Inventor · disambiguated record
Eric Conete
Also filed as: CONETE ERIC
35 granted patents·3 pending applications·675 citations·filing 1993–2022
97Inventor score
Top patents by PatentIndex Score
38 records- 0197US7249462B2Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbineSNECMA·Filed 2005·Granted Jul 31, 2007·78 cites·22 claims
- 0296US7234306B2Gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking membersSNECMA·Filed 2005·Granted Jun 26, 2007·62 cites·9 claims
- 0395US6398483B1Protection device for protecting control mechanism of inlet guide-vanes of turbojet engineSNECMA MOTEURS·Filed 2000·Granted Jun 4, 2002·48 cites·14 claims
- 0494US11821387B2Ejection cone having a flexible aerodynamic attachmentSAFRAN CERAM·Filed 2020·Granted Nov 21, 2023·4 cites·10 claims
- 0594US7677026B2Mixer for separate-flow nozzleSNECMA PROPULSION SOLIDE·Filed 2005·Granted Mar 16, 2010·48 cites·14 claims
- 0694US7237388B2Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzleSNECMA·Filed 2005·Granted Jul 3, 2007·48 cites·9 claims
- 0792US11519361B2Exhaust cone with flexible fittingSAFRAN CERAM·Filed 2019·Granted Dec 6, 2022·6 cites·9 claims
- 0888US6988369B2Combustion chamber sealing ring, and a combustion chamber including such a ringSNECMA MOTEURS·Filed 2003·Granted Jan 24, 2006·43 cites·20 claims
- 0987US9261008B2Exhaust with an acoustic attenuation systemHERAKLES·Filed 2013·Granted Feb 16, 2016·13 cites·9 claims
- 1085US8590316B2CMC mixer with structural outer cowlingCONETE ERIC·Filed 2008·Granted Nov 26, 2013·20 cites·15 claims
- 1181US9573852B2Method for brazing parts made from a composite material, with anchoring of the brazed jointHERAKLES·Filed 2013·Granted Feb 21, 2017·4 cites·9 claims
- 1281US7237387B2Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbineSNECMA·Filed 2005·Granted Jul 3, 2007·20 cites·10 claims
- 1380US9403240B2Method for the brazing of parts made from a composite material, incorporating a slug in the bondHERAKLES·Filed 2013·Granted Aug 2, 2016·4 cites·10 claims
- 1480US8919136B2Flexible abutment links for attaching a part made of CMCCONETE ERIC·Filed 2009·Granted Dec 30, 2014·14 cites·12 claims
- 1579US6732532B2Resilient mount for a CMC combustion chamber of a turbomachine in a metal casingSNECMA MOTEURS·Filed 2002·Granted May 11, 2004·24 cites·13 claims
- 1678US6708495B2Fastening a CMC combustion chamber in a turbomachine using brazed tabsSNECMA MOTEURS·Filed 2002·Granted Mar 23, 2004·44 cites·12 claims
- 1775US8424312B2Exhaust system for gas turbineCONETE ERIC·Filed 2008·Granted Apr 23, 2013·17 cites·18 claims
- 1874US6679062B2Architecture for a combustion chamber made of ceramic matrix materialSNECMA MOTEURS·Filed 2002·Granted Jan 20, 2004·38 cites·10 claims
- 1973US6823676B2Mounting for a CMC combustion chamber of a turbomachine by means of flexible connecting sleevesSNECMA MOTEURS·Filed 2002·Granted Nov 30, 2004·35 cites·12 claims
- 2071US9267531B2Assembly providing a connection that is self tightening with temperatureHERAKLES·Filed 2014·Granted Feb 23, 2016·4 cites·20 claims
- 2171US6675585B2Connection for a two-part CMC chamberSNECMA MOTEURS·Filed 2002·Granted Jan 13, 2004·36 cites·9 claims
- 2267US8640825B2Acoustic panel for an ejector nozzleVAUCHEL GUY BERNARD·Filed 2009·Granted Feb 4, 2014·8 cites·17 claims
- 2365US5367874AIntegral composite gas turbine afterburner structureSNECMA·Filed 1993·Granted Nov 29, 1994·27 cites·8 claims
- 2463US12195406B2CMC materials with integrated thermocoupleSAFRAN CERAM·Filed 2022·Granted Jan 14, 2025·0 cites·10 claims
- 2561US10066581B2Structure for fastening after-body parts of an aeroengineHERAKLES·Filed 2013·Granted Sep 4, 2018·2 cites·8 claims
- 2659US2023406780A1Method for fabricating a turbomachine blade made from a composite materialSAFRAN CERAM·Filed 2021·Application pending·0 cites
- 2755US11619380B2Constant volume combustion systemSAFRAN·Filed 2018·Granted Apr 4, 2023·0 cites·3 claims
- 2854US8205453B2Method for assembling end to end two parts having different thermal expansion coefficients and assembly thus obtainedCONETE ERIC·Filed 2008·Granted Jun 26, 2012·5 cites·12 claims
- 2953US12196157B2Turbomachine turbine assemblySAFRAN CERAM·Filed 2021·Granted Jan 14, 2025·0 cites·9 claims
- 3050US12078356B2Subassembly comprising means for compensating for a difference in expansionSAFRAN CERAM·Filed 2022·Granted Sep 3, 2024·0 cites·10 claims
- 3147US5359849AAfterburner assembly for a gas turbine engineSNECMA·Filed 1993·Granted Nov 1, 1994·14 cites·36 claims
- 3246US7168253B1Monobloc flameholder arm for an afterburner device of a bypass turbojetSNECMA MOTEURS·Filed 2004·Granted Jan 30, 2007·6 cites·19 claims
- 3346US2015275671A1Method of locally treating a part made of porous composite materialHERAKLES·Filed 2013·Application pending·0 cites
- 3445US11168610B2Constant-volume combustion system comprising a rotating closure element with segmented aperturesSAFRAN·Filed 2018·Granted Nov 9, 2021·0 cites·13 claims
- 3542US11959440B2Acoustic attenuation structure made of composite material and method for manufacturing sameSAFRAN CERAM·Filed 2020·Granted Apr 16, 2024·0 cites·12 claims
- 3640US12253048B2Fastening of an exhaust cone in a turbomachine turbineSAFRAN CERAM·Filed 2021·Granted Mar 18, 2025·0 cites·7 claims
- 3739US2012160933A1Structuring assembly for an exhaust nozzleVAUCHEL GUY BERNARD·Filed 2010·Application pending·0 cites
- 3831US5269138AVariable geometry flame trap device for use in an after-burner device of a gas turbineSNECMA·Filed 1993·Granted Dec 14, 1993·3 cites·7 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →