Thomas J. Praisner
32Patents
9h-index
34Co-inventors
75Inventor score
Filing activity: Aug 18, 2004 → Jan 26, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7887297B2 | Airfoil array with an endwall protrusion and components of the array | Mechanical Engineering; Lighting; Heating | 31 | Active |
| US7251592B1 | Boundary layer transition model | Physics | 31 | Expired |
| US8105037B2 | Endwall with leading-edge hump | Mechanical Engineering; Lighting; Heating | 29 | Active |
| US8356975B2 | Gas turbine engine with non-axisymmetric surface contoured vane platform | Emerging Cross-Sectional Technologies | 13 | Active |
| US8061980B2 | Separation-resistant inlet duct for mid-turbine frames | Emerging Cross-Sectional Technologies | 11 | Active |
| US8075259B2 | Turbine vane airfoil with turning flow and axial/circumferential trailing edge configuration | Emerging Cross-Sectional Technologies | 11 | Active |
| US8511978B2 | Airfoil array with an endwall depression and components of the array | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US8016567B2 | Separation resistant aerodynamic article | Emerging Cross-Sectional Technologies | 9 | Active |
| US8424313B1 | Gas turbine engine mid turbine frame with flow turning features | Emerging Cross-Sectional Technologies | 9 | Active |
| US8561414B1 | Gas turbine engine mid turbine frame with flow turning features | Emerging Cross-Sectional Technologies | 8 | Active |
| US8366399B2 | Blade or vane with a laterally enlarged base | Mechanical Engineering; Lighting; Heating | 7 | Active |
| US7686567B2 | Airfoil embodying mixed loading conventions | Emerging Cross-Sectional Technologies | 7 | Active |
| US8517686B2 | Flow passage for gas turbine engine | Emerging Cross-Sectional Technologies | 6 | Active |
| US9175567B2 | Low loss airfoil platform trailing edge | Emerging Cross-Sectional Technologies | 6 | Active |
| US7150427B1 | Boundary layer transition model | Physics | 6 | Expired |
| US8678740B2 | Turbomachine flow path having circumferentially varying outer periphery | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US8915090B2 | Gas turbine engine mid turbine frame with flow turning features | Emerging Cross-Sectional Technologies | 4 | Active |
| US9803559B2 | Variable vane and seal arrangement | Emerging Cross-Sectional Technologies | 4 | Active |
| US10808540B2 | Case for gas turbine engine | Emerging Cross-Sectional Technologies | 3 | 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 |
| US9926806B2 | Turbomachine flow path having circumferentially varying outer periphery | Emerging Cross-Sectional Technologies | 1 | Active |
| US10508549B2 | Gas turbine engine airfoil with large thickness properties | Emerging Cross-Sectional Technologies | 1 | Active |
| US9157326B2 | Airfoil for improved flow distribution with high radial offset | Emerging Cross-Sectional Technologies | 0 | Active |
| US10294795B2 | High pitch-to-chord turbine airfoils | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.