Inventor
SOUPIZON JEAN-LUC
FR40 patents
⚠️ This page may combine multiple inventors who share the name “SOUPIZON JEAN-LUC”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
SNECMA
14 patentsUS4925365AMay 15, 1990
Turbine stator ring assembly
SNECMA76 citations94
US7687021B2Mar 30, 2010
Method of fabricating a casing for turbine stator
SNECMA31 citations91
US6149074ANov 21, 2000
Device for cooling or heating a circular housing
SNECMA63 citations91
US7377749B2May 27, 2008
Device for balancing a rotating part, in particular a turbojet rotor
SNECMA38 citations89
US7484924B2Feb 3, 2009
Device for limiting turbine overspeed in a turbomachine
SNECMA9 citations84
US8011879B2Sep 6, 2011
Transition channel between two turbine stages
SNECMA7 citations83
US8348620B2Jan 8, 2013
Device for axially retaining blades mounted on a turbomachine rotor disk
SNECMA7 citations81
US7390170B2Jun 24, 2008
Device for assembling annular flanges together, in particular in a turbomachine
SNECMA15 citations80
US9551236B2Jan 24, 2017
Arrangement for the guiding of the flow of a liquid in relation to the rotor of a turbomachine
SNECMA2 citations71
US7252476B2Aug 7, 2007
Device for lubricating a component in a turbomachine
SNECMA3 citations62
US7794203B2Sep 14, 2010
Joining device for joining two assemblies, for example for a stator of a turbomachine
SNECMA6 citations60
US7367774B2May 6, 2008
System for protecting a main shaft of an engine having a fusible bearing
SNECMA4 citations60
US7360986B2Apr 22, 2008
System for blocking a main shaft of an engine having a fusible bearing
SNECMA5 citations60
US9920690B2Mar 20, 2018
Air supply device for aircraft engine turbines
SNECMA0 citations30
SNECMA MOTEURS
10 patentsUS7290982B2Nov 6, 2007
Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle
SNECMA MOTEURS20 citations83
US7025562B2Apr 11, 2006
Device for cooling turbine disks
SNECMA MOTEURS12 citations83
US7004721B2Feb 28, 2006
Annular platform for a nozzle of a low-pressure turbine of a turbomachine
SNECMA MOTEURS11 citations82
US7037078B2May 2, 2006
Turbomachine turbines with blade inserts having resonant frequencies that are adjusted to be different, and a method of adjusting the resonant frequency of a turbine blade insert
SNECMA MOTEURS13 citations76
US7137783B2Nov 21, 2006
Cooled gas turbine blades
SNECMA MOTEURS7 citations72
US6939104B2Sep 6, 2005
Turbine blade with sealing element
SNECMA MOTEURS10 citations66
US7351030B2Apr 1, 2008
Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectors
SNECMA MOTEURS3 citations61
US7326035B2Feb 5, 2008
Device for attaching a moving blade to a turbine rotor disk in a turbomachine
SNECMA MOTEURS5 citations61
US7004725B2Feb 28, 2006
Device for centering a tube in a turbine shaft
SNECMA MOTEURS6 citations56
US7210901B2May 1, 2007
Assembly of sectors of a dispensing unit in a gas turbine
SNECMA MOTEURS0 citations40