Inventor · disambiguated record
Dominique Magnaudeix
Also filed as: MAGNAUDEIX DOMINIQUE · MAGNAUDEIX DOMINIQUE MICHEL SERGE
23 granted patents·5 pending applications·53 citations·filing 2010–2022
93Inventor score
Files withSNECMA11SAFRAN AIRCRAFT ENGINES8KLEIN GILLES CHARLES CASIMIR4DAMBRINE BRUNO JACQUES GERARD1FRANCHET JEAN-MICHEL PATRICK MAURICE1
Top patents by PatentIndex Score
28 records- 0190US10166708B2Method for demoulding a composite material with an organic matrixSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jan 1, 2019·6 cites·10 claims
- 0290US9874103B2Method of making a metal reinforcing member for a blade of a turbine engineSNECMA·Filed 2013·Granted Jan 23, 2018·7 cites·10 claims
- 0390US9598966B2Metal structural reinforcement for a composite turbine engine bladeSNECMA·Filed 2013·Granted Mar 21, 2017·9 cites·11 claims
- 0489US10759122B2Method and tooling for shaping a fan casingSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Sep 1, 2020·3 cites·10 claims
- 0586US10233572B2Yarn take-up system for weaving and a method of weaving a reinforcing fiber structure for composite material partsSNECMA·Filed 2016·Granted Mar 19, 2019·4 cites·10 claims
- 0683US9963971B2Method for creating a metal reinforcement with insert for protecting a leading edge made of compositeSNECMA·Filed 2013·Granted May 8, 2018·5 cites·9 claims
- 0782US11021813B2Preform take-up in a jacquard loomSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 1, 2021·2 cites·8 claims
- 0881US8980031B2Method of fabricating a turbine engine blade out of composite materialDAMBRINE BRUNO JACQUES GERARD·Filed 2010·Granted Mar 17, 2015·5 cites·12 claims
- 0979US10786877B2Repair of an assembly comprising a main body and a reinforcementSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Sep 29, 2020·2 cites·10 claims
- 1078US9512730B2Method for manufacturing a turbine engine part by injection of resin under pressureSNECMA·Filed 2013·Granted Dec 6, 2016·3 cites·7 claims
- 1177US9328614B2Method of making a metal reinforcing pieceKLEIN GILLES CHARLES CASIMIR·Filed 2012·Granted May 3, 2016·3 cites·9 claims
- 1271US9482102B2Method of reinforcing a mechanical partKLEIN GILLES CHARLES CASIMIR·Filed 2012·Granted Nov 1, 2016·2 cites·10 claims
- 1361US11970955B2Core for high-temperature shaping of a metal part and manufacturing, regeneration and shaping processSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Apr 30, 2024·0 cites·10 claims
- 1461US9120189B2Method of making a piece of metal reinforcementFRANCHET JEAN-MICHEL PATRICK MAURICE·Filed 2011·Granted Sep 1, 2015·2 cites·20 claims
- 1554US10576578B2Method of manufacturing a leading edge shieldSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Mar 3, 2020·0 cites·16 claims
- 1654US2024399694A1Method for manufacturing a blade for an aircraft turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2022·Application pending·0 cites
- 1753US10737407B2Mold for fabricating a turbine fan casing out of composite material, and a method of closing such a moldSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 11, 2020·0 cites·11 claims
- 1847US9314834B2Device for shaping a metal sheet by die stampingKLEIN GILLES CHARLES CASIMIR·Filed 2012·Granted Apr 19, 2016·0 cites·13 claims
- 1946US9919457B2Method for producing preformsSNECMA·Filed 2013·Granted Mar 20, 2018·0 cites·5 claims
- 2046US9522486B2Method of producing tooling for resin transfer moldingSNECMA·Filed 2013·Granted Dec 20, 2016·0 cites·8 claims
- 2145US11045831B2Device for applying abradable material to a surface of a turbine engine casingSafran Aicraft Engines·Filed 2017·Granted Jun 29, 2021·0 cites·11 claims
- 2242US9199401B2Injection mold core for making a part out of composite material, the part having a closed boxSNECMA·Filed 2015·Granted Dec 1, 2015·0 cites·5 claims
- 2341US2013221570A1Method of manufacturing a composite part by injecting resin into a tool, and device comprising this toolSNECMA·Filed 2013·Application pending·0 cites
- 2441US2013180304A1"multi-effect" forming tooling for high-temperature formingLEVEQUE STEPHANE ANDRE·Filed 2011·Application pending·0 cites
- 2541US2013309096A1Method for bonding manufacturing intermediary parts, referred to as ips, to a turbomachine blade made of composite materialSNECMA·Filed 2013·Application pending·0 cites
- 2640US8732920B2Tooling and a method for hot forging pieces of sheet metalLECONTE GILBERT MICHEL MARIN·Filed 2012·Granted May 27, 2014·0 cites·5 claims
- 2738US2012317810A1Method for making a metal reinforcement for the blade of a turbine engineKLEIN GILLES CHARLES CASIMIR·Filed 2011·Application pending·0 cites
- 2829US9764392B2Device and method for localizing a position on a partSNECMA·Filed 2015·Granted Sep 19, 2017·0 cites·12 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →