Mustafa Dindar
14Patents
4h-index
18Co-inventors
57Inventor score
Filing activity: Jan 8, 2002 → Sep 16, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6607358B2 | Multi-component hybrid turbine blade | Emerging Cross-Sectional Technologies | 43 | Expired |
| US9181899B2 | Variable slope exhaust nozzle | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US10822100B2 | Hybrid electric propulsion system for an aircraft | Emerging Cross-Sectional Technologies | 7 | Active |
| US9995245B2 | Variable immersion lobe mixer for turbofan jet engine exhaust and method of fabricating the same | Emerging Cross-Sectional Technologies | 5 | Active |
| US10837362B2 | Inlet cowl for a turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US11873768B1 | Hydrogen fuel system for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11898495B1 | Hydrogen fuel system for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US8984890B2 | Turbofan engine mixer assembly | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9810178B2 | Exhaust nozzle with non-coplanar and/or non-axisymmetric shape | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10974813B2 | Engine nacelle for an aircraft | Emerging Cross-Sectional Technologies | 0 | Active |
| US11808161B2 | Flow control mechanism for nacelle of turbofan engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11732673B2 | Variable area exhaust nozzle system and method for control thereof | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11905884B1 | Hydrogen fuel system for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11555449B2 | Inlet cowl for a turbine engine | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.