Inventor · disambiguated record
Fernando Gea Aguilera
Also filed as: GEA AGUILERA FERNANDO
10 granted patents·5 pending applications·19 citations·filing 2019–2023
82Inventor score
Files withSAFRAN AIRCRAFT ENGINES15
Top patents by PatentIndex Score
15 records- 0192US11560796B2Profiled structure for an aircraft or turbomachine for an aircraftSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jan 24, 2023·14 cites·6 claims
- 0286US11913405B2Turbine engine with a flow splitter having a profile with inclined serrationsSAFRAN AIRCRAFT ENGINES·Filed 2023·Granted Feb 27, 2024·1 cites·13 claims
- 0371US11859534B2Profiled structure and associated turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jan 2, 2024·1 cites·19 claims
- 0470US11629664B2Turbine engine with a flow splitter having a profile with inclined serrationsSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Apr 18, 2023·1 cites·7 claims
- 0567US11732588B2Profiled structure for an aircraft or turbomachine for an aircraftSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Aug 22, 2023·0 cites·11 claims
- 0666US11525365B2Turbomachine with serrated-profile flow-splitter noseSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 13, 2022·1 cites·17 claims
- 0765US11668196B2Profiled structure for an aircraft or turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jun 6, 2023·1 cites·20 claims
- 0854US12371152B2Aeronautical thrusterSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Jul 29, 2025·0 cites·19 claims
- 0951US2025326484A1Propulsion unit for an aircraftSAFRAN AIRCRAFT ENGINES·Filed 2022·Application pending·0 cites
- 1049US12337986B2Reduced bulk acoustic treatment panel for a turbojet engineSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jun 24, 2025·0 cites·20 claims
- 1149US2025188951A1Propulsion system for an aircraftSAFRAN AIRCRAFT ENGINES·Filed 2023·Application pending·0 cites
- 1247US12509215B2Acoustic attenuation device for an aircraft propulsion unitSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Dec 30, 2025·0 cites·16 claims
- 1347US2025197014A1Aeronautical thrusterSAFRAN AIRCRAFT ENGINES·Filed 2023·Application pending·0 cites
- 1442US2025237182A1Outlet nozzle provided with chevrons for aeronautical thrusterSAFRAN AIRCRAFT ENGINES·Filed 2022·Application pending·0 cites
- 1541US2024317386A1Aeronautical thrusterSAFRAN AIRCRAFT ENGINES·Filed 2022·Application pending·0 cites
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →