Jacky Naudet

Person

Evry, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Device for maintaining and positioning harnesses on a turbo-jet engine
- Patent number 7,500,644
- Issue date Mar 10, 2009
- SNECMA
- Jacky Naudet
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Link between two mechanical members
- Patent number 7,438,492
- Issue date Oct 21, 2008
- SNECMA
- Jacky Naudet
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Device for stopping in rotation a fixed blade bearing sector in a g...
- Patent number 7,018,173
- Issue date Mar 28, 2006
- SNECMA Moteurs
- Serge Bongrand
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Device for controlling variable-pitch blades
- Patent number 6,688,846
- Issue date Feb 10, 2004
- SNECMA Moteurs
- Jean-Pierre Caubet
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Blade locking device with hammer fastener on a disk
- Patent number 6,464,463
- Issue date Oct 15, 2002
- SNECMA Moteurs
- Jean-Luc Christian Yvon Goga
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
High-pressure compressor stator
- Patent number 6,390,771
- Issue date May 21, 2002
- SNECMA Moteurs
- Pascal Gérard Gervais
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Axisymmetric, converging-diverging, jet-deflecting turbojet-engine...
- Patent number 6,349,539
- Issue date Feb 26, 2002
- SNECMA Moteurs
- Didier Georges Feder
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Leaktight seal of a circular vane stage
- Patent number 6,332,617
- Issue date Dec 25, 2001
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation - S.N.E.C....
- Jacques Leveaux
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Bladed disk with three-root blades
- Patent number 5,919,032
- Issue date Jul 6, 1999
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jacky Naudet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Braking nuts or screws and mountings obtained with same devices
- Patent number 5,702,217
- Issue date Dec 30, 1997
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Louis Charbonnel
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Turbo-jet equipped with inclined balancing disks within the rotor o...
- Patent number 5,579,644
- Issue date Dec 3, 1996
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jacky S. Naudet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Compressor turbojet engine whose rotor has a movable upstream stage
- Patent number 5,473,883
- Issue date Dec 12, 1995
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jacky S. Naudet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine engine stator with pivoting blades and control ring
- Patent number 5,466,122
- Issue date Nov 14, 1995
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Louis Charbonnel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Variable phase vane
- Patent number 5,407,322
- Issue date Apr 18, 1995
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Louis Charbonnel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Annular gasket disposed at one axial extremity of a rotor and cover...
- Patent number 5,330,324
- Issue date Jul 19, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Daniel Agram
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Stator for directing the inlet of air inside a turbo-engine and met...
- Patent number 5,328,327
- Issue date Jul 12, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jacky Naudet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Sealing device between blade stages and a rotary drum, particularly...
- Patent number 5,328,328
- Issue date Jul 12, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Louis Charbonnel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Sealing structure for a pivoting blade of a gas turbine
- Patent number 5,324,165
- Issue date Jun 28, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Louis Charbonnel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Method of fixing stemmed blade for a flow-straightening stage of a...
- Patent number 5,319,850
- Issue date Jun 14, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Louis Charbonnel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbomachine stator having a double skin casing including means for...
- Patent number 5,320,484
- Issue date Jun 14, 1994
- General Electric Company
- Jean-Louis Charbonnel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Device for checking the clearances of a gas turbine compressor casing
- Patent number 5,314,303
- Issue date May 24, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Louis Charbonnel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbo aero engine equipped with means facilitating adjustment of pl...
- Patent number 5,288,206
- Issue date Feb 22, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Alain M. L. Bromann
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Blade control rod and system of such rods
- Patent number 5,277,544
- Issue date Jan 11, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jacky Naudet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Stemmed blade for a flow-straightening stage of a gas turbine engin...
- Patent number 5,236,304
- Issue date Aug 17, 1993
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Louis Charbonnel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Operating mechanism for variably settable blades of a turbomachine
- Patent number 5,224,820
- Issue date Jul 6, 1993
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation
- Christophe Brichet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Rotor fitted with spacer blocks between the blades
- Patent number 5,161,949
- Issue date Nov 10, 1992
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation"S.N.E.M.C.A."
- Michel A. Brioude
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turboshaft engine casing joint with reinforced axial restraint
- Patent number 5,096,377
- Issue date Mar 17, 1992
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Philippe P. Catte
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Variable stator vane with separate guide disk
- Patent number 5,039,277
- Issue date Aug 13, 1991
- Societe National d'Etude et de Construction de Moteurs d'Aviation
- Jacky Naudet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Temporary locking system for variably settable stator blades
- Patent number 5,000,659
- Issue date Mar 19, 1991
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Philippe P. Catte
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Fastening spindle and method of assembly for attaching rotor elemen...
- Patent number 4,844,694
- Issue date Jul 4, 1989
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- Jacky Naudet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
Rotor blade for a turbo-machine
- Publication number 20050129521
- Publication date Jun 16, 2005
- SNECMA MOTEURS
- Jacky Naudet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Link between two mechanical members
- Publication number 20040265054
- Publication date Dec 30, 2004
- SNECMA MOTEURS
- Jacky Naudet
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Application
Device for maintaining and positioning harnesses on a turbo-jet engine
- Publication number 20040266274
- Publication date Dec 30, 2004
- SNECMA MOTEURS
- Jacky Naudet
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Method for making a blade ring
- Publication number 20040244195
- Publication date Dec 9, 2004
- Gerard Michel Roland Gueldry
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
Device for stopping in rotation a fixed blade bearing sector in a g...
- Publication number 20040240992
- Publication date Dec 2, 2004
- Serge Bongrand
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Device for controlling variable-pitch blades
- Publication number 20020034439
- Publication date Mar 21, 2002
- SNECMA MOTEURS
- Jean-Pierre Caubet
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
Blade locking device with hammer fastener on a disk
- Publication number 20010055527
- Publication date Dec 27, 2001
- Jean-Luc Christian Yvon Goga
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Jacky Naudet

