Luis Tapia
14Patents
7h-index
24Co-inventors
62Inventor score
Filing activity: Aug 30, 2006 → Sep 14, 2020
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7625178B2 | High effectiveness cooled turbine blade | Emerging Cross-Sectional Technologies | 48 | Active |
| US8628293B2 | Gas turbine engine components with cooling hole trenches | Emerging Cross-Sectional Technologies | 13 | Active |
| US8529193B2 | Gas turbine engine components with improved film cooling | Emerging Cross-Sectional Technologies | 10 | Active |
| US9228440B2 | Turbine blade airfoils including showerhead film cooling systems, and methods for forming an improved showerhead film cooled airfoil of a turbine blade | Emerging Cross-Sectional Technologies | 10 | Active |
| US9650900B2 | Gas turbine engine components with film cooling holes having cylindrical to multi-lobe configurations | Emerging Cross-Sectional Technologies | 9 | Active |
| US10113433B2 | Gas turbine engine components with lateral and forward sweep film cooling holes | Emerging Cross-Sectional Technologies | 9 | Active |
| US8371814B2 | Turbine engine components | Emerging Cross-Sectional Technologies | 8 | Active |
| US10830052B2 | Gas turbine component with cooling aperture having shaped inlet and method of forming the same | Emerging Cross-Sectional Technologies | 2 | Active |
| US8444387B2 | Seal plates for directing airflow through a turbine section of an engine and turbine sections | Emerging Cross-Sectional Technologies | 2 | Active |
| US9562437B2 | Turbine blade airfoils including film cooling systems, and methods for forming an improved film cooled airfoil of a turbine blade | Emerging Cross-Sectional Technologies | 1 | Active |
| US10669862B2 | Airfoil with leading edge convective cooling system | Emerging Cross-Sectional Technologies | 1 | Active |
| US11208900B2 | Gas turbine component with cooling aperture having shaped inlet and method of forming the same | Emerging Cross-Sectional Technologies | 0 | Active |
| US9777575B2 | Turbine rotor assemblies with improved slot cavities | Emerging Cross-Sectional Technologies | 0 | Active |
| US11220918B2 | Gas turbine component with cooling aperture having shaped inlet and method of forming the same | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.