Inventor · disambiguated record
Jean Pierre Mareix
Also filed as: MAREIX JEAN-PIERRE · MAREIX JEAN-PIERRE L · MAREIX JEAN-PIERRE LOUIS
14 granted patents·1 pending application·234 citations·filing 1989–2014
92Inventor score
Files withSNECMA9BEAUJARD ANTOINE JEAN-PHILIPPE3BERCHE EMMANUEL1CAMHI EMMANUEL PIERRE1SAFRAN AIRCRAFT ENGINES1
Top patents by PatentIndex Score
15 records- 0191US4943013AFastener system for a jet engine mountingSNECMA·Filed 1989·Granted Jul 24, 1990·91 cites·10 claims
- 0289US6464232B1Leaf sealSNECMA·Filed 1999·Granted Oct 15, 2002·60 cites·6 claims
- 0385US7950902B2Cooling channel formed in a wallSNECMA·Filed 2006·Granted May 31, 2011·9 cites·11 claims
- 0471US9863263B2Turbine wheel for a turbine engineSNECMA·Filed 2012·Granted Jan 9, 2018·5 cites·6 claims
- 0569US9103219B2CMC turbine nozzle adapted to support a metallic turbine internal casing by an axial contactBEAUJARD ANTOINE JEAN-PHILIPPE·Filed 2012·Granted Aug 11, 2015·4 cites·9 claims
- 0660US9638042B2Turbine engine comprising a metal protection for a composite partBEAUJARD ANTOINE JEAN-PHILIPPE·Filed 2012·Granted May 2, 2017·2 cites·9 claims
- 0757US5312227ATurbine casing delimiting an annular gas flow stream divided by radial armsSNECMA·Filed 1992·Granted May 17, 1994·39 cites·14 claims
- 0856US10329912B2Turbine rotor for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2013·Granted Jun 25, 2019·2 cites·12 claims
- 0955US8875393B2Cooling channel formed in a wallCAMHI EMMANUEL PIERRE·Filed 2010·Granted Nov 4, 2014·1 cites·8 claims
- 1054US9951636B2Double tube connecting deviceSNECMA·Filed 2013·Granted Apr 24, 2018·1 cites·9 claims
- 1154US9732618B2Turbine wheel in a turbine engineSNECMA·Filed 2013·Granted Aug 15, 2017·1 cites·14 claims
- 1254US9194241B2CMC turbine nozzle adapted to support a metallic turbine internal casing by a radial contactBEAUJARD ANTOINE JEAN-PHILIPPE·Filed 2012·Granted Nov 24, 2015·1 cites·9 claims
- 1348US9114469B2Electrode for forming a cooling channel in a wallSNECMA·Filed 2014·Granted Aug 25, 2015·0 cites·3 claims
- 1442US5520514ASealing lining between vanes and intermediate platformsSNECMA·Filed 1995·Granted May 28, 1996·18 cites·4 claims
- 1535US2012141257A1Segmented turbine ring for a turbomachine, and turbomachine fitted with such a ringBERCHE EMMANUEL·Filed 2011·Application pending·0 cites
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →