Jean-Michel Bernard GUIMBARD

Person

Cely en Biere, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Blade with 3D platform comprising an inter-blade bulb
- Patent number 9,518,467
- Issue date Dec 13, 2016
- SNECMA
- Jean-Michel Guimbard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine engine blade
- Patent number 9,022,744
- Issue date May 5, 2015
- SNECMA
- Renaud Gabriel Constant Royan
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Blade with non-axisymmetric platform
- Patent number 9,004,865
- Issue date Apr 14, 2015
- SNECMA
- Jean-Michel Guimbard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Optimized aerodynamic profile for a turbine vane, in particular for...
- Patent number 8,757,968
- Issue date Jun 24, 2014
- SNECMA
- Jean Bleuzen
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Optimized aerodynamic profile for a turbine vane, in particular for...
- Patent number 8,734,096
- Issue date May 27, 2014
- SNECMA
- Jean-Michel Guimbard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Optimized aerodynamic profile for a turbine blade, in particular fo...
- Patent number 8,734,115
- Issue date May 27, 2014
- SNECMA
- Jean Bleuzen
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Blade with non-axisymmetric platform: recess and boss on the extrados
- Patent number 8,647,066
- Issue date Feb 11, 2014
- SNECMA
- Jean-Michel Guimbard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Cooled blade for a turbomachine
- Patent number 8,162,594
- Issue date Apr 24, 2012
- SNECMA
- Jean-Michel Bernard Guimbard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Inter-turbine casing with cooling circuit, and turbofan comprising it
- Patent number 8,162,593
- Issue date Apr 24, 2012
- SNECMA
- Jean-Michel Bernard Guimbard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method of designing a multistage turbine for a turbomachine
- Patent number 8,083,476
- Issue date Dec 27, 2011
- SNECMA
- Jean-Michel Bernard Guimbard
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Transition channel between two turbine stages
- Patent number 8,011,879
- Issue date Sep 6, 2011
- SNECMA
- Jean-Michel Guimbard
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Cooling layout for a turbine blade, turbine blade included therein,...
- Patent number 7,658,591
- Issue date Feb 9, 2010
- SNECMA
- Alexandre Dervaux
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Stator turbine vane with improved cooling
- Patent number 7,527,470
- Issue date May 5, 2009
- SNECMA
- Jean-Michel Guimbard
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Cooled gas turbine blades
- Patent number 7,137,783
- Issue date Nov 21, 2006
- SNECMA Moteurs
- Philippe Pabion
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Annular platform for a nozzle of a low-pressure turbine of a turbom...
- Patent number 7,004,721
- Issue date Feb 28, 2006
- SNECMA Moteurs
- Sébastien Imbourg
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
TURBOMACHINE COMBUSTION CHAMBER
- Publication number 20220074595
- Publication date Mar 10, 2022
- Turbotech
- Damien Fauvet
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
BLADE WITH 3D PLATFORM COMPRISING AN INTER-BLADE BULB
- Publication number 20150147179
- Publication date May 28, 2015
- SNECMA
- Jean-Michel GUIMBARD
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Turbine engine blade
- Publication number 20140105750
- Publication date Apr 17, 2014
- SNECMA
- Renaud Gabriel Constant ROYAN
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE VANE, IN PARTICULAR FOR...
- Publication number 20120051895
- Publication date Mar 1, 2012
- SNECMA
- Jean-Michel GUIMBARD
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE VANE, IN PARTICULAR FOR...
- Publication number 20120020800
- Publication date Jan 26, 2012
- SNECMA
- Jean BLEUZEN
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE, IN PARTICULAR FO...
- Publication number 20120020799
- Publication date Jan 26, 2012
- SNECMA
- Jean BLEUZEN
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
BLADE WITH NON-AXISYMMETRIC PLATFORM: RECESS AND BOSS ON THE EXTRADOS
- Publication number 20110189023
- Publication date Aug 4, 2011
- SNECMA
- Jean-Michel Guimbard
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
BLADE WITH 3D PLATFORM COMPRISING AN INTER-BLADE BULB
- Publication number 20110110788
- Publication date May 12, 2011
- SNECMA
- Jean-Michel Guimbard
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
BLADE WITH NON-AXISYMMETRIC PLATFORM
- Publication number 20110014056
- Publication date Jan 20, 2011
- SNECMA
- Jean-Michel Guimbard
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
METHOD OF DESIGNING A MULTISTAGE TURBINE FOR A TURBOMACHINE
- Publication number 20090155062
- Publication date Jun 18, 2009
- SNECMA
- Jean-Michel Bernard GUIMBARD
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
INTER-TURBINE CASING WITH COOLING CIRCUIT, AND TURBOFAN COMPRISING IT
- Publication number 20080232953
- Publication date Sep 25, 2008
- SNECMA
- Jean-Michel Bernard GUIMBARD
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE WITH CONTRAROTATING HP AND LP TURBINES
- Publication number 20080184694
- Publication date Aug 7, 2008
- SNECMA
- Jean-Michel Bernard Guimbard
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TRANSITION CHANNEL BETWEEN TWO TURBINE STAGES
- Publication number 20080085182
- Publication date Apr 10, 2008
- SNECMA
- Jean-Michel Bernard GUIMBARD
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
COOLING LAYOUT FOR A TURBINE BLADE, TURBINE BLADE INCLUDED THEREIN,...
- Publication number 20070122281
- Publication date May 31, 2007
- SNECMA
- Alexandre DERVAUX
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Stator turbine vane with improved cooling
- Publication number 20060233644
- Publication date Oct 19, 2006
- SNECMA MOTEURS
- Jean-Michel Guimbard
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbine distributor part supplied with cooling air
- Publication number 20060093470
- Publication date May 4, 2006
- SNECMA
- Sabine Bermond
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Cooled gas turbine blades
- Publication number 20040265129
- Publication date Dec 30, 2004
- SNECMA MOTEURS
- Philippe Pabion
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Annular platform for a nozzle of a low-pressure turbine of a turbom...
- Publication number 20040161336
- Publication date Aug 19, 2004
- SNECMA MOTEURS
- Sebastien Imbourg
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Jean-Michel Bernard GUIMBARD

