SAFRAN NACELLES
🏢 View company profile →207Patents
206Active
207Granted
60Portfolio score
Filing activity: Jul 7, 2008 → Sep 20, 2023
Most-cited patents
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10634059B2 | Acoustic attenuation panel for a turbojet engine nacelle | Emerging Cross-Sectional Technologies | 7 | Active |
| US9448557B2 | Method and system for controlling at least one actuator of the cowlings of a turbojet engine thrust inverter | Emerging Cross-Sectional Technologies | 5 | Active |
| US10487738B2 | Front lip of a turbofan engine nacelle comprising hot-air bores upstream from acoustic panels | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US12116931B2 | Air intake for a turbojet engine nacelle | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US11427299B2 | Cell structure and acoustic attenuation device for a nacelle of an aircraft propulsion assembly | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US11142343B2 | Method of manufacturing a panel for an aircraft propulsion unit nacelle | Emerging Cross-Sectional Technologies | 3 | Active |
| US11686247B2 | Acoustic panel for a nacelle of an aircraft propulsion unit, and related manufacturing methods | Emerging Cross-Sectional Technologies | 3 | Active |
| US11614052B2 | Active toggle lock for a thrust reverser of an aircraft nacelle | Fixed Constructions | 2 | Active |
| US10767288B2 | Preform for a curved composite stiffener for an axisymmetric part such as a collar | Emerging Cross-Sectional Technologies | 2 | Active |
| US10746046B2 | Method for manufacturing a preform made of woven reinforcement fibers having a variable cross-section | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11428190B2 | Grid-type thrust reverser for turbojet engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10458363B2 | Thrust reverser for a nacelle of an aircraft turbojet engine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US12104526B2 | Aircraft part anti-icing treatment method | Emerging Cross-Sectional Technologies | 1 | Active |
| US12103694B2 | Nacelle air intake and nacelle comprising such an air intake | Emerging Cross-Sectional Technologies | 1 | Active |
| US10100780B2 | Nacelle for an aircraft turbojet engine comprising a secondary nozzle section with rotary doors | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11891185B2 | Nacelle for a propulsion assembly with a very high bypass ratio, comprising a removable and structural front internal structure | Emerging Cross-Sectional Technologies | 1 | Active |
| US10745140B2 | Locking device for pivoting cowls of a thrust reverser | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US12037941B2 | Supersonic speed attenuator of an air intake of an aircraft propulsion assembly comprising a de-icing device and de-icing method | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10654194B2 | Method for manufacturing a preform for composite materials | Emerging Cross-Sectional Technologies | 1 | Active |
| US11549462B2 | Turbojet engine nacelle including a single movable frame of a cascade thrust reverser and passages of ancillaries | Emerging Cross-Sectional Technologies | 1 | Active |
| US11994069B2 | System for cooling an aircraft turbojet engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US12092026B2 | Nacelle air intake and nacelle comprising such an air intake | Emerging Cross-Sectional Technologies | 1 | Active |
| US11840352B2 | Nacelle air intake and nacelle comprising such an air intake | Emerging Cross-Sectional Technologies | 1 | Active |
| US11492128B2 | Method for supplying electric power to an ultrasonic nacelle de-icing and anti-icing | Performing Operations; Transporting | 1 | Active |
| US11694669B2 | Method for manufacturing a cellular core for an acoustic panel | Emerging Cross-Sectional Technologies | 1 | Active |
Source: USPTO / EPO open patent data. Counts and citation impact are objective bibliographic measures.