Jean-Louis Charbonnel

Person

Boissise Le Roi, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Gas turbine engine comprising a starter in the auxiliary gear box
- Patent number 7,971,423
- Issue date Jul 5, 2011
- Hispano Suiza
- Chloe Avila
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Pivoting vane internal extremity bearing
- Patent number 5,796,199
- Issue date Aug 18, 1998
- 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
Arrangement of gas turbine engine comprising aerodynamic vanes and...
- Patent number 5,740,674
- Issue date Apr 21, 1998
- Societe Nationale d'Etude Et de Construction de Moteurs d'Aviation "Sherma"
- Bruno Beutin
- 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
Control device for a stage of blades with variable pitch
- Patent number 5,692,879
- Issue date Dec 2, 1997
- 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
Device for assembling a circular stage of pivoting vanes
- Patent number 5,636,968
- Issue date Jun 10, 1997
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jacques R. Audet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Axial fixing arrangement for rotor blades of a turbomachine
- Patent number 5,622,476
- Issue date Apr 22, 1997
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Danielle C. R. Adde
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine engine equipped with means for controlling the play between...
- Patent number 5,616,003
- Issue date Apr 1, 1997
- 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
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
Retaining and sealing system for rotor blades
- Patent number 5,445,499
- Issue date Aug 29, 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
Removable inspection hole plug
- Patent number 5,431,534
- Issue date Jul 11, 1995
- (S.N.E.C.M.A.) Societe National d'Etude et de Construction de Moteurs d'Aviation
- Jean-Louis Charbonnel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
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
Sealing and retaining device for a rotor notched with pin settings...
- Patent number 5,320,492
- Issue date Jun 14, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Michel A. Bouru
- 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
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
Apparatus for separating a liquid from a gas, particularly for turb...
- Patent number 4,561,867
- Issue date Dec 31, 1985
- 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
Inter-shaft bearing for multibody turbojet engines with damping by...
- Patent number 4,378,197
- Issue date Mar 29, 1983
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation, "S.N.E.C....
- Christian J. Cattaneo
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
GAS TURBINE ENGINE COMPRISING A STARTER IN THE AUXILIARY GEAR BOX
- Publication number 20090120098
- Publication date May 14, 2009
- HISPANO-SUIZA
- Chloe AVILA
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Jean-Louis Charbonnel

Person

Patents Grantslast 30 patents

Gas turbine engine comprising a starter in the auxiliary gear box

Pivoting vane internal extremity bearing

Arrangement of gas turbine engine comprising aerodynamic vanes and...

Braking nuts or screws and mountings obtained with same devices

Control device for a stage of blades with variable pitch

Device for assembling a circular stage of pivoting vanes

Axial fixing arrangement for rotor blades of a turbomachine

Turbine engine equipped with means for controlling the play between...

Turbine engine stator with pivoting blades and control ring

Retaining and sealing system for rotor blades

Removable inspection hole plug

Variable phase vane

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

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

Sealing structure for a pivoting blade of a gas turbine

Sealing and retaining device for a rotor notched with pin settings...

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...

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

Operating mechanism for variably settable blades of a turbomachine

Apparatus for separating a liquid from a gas, particularly for turb...

Inter-shaft bearing for multibody turbojet engines with damping by...

Patents Applicationslast 30 patents

GAS TURBINE ENGINE COMPRISING A STARTER IN THE AUXILIARY GEAR BOX