Inventor · disambiguated record
Patrick Jean-Louis Reghezza
Also filed as: REGHEZZA PATRICK · REGHEZZA PATRICK JEAN-LOUIS
28 granted patents·1 pending application·174 citations·filing 2003–2022
96Inventor score
Top patents by PatentIndex Score
29 records- 0186US7458769B2Device for damping vibration of a ring for axially retaining turbomachine fan bladesSNECMA·Filed 2006·Granted Dec 2, 2008·23 cites·9 claims
- 0283US8911210B2Vibration-damping shim for fan bladeBILZ LAURENT·Filed 2010·Granted Dec 16, 2014·16 cites·7 claims
- 0382US8870545B2Reinforced fan blade shimREGHEZZA PATRICK JEAN-LOUIS·Filed 2010·Granted Oct 28, 2014·10 cites·10 claims
- 0477US7938626B2Shim for a turbojet bladeSNECMA·Filed 2006·Granted May 10, 2011·18 cites·19 claims
- 0575US10677074B2Method for carrying out work on a rotor and associated foilSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jun 9, 2020·3 cites·9 claims
- 0675US7108484B2Restraining device for fan blade rootSNECMA MOTEURS·Filed 2003·Granted Sep 19, 2006·27 cites·4 claims
- 0772US8911212B2Turbomachine rotor with anti-wear shim between a disk and an annulusDELAPIERRE MICHAEL·Filed 2011·Granted Dec 16, 2014·5 cites·9 claims
- 0871US9677425B2Axisymmetrical intermediate case part including an insert positioned in an annular grooveSNECMA·Filed 2013·Granted Jun 13, 2017·5 cites·8 claims
- 0970US10253800B2System for repairing a fastener equipping a reactor wallSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Apr 9, 2019·3 cites·12 claims
- 1059US6910866B2Controlling the axial position of a fan bladeSNECMA MOTEURS·Filed 2003·Granted Jun 28, 2005·22 cites·20 claims
- 1157US8113783B2Assembly of a fan blade and of its damper, fan blade damper and method for calibrating the damperMACE JEROME PAUL MARCEAU·Filed 2008·Granted Feb 14, 2012·3 cites·14 claims
- 1256US8113785B2Turbomachine rotor and turbomachine comprising such a rotorFORGUE JEAN-BERNARD·Filed 2007·Granted Feb 14, 2012·7 cites·19 claims
- 1353US9500091B2Wear-resistant part for the support of a blade of a turbojet fanDELAPIERRE MICHAEL·Filed 2011·Granted Nov 22, 2016·1 cites·9 claims
- 1452US8535011B2Shim for a turbomachine bladeMACE JEROME·Filed 2008·Granted Sep 17, 2013·6 cites·5 claims
- 1551US10858941B2Shutter for turbine machine having an absent rectifier bladeSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 8, 2020·0 cites·9 claims
- 1651US8734103B2Method of repairing a flange of a casingREGHEZZA PATRICK JEAN-LOUIS·Filed 2011·Granted May 27, 2014·1 cites·11 claims
- 1751US8573944B2Anti-wear device of a turbomachine rotorDELAPIERRE MICHAEL·Filed 2010·Granted Nov 5, 2013·1 cites·14 claims
- 1850US9512724B2Method for repairing wear marks on a rotor supporting the fan of a bypass engineSNECMA·Filed 2013·Granted Dec 6, 2016·1 cites·12 claims
- 1949US12228045B2Method for repairing an end plate of a turbomachine rotorSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Feb 18, 2025·0 cites·4 claims
- 2047US10213882B2Method for repairing a fan casingSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Feb 26, 2019·0 cites·10 claims
- 2147US7080974B2Retention capacity of a blade having an asymmetrical hammerhead fastener, with the help of platform stiffenersSNECMA MOTEURS·Filed 2004·Granted Jul 25, 2006·10 cites·20 claims
- 2246US11060420B2Extraction device of a platform for holding a blade and method using this deviceSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jul 13, 2021·0 cites·9 claims
- 2346US10801369B2Intermediate casing of a turbine engine, provided with a sealing part at the arm/shroud interfaceSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Oct 13, 2020·0 cites·8 claims
- 2446US8827650B2Seal for a platform in the rotor of a turbine engineFORGUE JEAN-BERNARD·Filed 2009·Granted Sep 9, 2014·3 cites·11 claims
- 2544US2016032734A1Fan for a multi-flow turboshaft engine, and turboshaft engine equipped with such a fanSNECMA·Filed 2014·Application pending·0 cites
- 2643US8985961B2Turbomachine rotor comprising an anti-wear plug, and anti-wear plugCHRZASTEK THOMAS·Filed 2009·Granted Mar 24, 2015·3 cites·14 claims
- 2742US8465258B2Platform seal in a turbomachine rotor, method for improving the seal between a platform and a turbomachine bladeFORGUE JEAN-BERNARD·Filed 2009·Granted Jun 18, 2013·2 cites·10 claims
- 2838US7029237B2Retention capacity of blade having an asymmetrical hammerhead connectionSNECMA MOTEURS·Filed 2004·Granted Apr 18, 2006·4 cites·1 claims
- 2937US10724388B2Corrosion protection plug for filling an attachment opening, and system including said plugSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jul 28, 2020·0 cites·10 claims
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