2018·8 cites·14 claims
- 0695US9714580B2Trough seal for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jul 25, 2017·24 cites·18 claims
- 0794US10040115B2Additively manufactured casting articles for manufacturing gas turbine engine partsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 7, 2018·5 cites·17 claims
- 0893US10247419B2Combustor 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
- 0993US10104313B2Method for turbine component qualificationUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 16, 2018·11 cites·16 claims
- 1093US10012088B2Additive manufacturing system utilizing an epitaxy process and method of operationUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 3, 2018·5 cites·20 claims
- 1192US9109452B2Vortex generators for improved film effectivenessMARTIN THOMAS J·Filed 2012·Granted Aug 18, 2015·18 cites·18 claims
- 1290US10385774B2Split compressor turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 20, 2019·6 cites·21 claims
- 1389US11867402B2CMC stepped combustor linerRAYTHEON TECH CORP·Filed 2021·Granted Jan 9, 2024·2 cites·18 claims
- 1489US10329918B2Multiple piece engine componentUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 25, 2019·5 cites·13 claims
- 1589US10245637B2Low modulus shot sleeve for high temperature die castingUNITED TECHNOLOGIES CORP·Filed 2016·Granted Apr 2, 2019·2 cites·11 claims
- 1686US10233842B2Tangential on-board injectors for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2016·Granted Mar 19, 2019·4 cites·18 claims
- 1786US9091176B2Turbomachinery component cooling schemeMARTIN THOMAS J·Filed 2012·Granted Jul 28, 2015·10 cites·19 claims
- 1885US2025321005A1Cmc stepped combustor linerRTX CORP·Filed 2025·Application pending·0 cites
- 1983US10179362B2System and process to provide self-supporting additive manufactured ceramic coreUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jan 15, 2019·1 cites·8 claims
- 2082US10370981B2Gas turbine engine component cooling circuit with respirating pedestalUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·3 cites·12 claims
- 2182US9932835B2Airfoil cooling device and method of manufactureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 3, 2018·3 cites·18 claims
- 2281US10316668B2Gas turbine engine component having curved turbulatorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 11, 2019·9 cites·20 claims
- 2381US10247099B2Pedestals with heat transfer augmenterUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 2, 2019·6 cites·22 claims
- 2479US12359816B2CMC stepped combustor linerRTX CORP·Filed 2023·Granted Jul 15, 2025·0 cites·18 claims
- 2579US11306600B2Enhanced adhesion thermal barrier coatingRAYTHEON TECH CORP·Filed 2020·Granted Apr 19, 2022·1 cites·13 claims
- 2679US10196902B2Cooling for gas turbine engine componentsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 5, 2019·3 cites·14 claims
- 2779US10066549B2Variable vane segmentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 4, 2018·2 cites·14 claims
- 2878US10307816B2Additively manufactured core for use in casting an internal cooling circuit of a gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 4, 2019·1 cites·13 claims
- 2978US10259039B2Gas turbine engine component cooling passage and space casting coreUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 16, 2019·1 cites·5 claims
- 3077US10612392B2Gas turbine engine component with conformal fillet cooling pathUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 7, 2020·2 cites·13 claims
- 3177US10273809B2Centrifugal airfoil cooling modulationUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 30, 2019·4 cites·22 claims
- 3277US10094229B2Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operationUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 9, 2018·2 cites·14 claims
- 3376US10549338B2System and process to provide self-supporting additive manufactured ceramic coreUNITED TECHNOLOGIES CORP·Filed 2018·Granted Feb 4, 2020·0 cites·7 claims
- 3476US10156359B2Gas turbine engine component having vascular engineered lattice structureUNITED TECHNOLOGIES CORP·Filed 2013·Granted Dec 18, 2018·3 cites·17 claims
- 3575US11143034B2Multiple piece engine componentUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 12, 2021·0 cites·13 claims
- 3675US10844730B2Centrifugal airfoil cooling modulationUNITED TECHNOLOGIES CORP·Filed 2019·Granted Nov 24, 2020·1 cites·25 claims
- 3775US10247011B2Gas turbine engine component with increased cooling capacityUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 2, 2019·2 cites·20 claims
- 3875US10012090B2Airfoil cooling apparatusUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 3, 2018·2 cites·19 claims
- 3974US11022039B2Method of manufacturing conductive film holesUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jun 1, 2021·0 cites·19 claims
- 4074US10240464B2Gas turbine engine airfoil with leading edge trench and impingement coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 26, 2019·4 cites·16 claims
- 4174US9670797B2Modulated turbine vane coolingSLAVENS THOMAS N·Filed 2012·Granted Jun 6, 2017·5 cites·10 claims
- 4273US11059093B2Additively manufactured core for use in casting an internal cooling circuit of a gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jul 13, 2021·0 cites·8 claims
- 4373US10960460B2Additive manufactured mold, a method of manufacturing the mold, and a workpiece casted from the moldUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 30, 2021·1 cites·7 claims
- 4472US10683768B2Circumferential axial segmented trough sealUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 16, 2020·4 cites·9 claims
- 4571US10626730B2Enhanced cooling for blade tipUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 21, 2020·4 cites·24 claims
- 4670US9116051B2Actively cooled gas turbine sensor probe housingUNITED TECHNOLOGIES CORP·Filed 2013·Granted Aug 25, 2015·2 cites·19 claims
- 4769US11591914B2Cupped contour for gas turbine engine blade assemblyUNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 28, 2023·0 cites·16 claims
- 4869US10364041B2Twin centrifugal single spool engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jul 30, 2019·1 cites·17 claims
- 4967US10329923B2Gas turbine engine airfoil leading edge coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 25, 2019·1 cites·19 claims
- 5067US10301967B2Incident tolerant turbine vane gap flow discouragementUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 28, 2019·2 cites·17 claims
Showing the top 50 of 112 patent records by PatentIndex Score.
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