Inventor
Jacques Thebault
Inventor
Bordeaux, FR
Overview
Patents· 31 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
C04Bprimary
C04BLime, magnesia31%
Y10TTechnical subjects covered by former us classification21%
F16DCouplings for transmitting rotation8%
Y10STechnical subjects covered by former uspc cross-reference art collections [xracs] and digests7%
C23CCoating metallic material6%
B32BLayered products, i.e. products built-up of strata of flat or non-flat, e.g. cellular or honeycomb, form5%
C03CChemical composition of glasses, glazes or vitreous enamels2%
F02KJet-propulsion plants2%
F05CIndexing scheme relating to materials, material properties or material characteristics for machines, engines or pumps other than non-positive-displacement machines or engines2%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants2%
PatentTitleYear
9,382,164'Materials and parts that can withstand high temperatures in an oxidizing medium, and method for manufacturing same'20169,340,460'Ultra-refractory material that is stable in a wet environment, and process for manufacturing same'20168,357,423'Method for making a refractory carbide layer on a part made of C/C composite material'20138,261,891'Method of siliciding thermostructural composite materials, and parts obtained by the method'20128,084,079'Method for chemical infiltration in the gas phase for the densification of porous substrates with pyrolytic carbon'20117,736,554'Method of manufacturing a part out of impervious thermostructural composite material'20107,560,139'Thermostructural composite structure with a compositional gradient, its manufacturing process'20097,497,918'Method of siliciding thermostructural composite materials, and parts obtained by the method'20097,063,886'Thermostructural composite structure with a compositional gradient and its manufacturing process'20066,926,925'Method of making a continuous coating on the surface of a part'20056,740,408'Protecting composite material parts against oxidation'20046,616,756'Protection for a carbon material, in particular C/C composite, bowl that is to receive a crucible, such as a silica crucible for drawing silicon'20036,413,585'Thermochemical treatment, in halogenated atmosphere, of a carbon-containing material'20026,410,088'CVI (chemical vapor infiltration) densification of porous structures'20026,116,203'Method for making an internal combustion engine piston in thermostructural composite material'20006,001,419'Chemical vapor infiltration method with variable infiltration parameters'19995,996,676'Tooling using thermostructural composite materials containing carbon for heat treatment and/or thermochemical treatment installations'19995,853,821'Method of protecting a part made of a carbon-containing composite material against oxidation'19985,714,244'Method for protecting a porous carbon-containing material from oxidation, and material obtained thereby'19985,686,144'Method for applying an anti-oxidative coating on brake disks of a carbon-containing composite material'19975,622,751'Method of protecting products of composite material against oxidizing and products protected thereby'19975,411,762'Method of obtaining a sialon-based ceramic material by reducing an aluminosilicate material, and use thereof in forming a ceramic coating on a refractory substrate'19955,332,619'Process 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 process'19945,217,755'Chemical vapor infiltration method utilizing substantially diffusive conditions'19935,134,020'Composite material with multiple interphases between refractory reinforcing fibers and ceramix matrix'19925,132,169'Composite materials having multidirectional reinforcement textures made essentially of ceramic fibers having a silicon compound base'19925,128,117'Process for the manufacture of multidirectional reinforcement textures made essentially of ceramic fibers having a silicon compound base for the manufacture of composite materials'19925,026,604'Composite material with refractory fibrous reinforcement and ceramic matrix'19914,752,503'Process for the manufacture of a composite material with refractory fibrous reinforcement and ceramic matrix'19884,748,079'Composite materials constituted by a matrix in resin coke carbon, reinforced with pyrolytic carbon-coated refractory fibers'19884,705,694'Process for making bioactive coatings on osseous prostheses, and prostheses thus obtained'1987Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1987–1998Patents assigned to EUROP PROPULSION (14)· patent assignee history
1987–2016Based in Bordeaux, FR· patent location history
1999–2002Patents assigned to SNECMA (5)· patent assignee history
2004–2013Patents assigned to SNECMA PROPULSION SOLIDE (9)· patent assignee history
2004Based in Bordeaux-Cauderan, FR· patent location history
2011–2016Patents assigned to THEBAULT JACQUES (5)· patent assignee history
2013–2016Patents assigned to CENTRE NAT RECH SCIENT (2)· patent assignee history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| EUROP PROPULSION | 14 | 1987–1998 |
| SNECMA PROPULSION SOLIDE | 9 | 2004–2013 |
| SNECMA | 5 | 1999–2002 |
| THEBAULT JACQUESself | 5 | 2011–2016 |
| CENTRE NAT RECH SCIENT | 2 | 2013–2016 |
Locations
| Location | Patents | Span |
|---|---|---|
| Bordeaux, FR | 30 | 1987–2016 |
| Bordeaux-Cauderan, FR | 1 | 2004 |