Clement Roussille
34Patents
8h-index
52Co-inventors
74Inventor score
Filing activity: Nov 26, 2009 → Mar 28, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10378386B2 | Turbine ring assembly with support when cold and when hot | Mechanical Engineering; Lighting; Heating | 43 | Active |
| US10626745B2 | Turbine ring assembly supported by flanges | Mechanical Engineering; Lighting; Heating | 22 | Active |
| US9080454B2 | Composite material turbine engine vane, and method for manufacturing same | Emerging Cross-Sectional Technologies | 20 | Active |
| US8607454B2 | Method for producing a turbomachine blade made from a composite material | Emerging Cross-Sectional Technologies | 18 | Active |
| US9045992B2 | Turbomachine blades or vanes having complementary even/odd geometry | Emerging Cross-Sectional Technologies | 17 | Active |
| US9062562B2 | Composite material turbomachine engine blade or vane, compressor stator segment or turbine nozzle segment incorporating such vanes and method for manufacturing same | Emerging Cross-Sectional Technologies | 14 | Active |
| US9033673B2 | Turbomachine blade or vane having complementary asymmetrical geometry | Emerging Cross-Sectional Technologies | 13 | Active |
| US8846147B2 | Method for manufacturing a complexly shaped composite material part | Emerging Cross-Sectional Technologies | 9 | Active |
| US9605543B2 | Turbine engine blade made of composite material, and a method of fabricating it | Emerging Cross-Sectional Technologies | 7 | Active |
| US9506355B2 | Turbine engine blade or vane made of composite material, turbine nozzle or compressor stator incorporating such vanes and method of fabricating same | Emerging Cross-Sectional Technologies | 7 | Active |
| US10046482B2 | Method for manufacturing a turbomachine blade made of composite material | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US9790802B2 | Turbine engine rotor including blade made of composite material and having an added root | Emerging Cross-Sectional Technologies | 5 | Active |
| US10329930B2 | Turbine ring assembly with sealing | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US9157330B2 | Layout of a blisk | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10267172B2 | Rotary assembly for a turbomachine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10132171B2 | Rotor disk blade with friction-held root, rotor disk, turbomachine and associated assembly method | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9528378B2 | Composite turbomachine blade with in-built root | Emerging Cross-Sectional Technologies | 2 | Active |
| US10519786B2 | Method for manufacturing a turbine engine vane made of a composite material, resulting vane and turbine engine including same | Emerging Cross-Sectional Technologies | 2 | Active |
| US11118477B2 | Turbine ring assembly | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9194240B2 | Vibration damper comprising a peg between outer platforms of adjacent composite-material blades of a turbine engine rotor wheel | Emerging Cross-Sectional Technologies | 1 | Active |
| US9188013B2 | Turbine engine turbine blade made of a ceramic-matrix composite with recesses made by machining | Emerging Cross-Sectional Technologies | 0 | Active |
| US11828195B2 | Fibrous preform for the aerodynamic profile of a turbomachine blade | Emerging Cross-Sectional Technologies | 0 | Active |
| US12253048B2 | Fastening of an exhaust cone in a turbomachine turbine | Emerging Cross-Sectional Technologies | 0 | Active |
| US10539028B2 | Method of optimizing the profile of a composite material blade for rotor wheel of a turbine engine, and a blade having a compensated tang | Emerging Cross-Sectional Technologies | 0 | Active |
| US10724401B2 | Turbine ring assembly | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.