James B. Hoke
51Patents
11h-index
62Co-inventors
81Inventor score
Filing activity: Dec 31, 1997 → Jun 7, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7093439B2 | Heat shield panels for use in a combustor for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 89 | Expired |
| US6240731A | Low NOx combustor for gas turbine engine | Emerging Cross-Sectional Technologies | 64 | Expired |
| US6101814A | Low emissions can combustor with dilution hole arrangement for a turbine engine | Emerging Cross-Sectional Technologies | 60 | Expired |
| US9068748B2 | Axial stage combustor for gas turbine engines | Emerging Cross-Sectional Technologies | 44 | Active |
| US7363763B2 | Combustor | Emerging Cross-Sectional Technologies | 40 | Expired |
| US6715292B1 | Coke resistant fuel injector for a low emissions combustor | Mechanical Engineering; Lighting; Heating | 38 | Expired |
| US7954325B2 | Gas turbine combustor | Emerging Cross-Sectional Technologies | 37 | Active |
| US8443610B2 | Low emission gas turbine combustor | Emerging Cross-Sectional Technologies | 26 | Active |
| US8015829B2 | Combustor | Emerging Cross-Sectional Technologies | 23 | Active |
| US7007864B2 | Fuel nozzle design | Mechanical Engineering; Lighting; Heating | 23 | Expired |
| US9400104B2 | Flow modifier for combustor fuel nozzle tip | Mechanical Engineering; Lighting; Heating | 12 | Active |
| US8479521B2 | Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assemblies | Emerging Cross-Sectional Technologies | 7 | Active |
| US10598382B2 | Impingement film-cooled floatwall with backside feature | Emerging Cross-Sectional Technologies | 7 | Active |
| US9416970B2 | Combustor heat panel arrangement having holes offset from seams of a radially opposing heat panel | Emerging Cross-Sectional Technologies | 7 | Active |
| US9052111B2 | Turbine engine combustor wall with non-uniform distribution of effusion apertures | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US10215411B2 | Combustor panels having recessed rail | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US9625151B2 | Cooled combustor liner grommet | Emerging Cross-Sectional Technologies | 6 | Active |
| US10317080B2 | Co-swirl orientation of combustor effusion passages for gas turbine engine combustor | Emerging Cross-Sectional Technologies | 5 | Active |
| US9322554B2 | Temperature mixing enhancement with locally co-swirling quench jet pattern for gas turbine engine combustor | Emerging Cross-Sectional Technologies | 5 | Active |
| US9797601B2 | Bluff body fuel mixer | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US8789374B2 | Gas turbine combustor with liner air admission holes associated with interpersed main and pilot swirler assemblies | Emerging Cross-Sectional Technologies | 4 | Active |
| US9958162B2 | Combustor assembly for a turbine engine | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US8028528B2 | Annular gas turbine combustor | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US11199326B2 | Combustor panel | Emerging Cross-Sectional Technologies | 4 | Active |
| US10309314B2 | Finned ignitor grommet for a gas turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.