Marc Versaevel
21Patents
3h-index
52Co-inventors
58Inventor score
Filing activity: Mar 25, 2016 → Dec 2, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10634059B2 | Acoustic attenuation panel for a turbojet engine nacelle | Emerging Cross-Sectional Technologies | 7 | Active |
| US10487738B2 | Front lip of a turbofan engine nacelle comprising hot-air bores upstream from acoustic panels | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US11686247B2 | Acoustic panel for a nacelle of an aircraft propulsion unit, and related manufacturing methods | Emerging Cross-Sectional Technologies | 3 | Active |
| US12092026B2 | Nacelle air intake and nacelle comprising such an air intake | Emerging Cross-Sectional Technologies | 1 | Active |
| US12429015B2 | Assembly for an ejection cone of an aircraft turbomachine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11401866B2 | Active device for attenuating acoustic emissions for a turbojet engine including controlled turbines | Physics | 0 | Active |
| US11608781B2 | Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air | Emerging Cross-Sectional Technologies | 0 | Active |
| US12129042B2 | Acoustic sealing element | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12180891B2 | Acoustic panel for a turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12315486B2 | Method for creating alveolar cores having open inner conical shapes | Emerging Cross-Sectional Technologies | 0 | Active |
| US11655760B2 | Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air | Emerging Cross-Sectional Technologies | 0 | Active |
| US11629644B2 | Acoustic attenuation panel comprising a front skin and a central structure | Emerging Cross-Sectional Technologies | 0 | Active |
| US10408165B2 | Device with gratings for ejecting microjets in order to reduce the jet noise of a turbine engine | Emerging Cross-Sectional Technologies | 0 | Active |
| US10995038B2 | Method for manufacturing an acoustic attenuation panel made of an oxide ceramic-matrix composite material | Emerging Cross-Sectional Technologies | 0 | Active |
| US11591960B2 | Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air | Emerging Cross-Sectional Technologies | 0 | Active |
| US10875659B2 | Acoustic attenuation structure with a plurality of attenuation degrees for a propulsion assembly of an aircraft | Emerging Cross-Sectional Technologies | 0 | Active |
| US11220346B2 | Acoustic attenuation panel for an aircraft propulsion unit and propulsion unit including such a panel | Emerging Cross-Sectional Technologies | 0 | Active |
| US12264625B2 | Acoustic attenuation panel and its manufacturing methods | Emerging Cross-Sectional Technologies | 0 | Active |
| US11542865B2 | Air inflow lip for turbojet nacelle | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12305592B2 | Method for manufacturing a structure with cellular cores for a turbojet nacelle | Emerging Cross-Sectional Technologies | 0 | Active |
| US12170077B2 | Acoustic attenuation panel for low-frequency waves | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.