Inventor · disambiguated record
Jacques Thebault
Also filed as: THEBAULT JACQUES
31 granted patents·9 pending applications·813 citations·filing 1985–2012
98Inventor score
Top patents by PatentIndex Score
40 records- 0197US7560139B2Thermostructural composite structure with a compositional gradient, its manufacturing processSNECMA PROPULSION SOLIDE·Filed 2006·Granted Jul 14, 2009·98 cites·11 claims
- 0296US4752503AProcess for the manufacture of a composite material with refractory fibrous reinforcement and ceramic matrixEUROP PROPULSION·Filed 1985·Granted Jun 21, 1988·84 cites·9 claims
- 0394US5686144AMethod for applying an anti-oxidative coating on brake disks of a carbon-containing composite materialEUROP PROPULSION·Filed 1995·Granted Nov 11, 1997·96 cites·43 claims
- 0488US7736554B2Method of manufacturing a part out of impervious thermostructural composite materialSNECMA PROPULSION SOLIDE·Filed 2005·Granted Jun 15, 2010·16 cites·15 claims
- 0587US5622751AMethod of protecting products of composite material against oxidizing and products protected therebyEUROP PROPULSION·Filed 1996·Granted Apr 22, 1997·72 cites·15 claims
- 0686US8084079B2Method for chemical infiltration in the gas phase for the densification of porous substrates with pyrolytic carbonTHEBAULT JACQUES·Filed 2006·Granted Dec 27, 2011·10 cites·19 claims
- 0786US6740408B2Protecting composite material parts against oxidationSNECMA PROPULSION SOLIDE·Filed 2002·Granted May 25, 2004·32 cites·23 claims
- 0884US5026604AComposite material with refractory fibrous reinforcement and ceramic matrixEUROP PROPULSION·Filed 1988·Granted Jun 25, 1991·43 cites·6 claims
- 0982US5217755AChemical vapor infiltration method utilizing substantially diffusive conditionsEUROP PROPULSION·Filed 1991·Granted Jun 8, 1993·37 cites·6 claims
- 1079US6001419AChemical vapor infiltration method with variable infiltration parametersSNECMA·Filed 1996·Granted Dec 14, 1999·43 cites·8 claims
- 1177US5134020AComposite material with multiple interphases between refractory reinforcing fibers and ceramix matrixEUROP PROPULSION·Filed 1990·Granted Jul 28, 1992·33 cites·11 claims
- 1276US5714244AMethod for protecting a porous carbon-containing material from oxidation, and material obtained therebyEUROP PROPULSION·Filed 1995·Granted Feb 3, 1998·48 cites·29 claims
- 1375US8261891B2Method of siliciding thermostructural composite materials, and parts obtained by the methodTHEBAULT JACQUES·Filed 2009·Granted Sep 11, 2012·4 cites·10 claims
- 1474US6410088B1CVI (chemical vapor infiltration) densification of porous structuresSNECMA·Filed 1999·Granted Jun 25, 2002·31 cites·23 claims
- 1574US5332619AProcess for anti-oxidation protection of a material of which at least a surface is made of a ceramic formed from a silicon compound, and a material obtained by said processEUROP PROPULSION·Filed 1992·Granted Jul 26, 1994·27 cites·11 claims
- 1673US4748079AComposite materials constituted by a matrix in resin coke carbon, reinforced with pyrolytic carbon-coated refractory fibersEUROP PROPULSION·Filed 1985·Granted May 31, 1988·26 cites·4 claims
- 1770US7063886B2Thermostructural composite structure with a compositional gradient and its manufacturing processSNECMA PROPULSION SOLIDE·Filed 2003·Granted Jun 20, 2006·8 cites·12 claims
- 1870US5853821AMethod of protecting a part made of a carbon-containing composite material against oxidationEUROP PROPULSION·Filed 1997·Granted Dec 29, 1998·28 cites·14 claims
- 1969US9340460B2Ultra-refractory material that is stable in a wet environment, and process for manufacturing sameCOURCOT MENDEZ EMILIE·Filed 2012·Granted May 17, 2016·4 cites·11 claims
- 2066US7497918B2Method of siliciding thermostructural composite materials, and parts obtained by the methodSNECMA PROPULSION SOLIDE·Filed 2004·Granted Mar 3, 2009·7 cites·26 claims
