Clayton Stuart Cooper
63Patents
5h-index
52Co-inventors
75Inventor score
Filing activity: Oct 29, 2002 → Jul 8, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6851263B2 | Liner for a gas turbine engine combustor having trapped vortex cavity | Mechanical Engineering; Lighting; Heating | 29 | Expired |
| US10935245B2 | Annular concentric fuel nozzle assembly with annular depression and radial inlet ports | Emerging Cross-Sectional Technologies | 6 | Active |
| US10823422B2 | Tangential bulk swirl air in a trapped vortex combustor for a gas turbine engine | Emerging Cross-Sectional Technologies | 6 | Active |
| US10724739B2 | Combustor acoustic damping structure | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US10976053B2 | Involute trapped vortex combustor assembly | Emerging Cross-Sectional Technologies | 5 | Active |
| US11156361B2 | Multi-point injection mini mixing fuel nozzle assembly | Emerging Cross-Sectional Technologies | 4 | Active |
| US11473780B2 | Engine with rotating detonation combustion system | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US10393382B2 | Multi-point injection mini mixing fuel nozzle assembly | Emerging Cross-Sectional Technologies | 4 | Active |
| US11280495B2 | Gas turbine combustor fuel injector flow device including vanes | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US11286884B2 | Combustion section and fuel injector assembly for a heat engine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10520195B2 | Effervescent atomizing structure and method of operation for rotating detonation propulsion system | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10890327B2 | Liner of a gas turbine engine combustor including dilution holes with airflow features | Emerging Cross-Sectional Technologies | 2 | Active |
| US11320147B2 | Engine with rotating detonation combustion system | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10976052B2 | Volute trapped vortex combustor assembly | Emerging Cross-Sectional Technologies | 2 | Active |
| US10641169B2 | Hybrid combustor assembly and method of operation | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11674476B2 | Multiple chamber rotating detonation combustor | Mechanical Engineering; Lighting; Heating | 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 |
| 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 |
| US11428411B1 | Swirler with rifled venturi for dynamics mitigation | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11598526B2 | Combustor swirl vane apparatus | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10837643B2 | Mixer assembly for a combustor | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10495001B2 | Combustion section heat transfer system for a propulsion system | Emerging Cross-Sectional Technologies | 1 | Active |
| US11649966B1 | Combustor with an ignition tube | Mechanical Engineering; Lighting; Heating | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.