Inventor · disambiguated record
Frédéric Jean-Bernard Pouzadoux
Also filed as: POUZADOUX FREDERIC · POUZADOUX FREDERIC JEAN-BERNARD · POUZADOUX FRÉDÉRIC JEAN-BERNARD
9 granted patents·1 pending application·35 citations·filing 2013–2021
83Inventor score
Top patents by PatentIndex Score
10 records- 0195US10844725B2Leading edge shieldSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Nov 24, 2020·22 cites·8 claims
- 0292US11686203B2Fibrous texture for turbine engine blade made of composite materialSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jun 27, 2023·3 cites·9 claims
- 0376US11105210B2Blade comprising a leading edge shield and method for producing the bladeSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 31, 2021·2 cites·19 claims
- 0469US9695695B2Turbojet fan bladeSNECMA·Filed 2013·Granted Jul 4, 2017·5 cites·5 claims
- 0565US10619486B2Blade, associated fan and turbojet engineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Apr 14, 2020·1 cites·6 claims
- 0662US10883374B2Blade comprising a folded leading edge shield and method of manufacturing the bladeSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 5, 2021·1 cites·11 claims
- 0760US10533574B2Composite blade, comprising a leading-edge reinforcement made of another materialSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 14, 2020·1 cites·10 claims
- 0849US2021372428A1Hybridization of the fibres of the fibrous reinforcement of a bladeSAFRAN AIRCRAFT ENGINES·Filed 2019·Application pending·0 cites
- 0947US11131196B2Leading edge shieldSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Sep 28, 2021·0 cites·11 claims
- 1039US10865645B2Method for manufacturing a turbomachine fan having a reduced noise level at multiple rotational frequencies of said turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Dec 15, 2020·0 cites·9 claims
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