Nurhak Erbas-Sen
17Patents
6h-index
16Co-inventors
55Inventor score
Filing activity: Jun 7, 2012 → Jan 24, 2020
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9335050B2 | Gas turbine engine combustor | Mechanical Engineering; Lighting; Heating | 28 | Active |
| US9322560B2 | Combustor bulkhead assembly | Emerging Cross-Sectional Technologies | 12 | Active |
| US9243801B2 | Combustor liner with improved film cooling | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US9482432B2 | Gas turbine engine combustor with integrated combustor vane having swirler | Emerging Cross-Sectional Technologies | 9 | Active |
| US9194585B2 | Cooling for combustor liners with accelerating channels | Emerging Cross-Sectional Technologies | 8 | Active |
| US9404654B2 | Gas turbine engine combustor with integrated combustor vane | Emerging Cross-Sectional Technologies | 7 | Active |
| US9052111B2 | Turbine engine combustor wall with non-uniform distribution of effusion apertures | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US9217568B2 | Combustor liner with decreased liner cooling | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US10488046B2 | Gas turbine engine combustor bulkhead assembly | Emerging Cross-Sectional Technologies | 5 | Active |
| US9335049B2 | Combustor liner with reduced cooling dilution openings | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US10088159B2 | Active cooling of grommet bosses for a combustor panel of a gas turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
| US10047958B2 | Combustor wall with tapered cooling cavity | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9239165B2 | Combustor liner with convergent cooling channel | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10174949B2 | Gas turbine engine combustor liner assembly with convergent hyperbolic profile | Emerging Cross-Sectional Technologies | 1 | Active |
| US11326518B2 | Cooled component for a gas turbine engine | Emerging Cross-Sectional Technologies | 0 | Active |
| US9206984B2 | Combustor bulkhead assembly | General | 0 | Revoked |
| US10655855B2 | Gas turbine engine wall assembly with support shell contour regions | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.