Person

Patents Grantslast 30 patents

Device for maintaining and positioning harnesses on a turbo-jet engine

Link between two mechanical members

Device for stopping in rotation a fixed blade bearing sector in a g...

Device for controlling variable-pitch blades

Blade locking device with hammer fastener on a disk

High-pressure compressor stator

Axisymmetric, converging-diverging, jet-deflecting turbojet-engine...

Leaktight seal of a circular vane stage

Bladed disk with three-root blades

Braking nuts or screws and mountings obtained with same devices

Turbo-jet equipped with inclined balancing disks within the rotor o...

Compressor turbojet engine whose rotor has a movable upstream stage

Turbine engine stator with pivoting blades and control ring

Variable phase vane

Annular gasket disposed at one axial extremity of a rotor and cover...

Stator for directing the inlet of air inside a turbo-engine and met...

Sealing device between blade stages and a rotary drum, particularly...

Sealing structure for a pivoting blade of a gas turbine

Method of fixing stemmed blade for a flow-straightening stage of a...

Turbomachine stator having a double skin casing including means for...

Device for checking the clearances of a gas turbine compressor casing

Turbo aero engine equipped with means facilitating adjustment of pl...

Blade control rod and system of such rods

Stemmed blade for a flow-straightening stage of a gas turbine engin...

Operating mechanism for variably settable blades of a turbomachine

Rotor fitted with spacer blocks between the blades

Turboshaft engine casing joint with reinforced axial restraint

Variable stator vane with separate guide disk

Temporary locking system for variably settable stator blades

Fastening spindle and method of assembly for attaching rotor elemen...

Patents Applicationslast 30 patents

Rotor blade for a turbo-machine

Link between two mechanical members

Device for maintaining and positioning harnesses on a turbo-jet engine

Method for making a blade ring

Device for stopping in rotation a fixed blade bearing sector in a g...

Device for controlling variable-pitch blades

Blade locking device with hammer fastener on a disk