SAFRAN CERAMICS
🏢 View company profile →110Patents
110Active
110Granted
61Portfolio score
Filing activity: Sep 14, 2012 → Jun 13, 2023
Most-cited patents
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10590803B2 | Turbine ring assembly made from ceramic matrix composite material | Mechanical Engineering; Lighting; Heating | 37 | Active |
| US10655501B2 | Turbine ring assembly without cold assembly clearance | Emerging Cross-Sectional Technologies | 35 | Active |
| US10690007B2 | Turbine ring assembly with axial retention | Mechanical Engineering; Lighting; Heating | 33 | Active |
| US10724399B2 | Turbine ring sector having an environmental barrier doped with an electrically-conductive element | Mechanical Engineering; Lighting; Heating | 22 | Active |
| US10190426B2 | Stator sector for a turbine engine, and a method of fabricating it | Emerging Cross-Sectional Technologies | 5 | Active |
| US10392696B2 | Chemical vapour infiltration apparatus having a high loading capacity | Chemistry; Metallurgy | 5 | Active |
| US10329930B2 | Turbine ring assembly with sealing | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US10612186B2 | Method for producing a curved honeycomb structure made from composite material | Textiles; Paper | 3 | Active |
| US11519361B2 | Exhaust cone with flexible fitting | Emerging Cross-Sectional Technologies | 3 | Active |
| US10906205B2 | Shaping equipment and facility for gas-phase chemical infiltration of fibrous preforms | Chemistry; Metallurgy | 3 | Active |
| US11427299B2 | Cell structure and acoustic attenuation device for a nacelle of an aircraft propulsion assembly | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10233540B2 | Device for loading porous substrates of three-dimensional shape in order to be densified by directed flow chemical vapor infiltration | Chemistry; Metallurgy | 3 | Active |
| US11512024B2 | Method for densifying porous annular substrates by chemical vapour infiltration | Emerging Cross-Sectional Technologies | 3 | Active |
| US11821387B2 | Ejection cone having a flexible aerodynamic attachment | Emerging Cross-Sectional Technologies | 2 | Active |
| US11014856B2 | Method for producing a composite part containing a ceramic matrix | Chemistry; Metallurgy | 2 | Active |
| US10132171B2 | Rotor disk blade with friction-held root, rotor disk, turbomachine and associated assembly method | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10858958B2 | Turbine ring assembly held by jaw coupling | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10994446B2 | Method for the production of a part made from a composite material | Chemistry; Metallurgy | 1 | Active |
| US11261547B2 | Reinforcing fiber structure for composite material parts with great variation of thickness | Textiles; Paper | 1 | Active |
| US10597782B2 | Device for coating one or more yarns by a vapor deposition method | Textiles; Paper | 1 | Active |
| US10995431B2 | Fiber structure and a composite material part incorporating such a structure | Textiles; Paper | 1 | Active |
| US11255203B2 | Method for injecting a loaded slurry into a fibrous texture | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10400367B2 | Part made from oxide/oxide composite material for 3-D reinforcing and method for manufacture of same | Textiles; Paper | 1 | Active |
| US11802089B2 | Method for manufacturing a part made of a composite material | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11325355B2 | Process for manufacturing a fibrous preform filled with particles | Chemistry; Metallurgy | 1 | Active |
Source: USPTO / EPO open patent data. Counts and citation impact are objective bibliographic measures.