Darryl Eng
13Patents
4h-index
28Co-inventors
56Inventor score
Filing activity: Jun 13, 2008 → Jul 16, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8814507B1 | Cooling system for three hook ring segment | Mechanical Engineering; Lighting; Heating | 44 | Active |
| US8496443B2 | Modular turbine airfoil and platform assembly with independent root teeth | Mechanical Engineering; Lighting; Heating | 16 | Active |
| US8049353B1 | Stackable generator arrangement | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US9500094B1 | Turbine with radial acting seal | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US8939727B2 | Turbine blade and non-integral platform with pin attachment | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9963996B2 | Shroud cooling system for shrouds adjacent to airfoils within gas turbine engines | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9404377B2 | Turbine blade and non-integral platform with pin attachment | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11326460B1 | Airfoil profile for a turbine nozzle | Emerging Cross-Sectional Technologies | 1 | Active |
| US11415010B1 | Turbine nozzle and gas turbine including the same | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11454119B1 | Internal core profile for a turbine nozzle airfoil | Emerging Cross-Sectional Technologies | 0 | Active |
| US11377961B1 | Internal core profile for a turbine nozzle airfoil | Emerging Cross-Sectional Technologies | 0 | Active |
| US11608754B2 | Turbine nozzle assembly and gas turbine including the same | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11591912B2 | Internal core profile for a turbine nozzle airfoil | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.