Inventor · disambiguated record
James B. Hoke
Also filed as: HOKE JAMES · HOKE JAMES B
51 granted patents·9 pending applications·799 citations·filing 1997–2024
98Inventor score
Top patents by PatentIndex Score
60 records- 0198US9068748B2Axial stage combustor for gas turbine enginesHOKE JAMES B·Filed 2011·Granted Jun 30, 2015·51 cites·15 claims
- 0296US7093439B2Heat shield panels for use in a combustor for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2002·Granted Aug 22, 2006·148 cites·54 claims
- 0393US7954325B2Gas turbine combustorUNITED TECHNOLOGIES CORP·Filed 2005·Granted Jun 7, 2011·43 cites·13 claims
- 0493US6101814ALow emissions can combustor with dilution hole arrangement for a turbine engineUNITED TECHNOLOGIES CORP·Filed 1999·Granted Aug 15, 2000·114 cites·12 claims
- 0592US10215411B2Combustor panels having recessed railUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 26, 2019·7 cites·12 claims
- 0692US9797601B2Bluff body fuel mixerUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 24, 2017·6 cites·16 claims
- 0791US10598382B2Impingement film-cooled floatwall with backside featureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 24, 2020·7 cites·8 claims
- 0890US9400104B2Flow modifier for combustor fuel nozzle tipLOW KEVIN JOSEPH·Filed 2012·Granted Jul 26, 2016·20 cites·27 claims
- 0990US7363763B2CombustorUNITED TECHNOLOGIES CORP·Filed 2003·Granted Apr 29, 2008·67 cites·17 claims
- 1089US11029027B2Dilution/effusion hole pattern for thick combustor panelsUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jun 8, 2021·5 cites·17 claims
- 1189US8443610B2Low emission gas turbine combustorHOKE JAMES B·Filed 2009·Granted May 21, 2013·26 cites·23 claims
- 1289US8015829B2CombustorUNITED TECHNOLOGIES CORP·Filed 2008·Granted Sep 13, 2011·23 cites·19 claims
- 1389US6715292B1Coke resistant fuel injector for a low emissions combustorUNITED TECHNOLOGIES CORP·Filed 1999·Granted Apr 6, 2004·60 cites·6 claims
- 1489US6240731B1Low NOx combustor for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1997·Granted Jun 5, 2001·81 cites·6 claims
- 1586US8479521B2Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assembliesHOKE JAMES B·Filed 2011·Granted Jul 9, 2013·9 cites·12 claims
- 1685US10317080B2Co-swirl orientation of combustor effusion passages for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 11, 2019·9 cites·7 claims
- 1785US10077903B2Hybrid through holes and angled holes for combustor grommet coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 18, 2018·4 cites·10 claims
- 1885US8789374B2Gas turbine combustor with liner air admission holes associated with interpersed main and pilot swirler assembliesUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jul 29, 2014·7 cites·6 claims
- 1984US12359810B2Extended bulkhead panelRTX CORP·Filed 2024·Granted Jul 15, 2025·0 cites·8 claims
- 2084US11199326B2Combustor panelUNITED TECHNOLOGIES CORP·Filed 2019·Granted Dec 14, 2021·5 cites·11 claims
- 2184US9625151B2Cooled combustor liner grommetUNITED TECHNOLOGIES CORP·Filed 2012·Granted Apr 18, 2017·9 cites·7 claims
- 2284US9052111B2Turbine engine combustor wall with non-uniform distribution of effusion aperturesERBAS-SEN NURHAK·Filed 2012·Granted Jun 9, 2015·11 cites·14 claims
- 2383US11236906B2Combustor cooled quench zone arrayUNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 1, 2022·2 cites·16 claims
- 2482US10670275B2Cooling configurations for combustor attachment featuresUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 2, 2020·3 cites·15 claims
- 2581US10690346B2Washer for combustor assemblyUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 23, 2020·3 cites·5 claims
- 2681US9322554B2Temperature mixing enhancement with locally co-swirling quench jet pattern for gas turbine engine combustorKIM WON-WOOK·Filed 2011·Granted Apr 26, 2016·8 cites·29 claims
- 2776US12038175B2Extended bulkhead panelRAYTHEON TECH CORP·Filed 2022·Granted Jul 16, 2024·0 cites·5 claims
- 2875US11391460B2Effusion cooling for dilution/quench hole edges in combustor liner panelsUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jul 19, 2022·1 cites·16 claims
- 2975US9958162B2Combustor assembly for a turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 1, 2018·4 cites·4 claims
- 3074US10088159B2Active cooling of grommet bosses for a combustor panel of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 2, 2018·4 cites·15 claims
- 3172US10563584B2Float wall combustor panels having airflow distribution featuresUNITED TECHNOLOGIES CORP·Filed 2017·Granted Feb 18, 2020·2 cites·13 claims
- 3270US11143407B2Combustor with axial staging for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 12, 2021·3 cites·20 claims
- 3370US10309314B2Finned ignitor grommet for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 4, 2019·3 cites·17 claims
- 3469US11525577B2Extended bulkhead panelRAYTHEON TECH CORP·Filed 2020·Granted Dec 13, 2022·0 cites·10 claims
- 3569US7007864B2Fuel nozzle designUNITED TECHNOLOGIES CORP·Filed 2002·Granted Mar 7, 2006·30 cites·11 claims
- 3668US10670274B2Cooling configurations for combustor attachment featuresUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 2, 2020·1 cites·15 claims
- 3767US12135129B2Effusion cooling for dilution/quench hole edges in combustor liner panelsRAYTHEON TECH CORP·Filed 2022·Granted Nov 5, 2024·0 cites·12 claims
- 3866US10240533B2Fuel distribution within a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2013·Granted Mar 26, 2019·2 cites·13 claims
- 3963US9631560B2Fuel-air mixture distribution for gas turbine engine combustorsHOKE JAMES B·Filed 2011·Granted Apr 25, 2017·2 cites·19 claims
- 4062US10816209B2Bluff body fuel mixerUNITED TECHNOLOGIES CORP·Filed 2017·Granted Oct 27, 2020·0 cites·9 claims
- 4162US8028528B2Annular gas turbine combustorUNITED TECHNOLOGIES CORP·Filed 2005·Granted Oct 4, 2011·6 cites·14 claims
- 4261US2020025376A1Gas turbine engine combustor with tailored temperature profileUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 4360US10844790B2Fuel distribution within a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2019·Granted Nov 24, 2020·0 cites·18 claims
- 4459US9416970B2Combustor heat panel arrangement having holes offset from seams of a radially opposing heat panelKIRSOPP PHILIP J·Filed 2009·Granted Aug 16, 2016·10 cites·21 claims
- 4559US8671692B2Annular gas turbine combustor including converging and diverging segmentsBURD STEVEN W·Filed 2011·Granted Mar 18, 2014·1 cites·14 claims
- 4658US10317081B2Fuel injector assemblyHOKE JAMES B·Filed 2011·Granted Jun 11, 2019·1 cites·16 claims
- 4753US2015354819A1Combustor Cooled Quench Zone ArrayUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
- 4852US10260748B2Gas turbine engine combustor with tailored temperature profileUNITED TECHNOLOGIES CORP·Filed 2012·Granted Apr 16, 2019·0 cites·1 claims
- 4949US11112115B2Contoured dilution passages for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 7, 2021·0 cites·14 claims
- 5049US2016169515A1Edge cooling for combustor panelsUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
Showing the top 50 of 60 patent records by PatentIndex Score.
Join the waitlist — get patent alerts
Get an alert when James B. Hoke files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →