Patents/Inventors

Marc Versaevel

Moissy-CramayelFR30 patents

16 Patents

US126183832026
Assembly for an Exhaust Cone of an Aircraft Turbomachine
SAFRAN NACELLES
0 cites
US126001192026
Method for Manufacturing an Acoustic Panel with Oblique Cavities
SAFRAN NACELLES
0 cites
US124290152025
Assembly for an Ejection Cone of an Aircraft Turbomachine
SAFRAN NACELLES
0 cites
US123154862025
Method for Creating Alveolar Cores Having Open Inner Conical Shapes
Safran Nacelles
0 cites
US123055922025
Method for Manufacturing a Structure with Cellular Cores for a Turbojet Nacelle
Safran Nacelles
0 cites
US122646252025
Acoustic Attenuation Panel and Its Manufacturing Methods
Safran Nacelles
0 cites
US121808912024
Acoustic Panel for a Turbine Engine
SAFRAN NACELLES
0 cites
US121700772024
Acoustic Attenuation Panel for Low-frequency Waves
Safran Nacelles
0 cites
US121290422024
Acoustic Sealing Element
SAFRAN NACELLES
0 cites
US120920262024
Nacelle Air Intake and Nacelle Comprising Such an Air Intake
Safran Nacelles
0 cites
US116862472023
Acoustic Panel for a Nacelle of an Aircraft Propulsion Unit, and Related Manufacturing Methods
Safran Nacelles
0 cites
US116557602023
Air Intake of an Aircraft Turbojet Engine Nacelle Comprising Ventilation Orifices for a De-icing Flow of Hot Air
SAFRAN NACELLES
0 cites
US116296442023
Acoustic Attenuation Panel Comprising a Front Skin and a Central Structure
SAFRAN
0 cites
US116087812023
Air Intake of an Aircraft Turbojet Engine Nacelle Comprising Ventilation Orifices for a De-icing Flow of Hot Air
SAFRAN NACELLES
0 cites
US115919602023
Air Intake of an Aircraft Turbojet Engine Nacelle Comprising Ventilation Orifices for a De-icing Flow of Hot Air
SAFRAN NACELLES
0 cites
US115428652023
Air Inflow Lip for Turbojet Nacelle
Safran Nacelles
0 cites