Inventor · disambiguated record
François Charleux
Also filed as: CHARLEUX FRANCOIS · CHARLEUX FRANÇOIS
23 granted patents·2 pending applications·59 citations·filing 2006–2023
92Inventor score
Top patents by PatentIndex Score
25 records- 0191US8685868B2Reinforcing fibrous structure for a composite material and a part containing said structureBOUILLON ERIC·Filed 2006·Granted Apr 1, 2014·16 cites·16 claims
- 0289US8426326B2Fiber reinforcing texture for making a composite material partBOUILLON ERIC·Filed 2012·Granted Apr 23, 2013·8 cites·16 claims
- 0388US8263504B2Fiber reinforcing texture for making a composite material partBOUILLON ERIC·Filed 2007·Granted Sep 11, 2012·11 cites·16 claims
- 0485US8153539B2Reinforcing fiber texture with multiple-satin weaving for a composite material partCOUPE DOMINIQUE·Filed 2008·Granted Apr 10, 2012·10 cites·27 claims
- 0583US10612186B2Method for producing a curved honeycomb structure made from composite materialHERAKLES·Filed 2014·Granted Apr 7, 2020·6 cites·15 claims
- 0675US10995431B2Fiber structure and a composite material part incorporating such a structureSAFRAN CERAM·Filed 2018·Granted May 4, 2021·1 cites·7 claims
- 0771US12251890B2Method for producing a preform for part of a blade or propeller by winding a weave obtained by weaving to shapeSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Mar 18, 2025·0 cites·11 claims
- 0870US11261547B2Reinforcing fiber structure for composite material parts with great variation of thicknessSAFRAN CERAM·Filed 2016·Granted Mar 1, 2022·1 cites·13 claims
- 0970US10781708B2Guide vane made from composite material, comprising staggered attachment flanges for a gas turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Sep 22, 2020·2 cites·7 claims
- 1069US9309159B2Low-thickness thermostructural composite material part, and manufacture methodCHARLEUX FRANÇOIS·Filed 2010·Granted Apr 12, 2016·2 cites·7 claims
- 1166US12427741B2Propeller blade or airfoil with wound composite rootSAFRAN·Filed 2023·Granted Sep 30, 2025·0 cites·9 claims
- 1261US9784217B2Low-thickness thermostructural composite material part, and manufacture methodHERAKLES·Filed 2016·Granted Oct 10, 2017·0 cites·7 claims
- 1359US11560650B2Fiber structure and a composite material part incorporating such a structureSAFRAN CERAM·Filed 2021·Granted Jan 24, 2023·0 cites·5 claims
- 1456US11834765B2Weaving installation allowing the number of filaments in a strand to be determinedSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Dec 5, 2023·0 cites·10 claims
- 1552US12428755B2Fiber texture for a casing made of composite material with improved impact resistanceSAFRAN·Filed 2019·Granted Sep 30, 2025·0 cites·11 claims
- 1652US12270318B1Hybrid metal/composite blade with textile orientation adapted to mechanical stressesSAFRAN AIRCRAFT ENGINES·Filed 2023·Granted Apr 8, 2025·0 cites·6 claims
- 1752US10436036B2Fitted platform for a turbine engine fan, and a method of fabricating itSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 8, 2019·0 cites·9 claims
- 1849US9988750B2Method of fabricating a composite material part with improved intra-yarn densificationHERAKLES·Filed 2013·Granted Jun 5, 2018·0 cites·23 claims
- 1948US12392258B2Exterior ferrule of an intermediate housing made of composite material for an aircraft turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Aug 19, 2025·0 cites·11 claims
- 2048US11549400B2Fiber texture for a casing made of composite material with improved shear resistanceSAFRAN·Filed 2019·Granted Jan 10, 2023·0 cites·12 claims
- 2145US12480411B2Propeller blade or vane having a hollow composite rootSAFRAN AIRCRAFT ENGINES·Filed 2023·Granted Nov 25, 2025·0 cites·11 claims
- 2244US2025178294A1Method for manufacturing a part made of composite materialSAFRAN·Filed 2022·Application pending·0 cites
- 2343US11828184B2Method for manufacturing a composite platform for an aircraft turbine engine fanSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Nov 28, 2023·0 cites·9 claims
- 2438US8615877B2Method of producing a nozzle or a divergent nozzle element made of a compositeCHARLEUX FRANCOIS·Filed 2009·Granted Dec 31, 2013·2 cites·12 claims
- 2537US2024159163A1Method for manufacturing a turbomachine component made of composite material with a stiffening zoneSAFRAN·Filed 2022·Application pending·0 cites
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