Inventor
GENDRAUD ALAIN DOMINIQUE
FR25 patents
⚠️ This page may combine multiple inventors who share the name “GENDRAUD ALAIN DOMINIQUE”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
SAFRAN AIRCRAFT ENGINES
7 patentsUS10920593B2Feb 16, 2021
Movable ring assembly for a turbine engine turbine
SAFRAN AIRCRAFT ENGINES17 citations80
US10344610B2Jul 9, 2019
Turbomachine module
SAFRAN AIRCRAFT ENGINES6 citations67
US11585237B2Feb 21, 2023
System for the axial retention of a rolling element bearing
SAFRAN AIRCRAFT ENGINES2 citations64
US10900382B2Jan 26, 2021
Assembly comprising a locked securing stud
SAFRAN AIRCRAFT ENGINES5 citations63
US11441431B2Sep 13, 2022
Holding system for the dismantling of a blade wheel
SAFRAN AIRCRAFT ENGINES0 citations56
US12276209B2Apr 15, 2025
Mounting of a sealing ring on an aeronautical turbine engine
SAFRAN AIRCRAFT ENGINES0 citations49
US12071856B2Aug 27, 2024
Assembly for a turbomachine turbine
SAFRAN AIRCRAFT ENGINES0 citations49
DAKOWSKI MATHIEU
4 patentsUS8858169B2Oct 14, 2014
High-pressure turbine for turbomachine, associated guide vane sector and aircraft engine
DAKOWSKI MATHIEU9 citations82
US8100635B2Jan 24, 2012
Control of clearance at blade tips in a high-pressure turbine of a turbine engine
DAKOWSKI MATHIEU11 citations82
US8403636B2Mar 26, 2013
Turbine stage in a turbomachine
DAKOWSKI MATHIEU6 citations70
US8133018B2Mar 13, 2012
High-pressure turbine of a turbomachine
DAKOWSKI MATHIEU5 citations60
SNECMA
4 patentsUS9726033B2Aug 8, 2017
Rotor wheel for a turbine engine
SNECMA2 citations72
US9683452B2Jun 20, 2017
Labyrinth seal for gas turbine engine turbine
SNECMA3 citations70
US9957841B2May 1, 2018
Turbine stage for a turbine engine
SNECMA2 citations66
US9631495B2Apr 25, 2017
Cooling for the retaining dovetail of a turbomachine blade
SNECMA6 citations66
SNECMA MOTEURS
3 patentsUS6666645B1Dec 23, 2003
Arrangement for adjusting the diameter of a gas turbine stator
SNECMA MOTEURS68 citations95
US6726446B2Apr 27, 2004
Stay sector of stator shroud of the high-pressure turbine of a gas turbine engine with clearance control
SNECMA MOTEURS47 citations92
US6699011B2Mar 2, 2004
Linking arrangement of a turbine stator ring to a support strut
SNECMA MOTEURS26 citations89
GARIN FABRICE MARCEL NOEL
3 patentsUS9103220B2Aug 11, 2015
Interface element between a blade root and a blade root housing of a turbine disc, and turbine rotor comprising an interface element
GARIN FABRICE MARCEL NOEL11 citations80
US8961117B2Feb 24, 2015
Insulating a circumferential rim of an outer casing of a turbine engine from a corresponding ring sector
GARIN FABRICE MARCEL NOEL14 citations79
US8734100B2May 27, 2014
Turbine stage
GARIN FABRICE MARCEL NOEL2 citations59
GENDRAUD ALAIN DOMINIQUE
2 patentsUS8662828B2Mar 4, 2014
High pressure turbine of a turbomachine with improved assembly of the mobile blade radial clearance control box
GENDRAUD ALAIN DOMINIQUE4 citations62
US8721277B2May 13, 2014
Unit for locking ring sectors on a turbomachine casing, comprising radial passages for gripping it
GENDRAUD ALAIN DOMINIQUE2 citations60