Inventor · disambiguated record
Gilles Lepretre
Also filed as: LEPRETRE GILLES · LEPRETRE GILLES GERARD CLAUDE · LEPRETRE GILLES GÉRARD CLAUDE
14 granted patents·2 pending applications·196 citations·filing 1997–2022
91Inventor score
Top patents by PatentIndex Score
16 records- 0195US10655501B2Turbine ring assembly without cold assembly clearanceSAFRAN CERAM·Filed 2017·Granted May 19, 2020·37 cites·7 claims
- 0292US5941075AFuel injection system with improved air/fuel homogenizationSNECMA·Filed 1997·Granted Aug 24, 1999·79 cites·9 claims
- 0386US11015484B2Assembly for a spreader connection between a turbine casing and a turbine engine ring elementSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted May 25, 2021·4 cites·19 claims
- 0483US10544704B2Turbine ring assembly comprising a plurality of ring sectors made of ceramic matrix composite materialHERAKLES·Filed 2016·Granted Jan 28, 2020·5 cites·10 claims
- 0572US10578054B2Stiffening of the connection between flaps in a nozzle of variable cross sectionSAFRAN CERAM·Filed 2017·Granted Mar 3, 2020·2 cites·6 claims
- 0669US7412834B2Annular combustion chamber for a turbomachine with an improved inner fastening flangeSNECMA·Filed 2005·Granted Aug 19, 2008·12 cites·4 claims
- 0767US7040098B2Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directionsSNECMA MOTEURS·Filed 2004·Granted May 9, 2006·27 cites·4 claims
- 0854US11512605B2Attachment of a nozzle to a casing of a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Nov 29, 2022·0 cites·17 claims
- 0952US7409831B2Provision of sealing in a jet engine for bleeding air to the cabin using a tube with a double ball jointSNECMA·Filed 2004·Granted Aug 12, 2008·9 cites·8 claims
- 1052US2025026689A1Core for producing a ceramic matrix composite distributorSAFRAN CERAM·Filed 2022·Application pending·0 cites
- 1148US7073336B2Provision of sealing for the cabin-air bleed cavity using a segment sealSNECMA MOTEURS·Filed 2004·Granted Jul 11, 2006·9 cites·6 claims
- 1247US6679679B1Internal stator shroudSNECMA MOTEURS·Filed 2001·Granted Jan 20, 2004·12 cites·14 claims
- 1346US11208906B2Connection between a ceramic matrix composite stator sector and a metallic support of a turbomachine turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Dec 28, 2021·0 cites·15 claims
- 1443US12031455B2Turbomachine turbine having CMC nozzle with load spreadingSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jul 9, 2024·0 cites·14 claims
- 1543US11814990B2Turbomachine turbine having a CMC nozzle with load spreadingSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Nov 14, 2023·0 cites·10 claims
- 1630US2005102994A1Provision of sealing for the cabin-air bleed cavity of a jet engine using a brush sealSNECMA MOTEURS·Filed 2004·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →