AIRCELLE
247Patents
242Active
247Granted
60Portfolio score
Filing activity: Aug 9, 2001 → Oct 11, 2016 · 87 expiring within 5 years
Most-cited patents
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7461871B2 | Latch for joining two panels of an airplane structure | Emerging Cross-Sectional Technologies | 70 | Expired |
| US9004548B2 | Device for locking an opening part of a jet engine nacelle with respect to a fixed part, and nacelle equipped with such a device | Emerging Cross-Sectional Technologies | 49 | Active |
| US8692489B2 | System for controlling an electrical device of a nacelle | Emerging Cross-Sectional Technologies | 22 | Active |
| US8793973B2 | Thrust reverser for a dual-flow turbine engine nacelle | Emerging Cross-Sectional Technologies | 18 | Active |
| US8740137B2 | Removable air intake structure for a turbofan engine nacelle | Emerging Cross-Sectional Technologies | 18 | Active |
| US8047326B2 | Method for making an acoustic absorption panel in particular for the nacelle of an aircraft engine | Emerging Cross-Sectional Technologies | 16 | Active |
| US8038184B2 | Dynamically self-locking catching device | Emerging Cross-Sectional Technologies | 16 | Active |
| US8528857B2 | Translatable jet engine thrust reverser configuration providing improved maintenance access | Emerging Cross-Sectional Technologies | 16 | Active |
| US8245815B2 | Cellular-core structure for an acoustic panel | Emerging Cross-Sectional Technologies | 16 | Active |
| US8899512B2 | Acoustic attenuation panel for aircraft for engine nacelle | Emerging Cross-Sectional Technologies | 14 | Active |
| US8240982B2 | Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone | Emerging Cross-Sectional Technologies | 14 | Active |
| US8646574B2 | Acoustic skin for an aircraft nacelle acoustic panel | Emerging Cross-Sectional Technologies | 13 | Active |
| US8907595B2 | Aircraft engine nacelle comprising a mobile cowl moved by electric motors | Emerging Cross-Sectional Technologies | 13 | Active |
| US10118710B2 | Unducted fan for an aircraft turbine engine | Emerging Cross-Sectional Technologies | 13 | Active |
| US8919668B2 | Thrust reverser having a lockable variable nozzle section | Emerging Cross-Sectional Technologies | 12 | Active |
| US9127623B2 | Thrust reverser device | Emerging Cross-Sectional Technologies | 11 | Active |
| US8333344B2 | Aircraft nacelle guidance system installation | Mechanical Engineering; Lighting; Heating | 11 | Active |
| US9145832B2 | Gas shielding device | Emerging Cross-Sectional Technologies | 10 | Active |
| US6837459B2 | Air intake for large-size nacelle with enhanced transportability | Performing Operations; Transporting | 10 | Expired |
| US8783010B2 | Cascade type thrust reverser having a pivoting door | Emerging Cross-Sectional Technologies | 9 | Active |
| US9249756B2 | Assembly for an aircraft turbojet engine comprising a thrust reversal cowl | Performing Operations; Transporting | 9 | Active |
| US8931253B2 | Double-acting telescopic linear actuator with single-motor drive system | Emerging Cross-Sectional Technologies | 9 | Active |
| US8951006B2 | Nacelle for the jet engine of an aircraft | Emerging Cross-Sectional Technologies | 9 | Active |
| US8840061B2 | Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut | Emerging Cross-Sectional Technologies | 9 | Active |
| US8959768B2 | Method for making deicing system on a nacelle panel | Emerging Cross-Sectional Technologies | 9 | Active |
Source: USPTO / EPO open patent data. Counts and citation impact are objective bibliographic measures.