Inventor · disambiguated record
Eva Julie Lebeault
Also filed as: LEBEAULT EVA JULIE
12 granted patents·3 pending applications·3 citations·filing 2018–2023
80Inventor score
Files withSAFRAN AIRCRAFT ENGINES15
Top patents by PatentIndex Score
15 records- 0188US12215607B1Unducted turbine engine comprising stator blades having different chordsSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Feb 4, 2025·2 cites·10 claims
- 0264US10844736B2Straightener vane and structural arm connected in a primary flow pathSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Nov 24, 2020·1 cites·11 claims
- 0355US11661860B2Compressor module for turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted May 30, 2023·0 cites·9 claims
- 0454US12371152B2Aeronautical thrusterSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Jul 29, 2025·0 cites·19 claims
- 0554US11415011B2Stator wheel of a turbomachine comprising vanes having different chordsSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Aug 16, 2022·0 cites·11 claims
- 0649US2025188951A1Propulsion system for an aircraftSAFRAN AIRCRAFT ENGINES·Filed 2023·Application pending·0 cites
- 0747US2025197014A1Aeronautical thrusterSAFRAN AIRCRAFT ENGINES·Filed 2023·Application pending·0 cites
- 0845US11905846B2Turbomachine polyspherical hub for variable pitch bladesSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Feb 20, 2024·0 cites·11 claims
- 0942US12480452B2Aircraft dual-flow turbine engine assembly, the assembly being equipped with incidence-controlled air discharge finsSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Nov 25, 2025·0 cites·9 claims
- 1041US2024317386A1Aeronautical thrusterSAFRAN AIRCRAFT ENGINES·Filed 2022·Application pending·0 cites
- 1140US11933246B2Turbojet engine comprising a nacelle with an air intake to promote a reversed thrust phaseSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Mar 19, 2024·0 cites·11 claims
- 1239US11492968B2Discharge duct of an intermediate housing hub for an aircraft turbojet engine comprising cooling channelsSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Nov 8, 2022·0 cites·8 claims
- 1337US12291978B2Bypass turbomachine for an aircraftSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted May 6, 2025·0 cites·2 claims
- 1437US12134983B2Process 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 phaseSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Nov 5, 2024·0 cites·7 claims
- 1537US12110842B2Air outlet for a nacelle for an aircraft bypass turbojet engine comprising a guiding device to favor a reverse thrust phaseSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Oct 8, 2024·0 cites·15 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →