Charles Thistle
14Patents
2h-index
15Co-inventors
40Inventor score
Filing activity: Jan 22, 2016 → Dec 6, 2019
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10677073B2 | Blade platform with damper restraint | Emerging Cross-Sectional Technologies | 5 | Active |
| US10519782B2 | Airfoil having serpentine core resupply flow control | Emerging Cross-Sectional Technologies | 3 | Active |
| US11377967B2 | Pre-formed faceted turbine blade damper seal | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10731479B2 | Blade platform with damper restraint | Emerging Cross-Sectional Technologies | 2 | Active |
| US10047611B2 | Turbine blade attachment curved rib stiffeners | Emerging Cross-Sectional Technologies | 2 | Active |
| US10724386B2 | Blade platform with damper restraint | Emerging Cross-Sectional Technologies | 1 | Active |
| US10662784B2 | Damper with varying thickness for a blade | Emerging Cross-Sectional Technologies | 1 | Active |
| US10822959B2 | Blade tip cooling | Emerging Cross-Sectional Technologies | 0 | Active |
| US10077665B2 | Turbine blade attachment rails for attachment fillet stress reduction | Emerging Cross-Sectional Technologies | 0 | Active |
| US10533431B2 | Blade platform with damper restraint | General | 0 | Revoked |
| US10533430B2 | Damper with varying thickness for a blade | General | 0 | Revoked |
| US10570749B2 | Gas turbine blade with pedestal array | Emerging Cross-Sectional Technologies | 0 | Active |
| US10612394B2 | Airfoil having serpentine core resupply flow control | Emerging Cross-Sectional Technologies | 0 | Active |
| US10815792B2 | Gas turbine engine component with a cooling circuit having a flared base | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.