SAFRAN
🏢 View company profile →328Patents
328Active
328Granted
60Portfolio score
Filing activity: Aug 2, 2012 → Jun 13, 2023
Most-cited patents
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9254897B2 | Hydrodynamic appendage such as a keel or a centerboard, and a method of fabrication | Emerging Cross-Sectional Technologies | 7 | Active |
| US9204566B2 | Composite material FADEC box support | Electricity | 6 | Active |
| US10703487B2 | Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine | Emerging Cross-Sectional Technologies | 4 | Active |
| US10180070B2 | Tooling for fastening metal reinforcement on the leading edge of a turbine engine blade, and a method using such tooling | Emerging Cross-Sectional Technologies | 4 | Active |
| US9090025B2 | Fitting including a composite material bracket and a stiffener | Emerging Cross-Sectional Technologies | 4 | Active |
| US10954169B2 | Process for manufacturing a ceramic composite material part by pressurized injection of a loaded slurry into a porous mould | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US11285638B2 | Method of fabricating a composite material part by injecting a filled slurry into a fiber texture | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10017244B2 | Method of fabricating a force transfer part having a lug made of composite material, and a part obtained by such a method | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10508559B2 | Monobloc preform and blade for turbo machine | Emerging Cross-Sectional Technologies | 3 | Active |
| US10016912B2 | Fiber structure for an axisymmetric component made of composite material with a varying diameter, and component comprising same | Emerging Cross-Sectional Technologies | 3 | Active |
| US11169042B1 | Encased pressure sensor for measuring pressure in an aircraft wheel | Physics | 3 | Active |
| US11142343B2 | Method of manufacturing a panel for an aircraft propulsion unit nacelle | Emerging Cross-Sectional Technologies | 3 | Active |
| US9284842B2 | Axisymmetric part for an aviation turbine engine rotor | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10328604B2 | Method for manufacturing a refractory part made of composite material | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10329023B2 | Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US11037314B1 | Method for the non-destructive inspection of an aeronautical part and system thereof | Physics | 2 | Active |
| US10562093B2 | Supply system for supplying a mould with molten metal, and facility and manufacturing method implementing same | Performing Operations; Transporting | 2 | Active |
| US9916651B2 | Method for characterizing a part made of a woven composite material | Emerging Cross-Sectional Technologies | 2 | Active |
| US10315367B2 | Support tooling for winding a fiber texture, a method of fabricating a fiber texture, and a method of fabricating a fiber preform for a body of revolution | Performing Operations; Transporting | 2 | Active |
| US9415863B2 | Fiber reinforcement for making an elongate mechanical part out of composite material | Emerging Cross-Sectional Technologies | 2 | Active |
| US11655761B2 | Optimized heat exchange system for a turbomachine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10427983B2 | Method for manufacturing part made of composite material | Chemistry; Metallurgy | 2 | Active |
| US10240466B2 | Fiber preform for a hollow turbine engine vane | Emerging Cross-Sectional Technologies | 2 | Active |
| US10183450B2 | Method for impregnation of a fibrous preform and device for implementation of the said method | Performing Operations; Transporting | 2 | Active |
| US11085900B2 | Multielement method and device for testing parts with ultrasound | Physics | 2 | Active |
Source: USPTO / EPO open patent data. Counts and citation impact are objective bibliographic measures.