Inventor
REGHEZZA PATRICK JEAN-LOUIS
FR23 patents
⚠️ This page may combine multiple inventors who share the name “REGHEZZA PATRICK JEAN-LOUIS”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
SAFRAN AIRCRAFT ENGINES
8 patentsUS10677074B2Jun 9, 2020
Method for carrying out work on a rotor and associated foil
SAFRAN AIRCRAFT ENGINES3 citations66
US10253800B2Apr 9, 2019
System for repairing a fastener equipping a reactor wall
SAFRAN AIRCRAFT ENGINES3 citations64
US12228045B2Feb 18, 2025
Method for repairing an end plate of a turbomachine rotor
SAFRAN AIRCRAFT ENGINES0 citations52
US10801369B2Oct 13, 2020
Intermediate casing of a turbine engine, provided with a sealing part at the arm/shroud interface
SAFRAN AIRCRAFT ENGINES0 citations43
US11060420B2Jul 13, 2021
Extraction device of a platform for holding a blade and method using this device
SAFRAN AIRCRAFT ENGINES0 citations42
US10858941B2Dec 8, 2020
Shutter for turbine machine having an absent rectifier blade
SAFRAN AIRCRAFT ENGINES0 citations42
US10213882B2Feb 26, 2019
Method for repairing a fan casing
SAFRAN AIRCRAFT ENGINES0 citations41
US10724388B2Jul 28, 2020
Corrosion protection plug for filling an attachment opening, and system including said plug
SAFRAN AIRCRAFT ENGINES0 citations31
SNECMA
4 patentsUS7458769B2Dec 2, 2008
Device for damping vibration of a ring for axially retaining turbomachine fan blades
SNECMA23 citations87
US7938626B2May 10, 2011
Shim for a turbojet blade
SNECMA18 citations81
US9677425B2Jun 13, 2017
Axisymmetrical intermediate case part including an insert positioned in an annular groove
SNECMA5 citations66
US9512724B2Dec 6, 2016
Method for repairing wear marks on a rotor supporting the fan of a bypass engine
SNECMA1 citations43
FORGUE JEAN-BERNARD
3 patentsUS8113785B2Feb 14, 2012
Turbomachine rotor and turbomachine comprising such a rotor
FORGUE JEAN-BERNARD7 citations79
US8827650B2Sep 9, 2014
Seal for a platform in the rotor of a turbine engine
FORGUE JEAN-BERNARD3 citations56
US8465258B2Jun 18, 2013
Platform seal in a turbomachine rotor, method for improving the seal between a platform and a turbomachine blade
FORGUE JEAN-BERNARD2 citations56
DELAPIERRE MICHAEL
3 patentsUS8911212B2Dec 16, 2014
Turbomachine rotor with anti-wear shim between a disk and an annulus
DELAPIERRE MICHAEL5 citations68
US9500091B2Nov 22, 2016
Wear-resistant part for the support of a blade of a turbojet fan
DELAPIERRE MICHAEL1 citations48
US8573944B2Nov 5, 2013
Anti-wear device of a turbomachine rotor
DELAPIERRE MICHAEL1 citations45