Inventor · disambiguated record
Christophe Bourdeau
Also filed as: BOURDEAU CHRISTOPHE
9 granted patents·2 pending applications·45 citations·filing 2008–2024
82Inventor score
Top patents by PatentIndex Score
11 records- 0182US11200754B1Extended reality environment generationACCENTURE GLOBAL SOLUTIONS LTD·Filed 2020·Granted Dec 14, 2021·3 cites·20 claims
- 0281US11028801B2Grating for the formation of a reverse flow of an aircraft turbofan engineAIRBUS OPERATIONS SAS·Filed 2018·Granted Jun 8, 2021·5 cites·10 claims
- 0381US8434724B2Air outlet system for aircraft leading edgeCHELIN FREDERIC·Filed 2008·Granted May 7, 2013·19 cites·20 claims
- 0478US8640986B2Turbojet nacelle and method for controlling separation in a turbojet nacelleSURPLY THIERRY·Filed 2008·Granted Feb 4, 2014·18 cites·13 claims
- 0558US12012911B2Deflector provided with faces with different curvatures for a thrust reverser of an aircraft engine nacelleAIRBUS OPERATIONS SAS·Filed 2023·Granted Jun 18, 2024·0 cites·15 claims
- 0654US12247528B2Deflector provided with a spoiler for a thrust reverser of an aircraft engine nacelleAIRBUS OPERATIONS SAS·Filed 2023·Granted Mar 11, 2025·0 cites·12 claims
- 0750US12492668B2Aircraft nacelle provided with at least one thrust reversal device comprising at least one longitudinal deflector, aircraft comprising at least one propulsion assembly composed of such a nacelleAIRBUS OPERATIONS SAS·Filed 2024·Granted Dec 9, 2025·0 cites·12 claims
- 0848US12404820B2Aircraft nacelle equipped with at least one thrust reversal device comprising at least one longitudinal deflector configured to house a longitudinal actuatorAIRBUS OPERATIONS SAS·Filed 2024·Granted Sep 2, 2025·0 cites·13 claims
- 0947US12292015B2Aircraft nacelle equipped with at least one thrust reversal device comprising a downstream deflector, aircraft comprising at least one propulsion unit having such a nacelleAIRBUS OPERATIONS SAS·Filed 2024·Granted May 6, 2025·0 cites·11 claims
- 1045US2024124148A1Aircraft engine nacelle provided with a thrust reverser having a mobile ejection structureAIRBUS OPERATIONS SAS·Filed 2023·Application pending·0 cites
- 1133US2016154909A1Airframe-engine aerodynamic simulation using a mixing plane subdivided into angular sectorsAIRBUS OPERATIONS SAS·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →