James Page Strohl
13Patents
6h-index
20Co-inventors
62Inventor score
Filing activity: Nov 19, 2008 → Jul 1, 2019
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8573945B2 | Compressor stator vane | Mechanical Engineering; Lighting; Heating | 45 | Active |
| US8206095B2 | Compound variable elliptical airfoil fillet | Emerging Cross-Sectional Technologies | 14 | Active |
| US8573942B2 | Axial retention of a platform seal | Mechanical Engineering; Lighting; Heating | 12 | Active |
| US8066482B2 | Shaped cooling holes for reduced stress | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US8287241B2 | Turbine blade platform trailing edge undercut | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US8511982B2 | Compressor vane diaphragm | Emerging Cross-Sectional Technologies | 9 | Active |
| US8142137B2 | Cooled gas turbine vane assembly | Emerging Cross-Sectional Technologies | 5 | Active |
| US11131200B2 | Method and apparatus for improving turbine blade sealing in a gas turbine engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10590772B1 | Second stage turbine blade | Emerging Cross-Sectional Technologies | 1 | Active |
| US10167724B2 | Turbine blade platform undercut with decreasing radii curve | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11339458B2 | Nickel-base alloy for gas turbine components | Chemistry; Metallurgy | 0 | Active |
| US11060949B2 | Systems and methods for modal testing of turbine blades | Physics | 0 | Active |
| US11339668B2 | Method and apparatus for improving cooling of a turbine shroud | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.