Inventor · disambiguated record
James P. Bangerter
Also filed as: BANGERTER JAMES P
16 granted patents·2 pending applications·62 citations·filing 2012–2018
91Inventor score
Top patents by PatentIndex Score
18 records- 0191US9945295B2Composite piston ring seal for axially and circumferentially translating ductsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 17, 2018·6 cites·16 claims
- 0288US9995157B2Gas turbine engine turbine vane platform coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 12, 2018·6 cites·15 claims
- 0388US9010122B2Turbine engine combustor and stator vane assemblyBANGERTER JAMES P·Filed 2012·Granted Apr 21, 2015·16 cites·18 claims
- 0486US10087884B2Stepped fairing modulated exhaust coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 2, 2018·4 cites·9 claims
- 0586US9194585B2Cooling for combustor liners with accelerating channelsUNITED TECHNOLOGIES CORP·Filed 2012·Granted Nov 24, 2015·10 cites·20 claims
- 0685US10317080B2Co-swirl orientation of combustor effusion passages for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 11, 2019·9 cites·7 claims
- 0770US10309314B2Finned ignitor grommet for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 4, 2019·3 cites·17 claims
- 0866US9511388B2Method and system for holding a combustor panel during coating processUNITED TECHNOLOGIES CORP·Filed 2012·Granted Dec 6, 2016·2 cites·12 claims
- 0965US10634351B2Combustor panel T-junction coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 28, 2020·2 cites·13 claims
- 1064US10371089B2System for actuating an exhaust cowlUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·1 cites·16 claims
- 1162US10107497B2Gas turbine engine combustor linerBANGERTER JAMES P·Filed 2012·Granted Oct 23, 2018·2 cites·17 claims
- 1260US10760500B2Composite piston ring seal for axially and circumferentially translating ductsUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 1, 2020·0 cites·19 claims
- 1358US10088162B2Combustor with grommet having projecting lipUNITED TECHNOLOGIES CORP·Filed 2013·Granted Oct 2, 2018·1 cites·23 claims
- 1455US10197285B2Gas turbine engine wall assembly interfaceUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 5, 2019·0 cites·20 claims
- 1553US10655855B2Gas turbine engine wall assembly with support shell contour regionsUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 19, 2020·0 cites·20 claims
- 1649US10808937B2Gas turbine engine wall assembly with offset railUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 20, 2020·0 cites·11 claims
- 1749US2016169515A1Edge cooling for combustor panelsUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1835US2016160652A1Cooled pocket in a turbine vane platformUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →