Joseph Zelina
35Patents
5h-index
34Co-inventors
69Inventor score
Filing activity: Aug 18, 1998 → Feb 8, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6119459A | Elliptical axial combustor swirler | Mechanical Engineering; Lighting; Heating | 26 | Expired |
| US6286300A | Combustor with fuel preparation chambers | Emerging Cross-Sectional Technologies | 17 | Expired |
| US10502425B2 | Contoured shroud swirling pre-mix fuel injector assembly | Emerging Cross-Sectional Technologies | 13 | Active |
| US10823422B2 | Tangential bulk swirl air in a trapped vortex combustor for a gas turbine engine | Emerging Cross-Sectional Technologies | 6 | Active |
| US11578871B1 | Gas turbine engine combustor with primary and secondary fuel injectors | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US10976053B2 | Involute trapped vortex combustor assembly | Emerging Cross-Sectional Technologies | 5 | Active |
| US11473780B2 | Engine with rotating detonation combustion system | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US10520195B2 | Effervescent atomizing structure and method of operation for rotating detonation propulsion system | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10976052B2 | Volute trapped vortex combustor assembly | Emerging Cross-Sectional Technologies | 2 | Active |
| US11320147B2 | Engine with rotating detonation combustion system | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10641169B2 | Hybrid combustor assembly and method of operation | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US12173898B1 | Combustion section with a primary combustor and a set of secondary combustors | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11359578B2 | Ramjet engine with rotating detonation combustion system and method for operation | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10823418B2 | Gas turbine engine combustor comprising air inlet tubes arranged around the combustor | Emerging Cross-Sectional Technologies | 1 | Active |
| US11674476B2 | Multiple chamber rotating detonation combustor | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10495001B2 | Combustion section heat transfer system for a propulsion system | Emerging Cross-Sectional Technologies | 1 | Active |
| US11970993B2 | Engine with rotating detonation combustion system | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11073286B2 | Trapped vortex combustor and method for operating the same | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US12196422B2 | Combustor with secondary fuel nozzle in dilution fence | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12313264B2 | Coupling assembly for a turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12169068B2 | Combustor for a turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11774103B2 | Engine with rotating detonation combustion system | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11959441B2 | Engine with rotating detonation combustion system | Emerging Cross-Sectional Technologies | 0 | Active |
| US11970994B2 | Engine with rotating detonation combustion system | Emerging Cross-Sectional Technologies | 0 | Active |
| US11906168B2 | Volute trapped vortex combustor assembly | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.