Inventor · disambiguated record
Thierry Godon
Also filed as: GODON THIERRY · GODON THIERRY CLAUDE HENRI
24 granted patents·5 pending applications·61 citations·filing 2010–2022
94Inventor score
Files withGODON THIERRY10SAFRAN AIRCRAFT ENGINES6DAMBRINE BRUNO JACQUES GERARD4SNECMA4DAMBRINE BRUNO JACQUES GÉRARD3
Top patents by PatentIndex Score
29 records- 0191US8448837B2Method for manufacturing a one-piece annular metal part having a reinforcing insert of composite materialDAMBRINE BRUNO JACQUES GERARD·Filed 2012·Granted May 28, 2013·6 cites·11 claims
- 0285US9669570B2Process for injection moulding a composite partGODON THIERRY·Filed 2012·Granted Jun 6, 2017·7 cites·10 claims
- 0382US10137640B2Method for adhering parts and device for implementing said methodSNECMA·Filed 2014·Granted Nov 27, 2018·4 cites·13 claims
- 0481US8980031B2Method of fabricating a turbine engine blade out of composite materialDAMBRINE BRUNO JACQUES GERARD·Filed 2010·Granted Mar 17, 2015·5 cites·12 claims
- 0579US10183450B2Method for impregnation of a fibrous preform and device for implementation of the said methodSNECMA·Filed 2014·Granted Jan 22, 2019·3 cites·11 claims
- 0679US9321100B2Method for producing a metal reinforcement for a turbomachine bladeDAMBRINE BRUNO JACQUES GÉRARD·Filed 2011·Granted Apr 26, 2016·7 cites·10 claims
- 0778US9364887B2Process for manufacturing a metal part, such as turbine engine blade reinforcementGODON THIERRY·Filed 2012·Granted Jun 14, 2016·6 cites·19 claims
- 0877US9150948B2Method for manufacturing an integral rotationally symmetrical metal part including a reinforcement consisting of ceramic fibersDAMBRINE BRUNO JACQUES GERARD·Filed 2012·Granted Oct 6, 2015·2 cites·10 claims
- 0976US9296072B2Method for manufacturing a metal partDAMBRINE BRUNO JACQUES GÉRARD·Filed 2011·Granted Mar 29, 2016·3 cites·10 claims
- 1075US9539787B2Multilayer woven fibrous structure including a hollow tubular part, production method thereof and composite part comprising sameGODON THIERRY·Filed 2012·Granted Jan 10, 2017·2 cites·10 claims
- 1174US10259169B2Method of fastening structural metal reinforcement on a portion of a gas turbine blade made of composite material, and an injection mold for performing such a methodSAFRAN AIRCRAFT ENGINES·Filed 2013·Granted Apr 16, 2019·2 cites·5 claims
- 1273US9315927B2Method for producing a solid partDAMBRINE BRUNO JACQUES GÉRARD·Filed 2011·Granted Apr 19, 2016·2 cites·11 claims
- 1369US9387632B2Method and device for manufacturing a cylindrical part from composite materialVARIN FRANCK BERNARD LEON·Filed 2012·Granted Jul 12, 2016·2 cites·9 claims
- 1468US10745109B2Assembly of two parts, one of which is made of composite material, the parts being assembled together by a mechanical anchor elementSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Aug 18, 2020·1 cites·10 claims
- 1567US9346134B2Process for making a metal part such as a turbine engine blade reinforcementGODON THIERRY·Filed 2012·Granted May 24, 2016·1 cites·14 claims
- 1665US9321106B2Process for manufacturing a one-piece axisymmetric metallic part from composite fibrous structuresGODON THIERRY·Filed 2012·Granted Apr 26, 2016·2 cites·10 claims
- 1763US9199331B2Method for fabricating a single-piece part for a turbine engine by diffusion bondingGODON THIERRY·Filed 2012·Granted Dec 1, 2015·2 cites·16 claims
- 1862US9365956B2Fibrous structure for a part made of composite material having one or more archshaped portionsGODON THIERRY·Filed 2011·Granted Jun 14, 2016·2 cites·11 claims
- 1962US2017073857A1Multilayer woven fibrous structure including a hollow tubular part, production method thereof and composite part comprising sameSNECMA·Filed 2016·Application pending·0 cites
- 2060US9476309B2Method of fabricating a part and a composite solid part obtained by the methodDAMBRINE BRUNO·Filed 2011·Granted Oct 25, 2016·1 cites·10 claims
- 2154US9605364B2Method for producing a fibrous metal structure by means of weavingGODON THIERRY·Filed 2011·Granted Mar 28, 2017·1 cites·6 claims
- 2254US2025026091A1Method for manufacturing a blade, in particular a composite bladeSAFRAN AIRCRAFT ENGINES·Filed 2022·Application pending·0 cites
- 2353US2025091303A1Method for manufacturing a composite part, in particular an aeronautical composite part and associated systemSAFRAN AIRCRAFT ENGINES·Filed 2022·Application pending·0 cites
- 2451US9382647B2Fibrous structure for a part made of a composite material and having a complex shapeDAMBRINE BRUNO JACQUES GERARD·Filed 2012·Granted Jul 5, 2016·0 cites·10 claims
- 2548US9238282B2Method for manufacturing a metal partGODON THIERRY·Filed 2012·Granted Jan 19, 2016·0 cites·9 claims
- 2644US11117287B2Method of impregnating a fiber texture of hollow shapeSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Sep 14, 2021·0 cites·13 claims
- 2744US2013312261A1Method for producing a reinforced metal part, such as a reinforcement for a turbine-engine bladeGODON THIERRY·Filed 2012·Application pending·0 cites
- 2844US2014064957A1Gas turbine fan casing having a belt for fastening equipmentSNECMA·Filed 2013·Application pending·0 cites
- 2943US10836072B2Method of fabricating an impregnated fiber assemblySAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Nov 17, 2020·0 cites·13 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →