Philippe Picot

Person

Le Chatelet-En-Brie, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Blade comprising a trailing edge having three distinct cooling regions
- Patent number 10,767,491
- Issue date Sep 8, 2020
- SAFRAN AIRCRAFT ENGINES
- Patrice Eneau
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Turbine or compressor stage including an interface part made of cer...
- Patent number 9,920,638
- Issue date Mar 20, 2018
- SNECMA
- Son Le Hong
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Optimized aerodynamic airfoil for a turbine blade
- Patent number 8,038,410
- Issue date Oct 18, 2011
- SNECMA
- Gregory Pierre Lafarge
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Optimized aerodynamic profile for a turbine blade
- Patent number 7,785,075
- Issue date Aug 31, 2010
- SNECMA
- Erwan Daniel Botrel
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Cooling circuits for a gas turbine blade
- Patent number 6,916,155
- Issue date Jul 12, 2005
- SNECMA Moteurs
- Patrice Eneau
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine blade cooling circuits
- Patent number 6,705,836
- Issue date Mar 16, 2004
- SNECMA Moteurs
- Isabelle Bourriaud
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
BLADE COMPRISING A TRAILING EDGE HAVING THREE DISTINCT COOLING REGIONS
- Publication number 20180306035
- Publication date Oct 25, 2018
- SAFRAN AIRCRAFT ENGINES
- Patrice ENEAU
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBINE OR COMPRESSOR STAGE INCLUDING AN INTERFACE PART MADE OF CER...
- Publication number 20150010404
- Publication date Jan 8, 2015
- SNECMA
- Son LE HONG
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
OPTIMIZED AERODYNAMIC AIRFOIL FOR A TURBINE BLADE
- Publication number 20080206061
- Publication date Aug 28, 2008
- SNECMA
- Gregory Pierre LAFARGE
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE
- Publication number 20070248465
- Publication date Oct 25, 2007
- SNECMA
- Erwan Daniel BOTREL
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Gas turbine blade cooling circuits
- Publication number 20030044277
- Publication date Mar 6, 2003
- SNECMA MOTEURS
- Isabelle Bourriaud
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Cooling circuits for a gas turbine blade
- Publication number 20030044278
- Publication date Mar 6, 2003
- SNECMA MOTEURS
- Patrice Eneau
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

Philippe Picot

Person

Patents Grantslast 30 patents

Blade comprising a trailing edge having three distinct cooling regions

Turbine or compressor stage including an interface part made of cer...

Optimized aerodynamic airfoil for a turbine blade

Optimized aerodynamic profile for a turbine blade

Cooling circuits for a gas turbine blade

Gas turbine blade cooling circuits

Patents Applicationslast 30 patents

BLADE COMPRISING A TRAILING EDGE HAVING THREE DISTINCT COOLING REGIONS

TURBINE OR COMPRESSOR STAGE INCLUDING AN INTERFACE PART MADE OF CER...

OPTIMIZED AERODYNAMIC AIRFOIL FOR A TURBINE BLADE

OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE

Gas turbine blade cooling circuits

Cooling circuits for a gas turbine blade