Renaud Martet
11Patents
5h-index
25Co-inventors
62Inventor score
Filing activity: Mar 29, 2007 → Mar 16, 2020
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7972107B2 | Device for cooling a turbomachine turbine casing | Emerging Cross-Sectional Technologies | 11 | Active |
| US8672635B2 | Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the first stage of a turbine | Emerging Cross-Sectional Technologies | 9 | Active |
| US8734113B2 | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fourth stage of a turbine | Emerging Cross-Sectional Technologies | 6 | Active |
| US8734096B2 | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine | Emerging Cross-Sectional Technologies | 6 | Active |
| US8734115B2 | Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the third stage of a turbine | Emerging Cross-Sectional Technologies | 6 | Active |
| US9022744B2 | Turbine engine blade | Emerging Cross-Sectional Technologies | 3 | Active |
| US11035244B2 | Aircraft turbine engine sealing module | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US8128375B2 | Turbomachine blade that is cast with a local fattening of the section of the airfoil | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9631495B2 | Cooling for the retaining dovetail of a turbomachine blade | Emerging Cross-Sectional Technologies | 1 | Active |
| US11788430B2 | Counter-rotating turbine of an aircraft turbomachine and method for the non-destructive testing of a counter-rotating turbine rotor | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11428109B2 | Turbine blade | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.