Inventor
LEBEAULT EVA JULIE
FR13 patents
Patents
13 patentsUS12215607B1Feb 4, 2025
Unducted turbine engine comprising stator blades having different chords
SAFRAN AIRCRAFT ENGINES2 citations71
US11661860B2May 30, 2023
Compressor module for turbomachine
SAFRAN AIRCRAFT ENGINES0 citations59
US11415011B2Aug 16, 2022
Stator wheel of a turbomachine comprising vanes having different chords
SAFRAN AIRCRAFT ENGINES0 citations59
US10844736B2Nov 24, 2020
Straightener vane and structural arm connected in a primary flow path
SAFRAN AIRCRAFT ENGINES1 citations57
US12570404B2Mar 10, 2026
Propulsion assembly for an aircraft comprising a stator vane integrated into an upstream part of a mounting pylon of reduced height
SAFRAN AIRCRAFT ENGINES0 citations49
US12480452B2Nov 25, 2025
Aircraft dual-flow turbine engine assembly, the assembly being equipped with incidence-controlled air discharge fins
SAFRAN AIRCRAFT ENGINES0 citations49
US12291978B2May 6, 2025
Bypass turbomachine for an aircraft
SAFRAN AIRCRAFT ENGINES0 citations49
US11905846B2Feb 20, 2024
Turbomachine polyspherical hub for variable pitch blades
SAFRAN AIRCRAFT ENGINES0 citations49
US12110842B2Oct 8, 2024
Air outlet for a nacelle for an aircraft bypass turbojet engine comprising a guiding device to favor a reverse thrust phase
SAFRAN AIRCRAFT ENGINES0 citations48
US12371152B2Jul 29, 2025
Aeronautical thruster
SAFRAN AIRCRAFT ENGINES0 citations47
US11933246B2Mar 19, 2024
Turbojet engine comprising a nacelle with an air intake to promote a reversed thrust phase
SAFRAN AIRCRAFT ENGINES0 citations47
US11492968B2Nov 8, 2022
Discharge duct of an intermediate housing hub for an aircraft turbojet engine comprising cooling channels
SAFRAN AIRCRAFT ENGINES0 citations46
US12134983B2Nov 5, 2024
Process for using an air input of a turboreactor nacelle comprising an air input lip which comprises a portion which can be moved to promote a thrust inversion phase
SAFRAN AIRCRAFT ENGINES0 citations44