Eric A. Grover
32Patents
8h-index
27Co-inventors
71Inventor score
Filing activity: Aug 18, 2004 → Jun 13, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7251592B1 | Boundary layer transition model | Physics | 31 | Expired |
| US7887297B2 | Airfoil array with an endwall protrusion and components of the array | Mechanical Engineering; Lighting; Heating | 31 | Active |
| US8105037B2 | Endwall with leading-edge hump | Mechanical Engineering; Lighting; Heating | 29 | Active |
| US8240121B2 | Retrofit dirt separator for gas turbine engine | Emerging Cross-Sectional Technologies | 18 | Active |
| US8356975B2 | Gas turbine engine with non-axisymmetric surface contoured vane platform | Emerging Cross-Sectional Technologies | 13 | Active |
| US9140128B2 | Endwall contouring | Emerging Cross-Sectional Technologies | 12 | Active |
| US8511978B2 | Airfoil array with an endwall depression and components of the array | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US10995861B2 | Cantilevered hydrostatic advanced low leakage seal | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US7686567B2 | Airfoil embodying mixed loading conventions | Emerging Cross-Sectional Technologies | 7 | Active |
| US8366399B2 | Blade or vane with a laterally enlarged base | Mechanical Engineering; Lighting; Heating | 7 | Active |
| US8517686B2 | Flow passage for gas turbine engine | Emerging Cross-Sectional Technologies | 6 | Active |
| US8678740B2 | Turbomachine flow path having circumferentially varying outer periphery | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US9212558B2 | Endwall contouring | Emerging Cross-Sectional Technologies | 3 | Active |
| US9976433B2 | Gas turbine engine with non-axisymmetric surface contoured rotor blade platform | Emerging Cross-Sectional Technologies | 3 | Active |
| US11473434B2 | Gas turbine engine airfoil | Emerging Cross-Sectional Technologies | 2 | Active |
| US9951638B2 | Shaped rim cavity wing surface | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10385728B2 | Airfoil contour for low-loss on-boarding of cooling air through an articulating spindle | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11359726B2 | Non-contact seal assembly with multiple axially spaced spring elements | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11028717B2 | Bearing assembly for gas turbine engines | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9181815B2 | Shaped rim cavity wing surface | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10982770B2 | Hydrostatic seal with extended housing | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11118471B2 | Variable area vane endwall treatments | Emerging Cross-Sectional Technologies | 1 | Active |
| US9926806B2 | Turbomachine flow path having circumferentially varying outer periphery | Emerging Cross-Sectional Technologies | 1 | Active |
| US11378187B2 | Articulating cantilevered hydrostatic seal | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10961858B2 | Hydrostatic seal with enhanced maneuver response | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.