Inventor · disambiguated record
Stanislav Kostka
Also filed as: KOSTKA JR STANISLAV · KOSTKA STANISLAV
34 granted patents·7 pending applications·92 citations·filing 2014–2020
96Inventor score
Top patents by PatentIndex Score
41 records- 0197US9976743B2Dilution hole assemblyUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 22, 2018·11 cites·19 claims
- 0291US10443848B2Grommet assembly and method of designUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 15, 2019·6 cites·20 claims
- 0391US9851105B2Self-cooled orifice structureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 26, 2017·7 cites·20 claims
- 0486US10612781B2Combustor wall aperture body with cooling circuitUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 7, 2020·4 cites·18 claims
- 0586US10598379B2Film cooled multi-walled structure with one or more indentationsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 24, 2020·7 cites·19 claims
- 0686US10174946B2Nozzle guide for a combustor of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jan 8, 2019·4 cites·20 claims
- 0786US10094287B2Gas turbine engine component with vascular cooling schemeUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 9, 2018·4 cites·25 claims
- 0884US10794595B2Stepped heat shield for a turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 6, 2020·4 cites·16 claims
- 0984US10502422B2Cooling a quench aperture body of a combustor wallUNITED TECHNOLOGIES CORP·Filed 2014·Granted Dec 10, 2019·7 cites·15 claims
- 1083US10935244B2Heat shield panels with overlap joints for a turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2018·Granted Mar 2, 2021·2 cites·10 claims
- 1182US10317079B2Cooling an aperture body of a combustor wallUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 11, 2019·6 cites·18 claims
- 1280US10352566B2Gas turbine engine combustor liner panelUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jul 16, 2019·6 cites·4 claims
- 1379US10533745B2Film cooling a combustor wall of a turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jan 14, 2020·2 cites·20 claims
- 1479US10386066B2Turbine engine multi-walled structure with cooling element(s)UNITED TECHNOLOGIES CORP·Filed 2014·Granted Aug 20, 2019·5 cites·19 claims
- 1577US9909761B2Combustor wall assembly for a turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 6, 2018·2 cites·12 claims
- 1673US10222064B2Heat shield panels with overlap joints for a turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 5, 2019·3 cites·16 claims
- 1772US10386068B2Cooling a quench aperture body of a combustor wallUNITED TECHNOLOGIES CORP·Filed 2014·Granted Aug 20, 2019·3 cites·19 claims
- 1871US10753608B2Turbine engine multi-walled structure with internal cooling element(s)UNITED TECHNOLOGIES CORP·Filed 2014·Granted Aug 25, 2020·3 cites·19 claims
- 1969US10378768B2Combustor quench aperture coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Aug 13, 2019·2 cites·18 claims
- 2067US11226098B2Film-cooled multi-walled structure with one or more indentationsUNITED TECHNOLOGIES CORP·Filed 2020·Granted Jan 18, 2022·0 cites·20 claims
- 2167US10968829B2Cooling an igniter body of a combustor wallRAYTHEON TECH CORP·Filed 2014·Granted Apr 6, 2021·2 cites·2 claims
- 2265US11193672B2Combustor quench aperture coolingRAYTHEON TECH CORP·Filed 2019·Granted Dec 7, 2021·0 cites·18 claims
- 2363US11320146B2Film cooling a combustor wall of a turbine engineUNITED TECHNOLOGIES CORP·Filed 2019·Granted May 3, 2022·0 cites·16 claims
- 2463US2020141581A1Low lump mass combustor wall with quench aperture(s)UNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2560US10697636B2Cooling a combustor heat shield proximate a quench apertureUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 30, 2020·1 cites·10 claims
- 2659US10088161B2Gas turbine engine wall assembly with circumferential rail stud architectureUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 2, 2018·1 cites·17 claims
- 2755US10451281B2Low lump mass combustor wall with quench aperture(s)UNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 22, 2019·0 cites·13 claims
- 2853US10317078B2Cooling a multi-walled structure of a turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 11, 2019·0 cites·8 claims
- 2952US10234140B2Gas turbine engine wall assembly with enhanced flow architectureUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 19, 2019·0 cites·20 claims
- 3051US10670268B2Gas turbine engine combustor liner panelUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 2, 2020·0 cites·16 claims
- 3149US11112115B2Contoured dilution passages for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 7, 2021·0 cites·14 claims
- 3249US10378773B2Turbine engine diffuser assembly with airflow mixerUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 13, 2019·0 cites·14 claims
- 3349US2016238249A1Combustor wall having cooling element(s) within a cooling cavityUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 3448US10670272B2Fuel injector guide(s) for a turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 2, 2020·0 cites·14 claims
- 3548US2016123592A1Gas turbine engine combustor liner panelUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 3648US2016201908A1Vena contracta swirling dilution passages for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 3747US2016370008A1Conductive panel surface cooling augmentation for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 3839US2016178201A1Gas turbine engine components and cooling cavitiesUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 3938US11080990B2Portable 360-degree video-based fire and smoke detector and wireless alerting systemFACTORY MUTUAL INSURANCE COMPANY·Filed 2019·Granted Aug 3, 2021·0 cites·14 claims
- 4038US10480787B2Combustor wall cooling channel formed by additive manufacturingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Nov 19, 2019·0 cites·13 claims
- 4135US2017003027A1Gas turbine engine combustor liner panel with synergistic cooling featuresUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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