- 2164US6616756B2Protection for a carbon material, in particular C/C composite, bowl that is to receive a crucible, such as a silica crucible for drawing siliconSNECMA MOTEURS·Filed 2001·Granted Sep 9, 2003·4 cites·21 claims
- 2262US6926925B2Method of making a continuous coating on the surface of a partSNECMA PROPULSION SOLIDE·Filed 2002·Granted Aug 9, 2005·7 cites·24 claims
- 2359US9382164B2Materials and parts that can withstand high temperatures in an oxidizing medium, and method for manufacturing sameANDREANI ANNE-SOPHIE·Filed 2011·Granted Jul 5, 2016·2 cites·20 claims
- 2458US5132169AComposite materials having multidirectional reinforcement textures made essentially of ceramic fibers having a silicon compound baseEUROP PROPULSION·Filed 1991·Granted Jul 21, 1992·11 cites·3 claims
- 2555US5411762AMethod of obtaining a sialon-based ceramic material by reducing an aluminosilicate material, and use thereof in forming a ceramic coating on a refractory substrateEUROP PROPULSION·Filed 1994·Granted May 2, 1995·13 cites·17 claims
- 2654US8357423B2Method for making a refractory carbide layer on a part made of C/C composite materialSNECMA PROPULSION SOLIDE·Filed 2008·Granted Jan 22, 2013·1 cites·9 claims
- 2750US2008190552A1Method For Soldering Composite Material PartsBOUILLON ERIC·Filed 2005·Application pending·0 cites
- 2848US2009110877A1Method and substrate for making composite material parts by chemical vapour infiltration densification and resulting partsSNECMA PROPULSION SOLIDE·Filed 2006·Application pending·0 cites
- 2947US5128117AProcess for the manufacture of multidirectional reinforcement textures made essentially of ceramic fibers having a silicon compound base for the manufacture of composite materialsEUROP PROPULSION·Filed 1989·Granted Jul 7, 1992·8 cites·6 claims
- 3047US2006006212A1Method of brazing composite material parts sealed with a silicon-based compositionTHEBAULT JACQUES·Filed 2005·Application pending·0 cites
- 3145US6413585B1Thermochemical treatment, in halogenated atmosphere, of a carbon-containing materialSNECMA·Filed 1997·Granted Jul 2, 2002·10 cites·11 claims
- 3241US2006141154A1Method for treating the surface of a part made of a heat-structured composite material and use thereof in brazing parts made of a heat-structured composite materialTHEBAULT JACQUES·Filed 2004·Application pending·0 cites
- 3338US2004194941A1Active cooling panel of thermostructural composite material and method for its manufactureSNECMA PROPULSION SOLIDE·Filed 2004·Application pending·0 cites
- 3438US2007199626A1Protection Against the Oxidation of Composite Material Parts Containing Carbon and Parts thus ProtectedDISS PASCAL·Filed 2004·Application pending·0 cites
- 3538US2012164430A1Composite material part having a ceramic matrix, and method for manufacturing sameTHEBAULT JACQUES·Filed 2010·Application pending·0 cites
- 3635US2014287912A1Process for Preparing a Monolithic Catalysis Element Comprising a Fibrous Support and Said Monolithic Catalysis ElementHERAKLES·Filed 2012·Application pending·0 cites
- 3730US5996676ATooling using thermostructural composite materials containing carbon for heat treatment and/or thermochemical treatment installationsSNECMA·Filed 1996·Granted Dec 7, 1999·0 cites·10 claims
- 3828US6116203AMethod for making an internal combustion engine piston in thermostructural composite materialSNECMA·Filed 1998·Granted Sep 12, 2000·1 cites·13 claims
- 3928US4705694AProcess for making bioactive coatings on osseous prostheses, and prostheses thus obtainedEUROP PROPULSION·Filed 1986·Granted Nov 10, 1987·9 cites·1 claims
- 4028US2005077341A1Method of manufacturing an active cooling panel out of thermostructural composite materialSNECMA PROPULSION SOLIDE·Filed 2004·Application pending·0 cites
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