Fathi Ahmad
33Patents
4h-index
49Co-inventors
59Inventor score
Filing activity: Aug 31, 2004 → Dec 7, 2020
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7160084B2 | Blade of a turbine | Mechanical Engineering; Lighting; Heating | 9 | Expired |
| US7416394B2 | Gas turbine and rotor blade for a turbomachine | Mechanical Engineering; Lighting; Heating | 5 | Expired |
| US8574671B2 | Method for adjusting the coolant consumption within actively cooled components, and component | Emerging Cross-Sectional Technologies | 5 | Active |
| US8075279B2 | Coated turbine blade | Emerging Cross-Sectional Technologies | 4 | Active |
| US8607455B2 | Method for the production of coated turbine moving blades and moving-blade ring for a rotor of an axial-throughflow turbine | Emerging Cross-Sectional Technologies | 4 | Active |
| US7845905B2 | Hollow turbine blade | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US8602741B2 | Turbine vane for a stationary gas turbine | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US8267659B2 | Turbine blade | Emerging Cross-Sectional Technologies | 3 | Active |
| US9238976B2 | Guide vane system for a turbomachine having segmented guide vane carriers | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9926787B2 | Coolant bridging line for a gas turbine, which coolant bridging line can be inserted into a hollow, cooled turbine blade | Emerging Cross-Sectional Technologies | 2 | Active |
| US8109712B2 | Method of producing a turbine or compressor component, and turbine or compressor component | Emerging Cross-Sectional Technologies | 2 | Active |
| US10287892B2 | Turbine blade and turbine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US8956116B2 | Cooling of a gas turbine component designed as a rotor disk or turbine blade | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11326458B2 | Aerofoil for a turbine blade | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10927675B2 | Method for maintaining a turbomachine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9745852B2 | Axial rotor portion and turbine rotor blade for a gas turbine | Emerging Cross-Sectional Technologies | 1 | Active |
| US7465150B2 | Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US8951016B2 | Rotor blade for an axial flow turbomachine and mounting for such a rotor blade | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US8545169B2 | Cooled turbine blade for a gas turbine and use of such a turbine blade | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11224926B2 | Method for producing a cavity in a blade platform; corresponding blade | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10487669B2 | Turbine blade with a central blowout at the trailing edge | Emerging Cross-Sectional Technologies | 0 | Active |
| US10662787B2 | Local two-layer thermal barrier coating | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10669857B2 | Method for producing a base body of a turbine blade | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10781703B2 | Turbine rotor blade | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10018051B2 | Gas turbine and mounting method | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.