Inventor · disambiguated record
Georges Jean Xavier Riou
Also filed as: RIOU GEORGES · RIOU GEORGES JEAN XAVIER
21 granted patents·226 citations·filing 1999–2021
94Inventor score
Files withSAFRAN AIRCRAFT ENGINES10SNECMA6GAUDRY FLORIAN1JULLIARD JACQUES MICHEL ALBERT1MARDJONO JACKY NOVI1
Top patents by PatentIndex Score
21 records- 0195US10280839B2Acoustic treatment panelSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted May 7, 2019·18 cites·12 claims
- 0294US11434826B2Acoustic treatment panel for a turbojet engineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Sep 6, 2022·6 cites·9 claims
- 0391US8579225B2Device for acoustic treatment of the noise emitted by a turbojetMARDJONO JACKY NOVI·Filed 2011·Granted Nov 12, 2013·27 cites·13 claims
- 0487US9546602B2Multi-layer acoustic treatment panelJULLIARD JACQUES MICHEL ALBERT·Filed 2011·Granted Jan 17, 2017·30 cites·13 claims
- 0586US9932897B2Removable acoustic panels for turbojet engine casingSNECMA·Filed 2013·Granted Apr 3, 2018·9 cites·16 claims
- 0686US8544598B2Soundproofing panel for turbomachine and turbomachine comprising such a panelGAUDRY FLORIAN·Filed 2012·Granted Oct 1, 2013·19 cites·18 claims
- 0783US11248530B2Acoustic treatment panel for a turbojet engineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Feb 15, 2022·3 cites·15 claims
- 0881US7520369B2Soundproofing panel with beads, and a method of manufactureSNECMA·Filed 2004·Granted Apr 21, 2009·24 cites·18 claims
- 0979US7891195B2Central body of a turbojet nozzleSNECMA·Filed 2007·Granted Feb 22, 2011·15 cites·18 claims
- 1077US6085865ASoundproofing panel and method of producing said panelSNECMA·Filed 1999·Granted Jul 11, 2000·55 cites·10 claims
- 1174US10502134B2Reduction of turbofan noiseSNECMA·Filed 2015·Granted Dec 10, 2019·2 cites·5 claims
- 1271US11859534B2Profiled structure and associated turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jan 2, 2024·1 cites·19 claims
- 1367US10557417B2Acoustic absorber cell for a turbojet, and an associated acoustic treatment panelSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Feb 11, 2020·1 cites·15 claims
- 1467US7661261B2Acoustic flow straightener for turbojet engine fan casingSNECMA·Filed 2008·Granted Feb 16, 2010·7 cites·11 claims
- 1564US11220346B2Acoustic attenuation panel for an aircraft propulsion unit and propulsion unit including such a panelSAFRAN NACELLES·Filed 2019·Granted Jan 11, 2022·1 cites·11 claims
- 1662US8876467B2Inner wall for a turbomachine nacelleRIOU GEORGES JEAN XAVIER·Filed 2009·Granted Nov 4, 2014·8 cites·19 claims
- 1750US10662876B2Turbomachine vane comprising an electroacoustic source with improved assembly mode, row of outlet guide vanes and turbomachine comprising such a vaneSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted May 26, 2020·0 cites·11 claims
- 1849US12337986B2Reduced bulk acoustic treatment panel for a turbojet engineSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jun 24, 2025·0 cites·20 claims
- 1945US12092033B2Integration of a fan flutter damper in an engine casingSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Sep 17, 2024·0 cites·13 claims
- 2044US11560842B2Acoustic panel and associated propulsion unitSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jan 24, 2023·0 cites·11 claims
- 2144US11143462B2Panel for heat exchange and improved noise reduction for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Oct 12, 2021·0 cites·10 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →