Inventor
NAUDET JACKY
FR28 patents
⚠️ This page may combine multiple inventors who share the name “NAUDET JACKY”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
SNECMA
24 patentsUS5328327AJul 12, 1994
Stator for directing the inlet of air inside a turbo-engine and method for mounting a vane of said stator
SNECMA68 citations96
US5039277AAug 13, 1991
Variable stator vane with separate guide disk
SNECMA61 citations96
US4844694AJul 4, 1989
Fastening spindle and method of assembly for attaching rotor elements of a gas-turbine engine
SNECMA72 citations96
US4604030AAug 5, 1986
Compressor with variable incidence stator vanes
SNECMA81 citations96
US4730983AMar 15, 1988
System for attaching a rotor blade to a rotor disk
SNECMA64 citations95
US4706354ANov 17, 1987
Method of manufacturing a root pivot assembly of a variable incidence turbo-machine blade
SNECMA53 citations95
US6011617AJan 4, 2000
System for inspecting internal zones of a machine by optical fibre endoscopy
SNECMA23 citations92
US5277544AJan 11, 1994
Blade control rod and system of such rods
SNECMA29 citations92
US4595339AJun 17, 1986
Centripetal accelerator for air exhaustion in a cooling device of a gas turbine combined with the compressor disc
SNECMA30 citations92
US7500644B2Mar 10, 2009
Device for maintaining and positioning harnesses on a turbo-jet engine
SNECMA98 citations91
US5314303AMay 24, 1994
Device for checking the clearances of a gas turbine compressor casing
SNECMA38 citations90
US5161949ANov 10, 1992
Rotor fitted with spacer blocks between the blades
SNECMA64 citations90
US5288206AFeb 22, 1994
Turbo aero engine equipped with means facilitating adjustment of plays of the stator and between the stator and rotor
SNECMA41 citations89
US4750746AJun 14, 1988
Device for attaching a seal member to a shaft
SNECMA36 citations87
US5466122ANov 14, 1995
Turbine engine stator with pivoting blades and control ring
SNECMA27 citations85
US7438492B2Oct 21, 2008
Link between two mechanical members
SNECMA13 citations78
US5224820AJul 6, 1993
Operating mechanism for variably settable blades of a turbomachine
SNECMA20 citations78
US5319850AJun 14, 1994
Method of fixing stemmed blade for a flow-straightening stage of a gas turbine engine
SNECMA9 citations73
US5236304AAug 17, 1993
Stemmed blade for a flow-straightening stage of a gas turbine engine and method of fixing said blade
SNECMA10 citations73
US4787820ANov 29, 1988
Turbine plant compressor disc with centripetal accelerator for the induction of turbine cooling air
SNECMA13 citations73
US5096377AMar 17, 1992
Turboshaft engine casing joint with reinforced axial restraint
SNECMA13 citations71
US5000659AMar 19, 1991
Temporary locking system for variably settable stator blades
SNECMA10 citations71
US4732536AMar 22, 1988
Turbo-machine compressor with variable incidence stator vanes
SNECMA14 citations69
US5919032AJul 6, 1999
Bladed disk with three-root blades
SNECMA15 citations67
SNECMA MOTEURS
4 patentsUS6688846B2Feb 10, 2004
Device for controlling variable-pitch blades
SNECMA MOTEURS28 citations87
US6629463B2Oct 7, 2003
Acoustic inspection of one-piece bladed wheels
SNECMA MOTEURS32 citations87
US6464463B2Oct 15, 2002
Blade locking device with hammer fastener on a disk
SNECMA MOTEURS29 citations86
US7018173B2Mar 28, 2006
Device for stopping in rotation a fixed blade bearing sector in a gas turbine casing
SNECMA MOTEURS7 citations67