David R. Pack
19Patents
4h-index
17Co-inventors
57Inventor score
Filing activity: Nov 14, 2001 → Sep 16, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6974308B2 | High effectiveness cooled turbine vane or blade | Emerging Cross-Sectional Technologies | 128 | Expired |
| US10378364B2 | Modified structural truss for airfoils | Emerging Cross-Sectional Technologies | 13 | Active |
| US10871074B2 | Blade/vane cooling passages | Emerging Cross-Sectional Technologies | 8 | Active |
| US9719363B2 | Segmented rim seal spacer for a gas turbine engine | Emerging Cross-Sectional Technologies | 5 | Active |
| US11149550B2 | Blade neck transition | Emerging Cross-Sectional Technologies | 4 | Active |
| US11629602B2 | Cooling schemes for airfoils for gas turbine engines | Emerging Cross-Sectional Technologies | 3 | Active |
| US11286793B2 | Airfoil with ribs having connector arms and apertures defining a cooling circuit | Emerging Cross-Sectional Technologies | 2 | Active |
| US11480059B2 | Airfoil with rib having connector arms | Emerging Cross-Sectional Technologies | 1 | Active |
| US11905849B2 | Cooling schemes for airfoils for gas turbine engines | Emerging Cross-Sectional Technologies | 1 | Active |
| US11209221B2 | Modified shaped heat exchanger inlets/outlets | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12281595B1 | Turbine blade with boomerang shaped wall cooling passages | Emerging Cross-Sectional Technologies | 0 | Active |
| US11970954B2 | Airfoil with rib having connector arms | Emerging Cross-Sectional Technologies | 0 | Active |
| US12404775B1 | Turbine blade with cooling channels | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10316671B2 | Gas turbine engine blade with variable density and wide chord tip | Emerging Cross-Sectional Technologies | 0 | Active |
| US12173618B2 | Airfoils with lobed cooling cavities | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10378453B2 | Method and assembly for reducing secondary heat in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11952911B2 | Airfoil with connecting rib | Emerging Cross-Sectional Technologies | 0 | Active |
| US12000305B2 | Airfoil with ribs defining shaped cooling channel | Emerging Cross-Sectional Technologies | 0 | Active |
| US10954799B2 | Gas turbine engine blade with variable density and wide chord tip | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.