Frédéric Chelin
23Patents
5h-index
24Co-inventors
65Inventor score
Filing activity: Jul 4, 2007 → Jun 13, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8434724B2 | Air outlet system for aircraft leading edge | Emerging Cross-Sectional Technologies | 12 | Active |
| US9010084B2 | Aircraft nacelle including an optimised acoustic processing system | Emerging Cross-Sectional Technologies | 11 | Active |
| US8851416B2 | Aircraft nacelle including at least one radial partition between two conducts | Emerging Cross-Sectional Technologies | 6 | Active |
| US9003810B2 | Aircraft cover including means for limiting the scoop phenomena of pneumatic type | Emerging Cross-Sectional Technologies | 6 | Active |
| US8142144B2 | Turbine engine for aircraft | Emerging Cross-Sectional Technologies | 5 | Active |
| US8991054B2 | Process for the production of a panel for the acoustic treatment incorporating the frost treatment function with hot air | Emerging Cross-Sectional Technologies | 4 | Active |
| US9003760B2 | Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle | Emerging Cross-Sectional Technologies | 4 | Active |
| US8628635B2 | Method for making a network of drainage pipes and acoustic processing panel including such a network of drainage pipes | Emerging Cross-Sectional Technologies | 3 | Active |
| US9353648B2 | Panel for the acoustic treatment comprising hot air ducts and at least one annular channel | Emerging Cross-Sectional Technologies | 3 | Active |
| US8794572B2 | Air intake of an aircraft nacelle that incorporates a reinforced lip with a defrost system by joule-effect | Performing Operations; Transporting | 3 | Active |
| US8993090B2 | Part for and method of repairing a damaged structure, in particular an airframe skin, and a repair kit for implementing it | Emerging Cross-Sectional Technologies | 3 | Active |
| US9114884B2 | Aircraft nacelle comprising a reinforced outer wall | Emerging Cross-Sectional Technologies | 2 | Active |
| US8960589B2 | Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment | Emerging Cross-Sectional Technologies | 2 | Active |
| US9719422B2 | Process for the production of an acoustic treatment panel that integrates channels juxtaposed with an alveolar structure | Emerging Cross-Sectional Technologies | 2 | Active |
| US10377503B2 | Engine assembly of an aircraft including a display unit | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9284060B2 | Aircraft nacelle including a rear frame inclined to the rear | Emerging Cross-Sectional Technologies | 1 | Active |
| US9261021B2 | Turbine engine for aircraft | Emerging Cross-Sectional Technologies | 0 | Active |
| US12012911B2 | Deflector provided with faces with different curvatures for a thrust reverser of an aircraft engine nacelle | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US8918977B2 | Process for the destruction of a blind fastener and device for its implementation | Emerging Cross-Sectional Technologies | 0 | Active |
| US12404820B2 | Aircraft nacelle equipped with at least one thrust reversal device comprising at least one longitudinal deflector configured to house a longitudinal actuator | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12247528B2 | Deflector provided with a spoiler for a thrust reverser of an aircraft engine nacelle | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US8757541B2 | Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle | Performing Operations; Transporting | 0 | Active |
| US12292015B2 | Aircraft nacelle equipped with at least one thrust reversal device comprising a downstream deflector, aircraft comprising at least one propulsion unit having such a nacelle | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.