Person

Patents Grantslast 30 patents

Blade with 3D platform comprising an inter-blade bulb

Turbine engine blade

Blade with non-axisymmetric platform

Optimized aerodynamic profile for a turbine vane, in particular for...

Optimized aerodynamic profile for a turbine vane, in particular for...

Optimized aerodynamic profile for a turbine blade, in particular fo...

Blade with non-axisymmetric platform: recess and boss on the extrados

Cooled blade for a turbomachine

Inter-turbine casing with cooling circuit, and turbofan comprising it

Method of designing a multistage turbine for a turbomachine

Transition channel between two turbine stages

Cooling layout for a turbine blade, turbine blade included therein,...

Stator turbine vane with improved cooling

Cooled gas turbine blades

Annular platform for a nozzle of a low-pressure turbine of a turbom...

Patents Applicationslast 30 patents

TURBOMACHINE COMBUSTION CHAMBER

BLADE WITH 3D PLATFORM COMPRISING AN INTER-BLADE BULB

Turbine engine blade

OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE VANE, IN PARTICULAR FOR...

OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE VANE, IN PARTICULAR FOR...

OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE, IN PARTICULAR FO...

BLADE WITH NON-AXISYMMETRIC PLATFORM: RECESS AND BOSS ON THE EXTRADOS

BLADE WITH 3D PLATFORM COMPRISING AN INTER-BLADE BULB

BLADE WITH NON-AXISYMMETRIC PLATFORM

METHOD OF DESIGNING A MULTISTAGE TURBINE FOR A TURBOMACHINE

INTER-TURBINE CASING WITH COOLING CIRCUIT, AND TURBOFAN COMPRISING IT

GAS TURBINE WITH CONTRAROTATING HP AND LP TURBINES

TRANSITION CHANNEL BETWEEN TWO TURBINE STAGES

COOLING LAYOUT FOR A TURBINE BLADE, TURBINE BLADE INCLUDED THEREIN,...

Stator turbine vane with improved cooling

Turbine distributor part supplied with cooling air

Cooled gas turbine blades

Annular platform for a nozzle of a low-pressure turbine of a turbom...