Francois LEGLAYE

Person

Vaux Le Penil, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Convergent-divergent flap pair for a variable-geometry turbojet eng...
- Patent number 11,739,712
- Issue date Aug 29, 2023
- SAFRAN AIRCRAFT ENGINES
- François Leglaye
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Convergent-divergent flap pair for a variable-geometry turbojet eng...
- Patent number 11,713,730
- Issue date Aug 1, 2023
- SAFRAN AIRCRAFT ENGINES
- Thierry Kohn
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbomachine combustion chamber provided with air deflection means...
- Patent number 10,233,836
- Issue date Mar 19, 2019
- SAFRAN AIRCRAFT ENGINES
- Francois Leglaye
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Turbine engine, such as a turbojet or a turboprop engine
- Patent number 10,190,430
- Issue date Jan 29, 2019
- SAFRAN AIRCRAFT ENGINES
- Francois Leglaye
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine engine wall having at least some cooling orifices that are...
- Patent number 9,995,219
- Issue date Jun 12, 2018
- SNECMA
- Francois Leglaye
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbomachine sparkplug fixing assembly
- Patent number 9,982,603
- Issue date May 29, 2018
- SNECMA
- Pierre-François Simon Paul Pireyre
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Spark plug for combustion chamber of a gas turbine engine
- Patent number 9,413,141
- Issue date Aug 9, 2016
- SNECMA
- Francois Leglaye
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENG...
- Publication number 20220290631
- Publication date Sep 15, 2022
- SAFRAN AIRCRAFT ENGINES
- Thierry KOHN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENG...
- Publication number 20220275771
- Publication date Sep 1, 2022
- SAFRAN AIRCRAFT ENGINES
- François LEGLAYE
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOMACHINE SPARKPLUG FIXING ASSEMBLY
- Publication number 20160369701
- Publication date Dec 22, 2016
- SNECMA
- Pierre-Francois Simon Paul Pireyre
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOMACHINE COMBUSTION CHAMBER PROVIDED WITH AIR DEFLECTION MEANS...
- Publication number 20160237896
- Publication date Aug 18, 2016
- SNECMA
- Francois LEGLAYE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE ENGINE WALL HAVING AT LEAST SOME COOLING ORIFICES THAT ARE...
- Publication number 20150338103
- Publication date Nov 26, 2015
- SNECMA
- Francois LEGLAYE
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
ANNULAR WALL FOR TURBOMACHINE COMBUSTION CHAMBER COMPRISING COOLING...
- Publication number 20150167977
- Publication date Jun 18, 2015
- SNECMA
- Francois LEGLAYE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE ENGINE, SUCH AS A TURBOJET OR A TURBOPROP ENGINE
- Publication number 20150047356
- Publication date Feb 19, 2015
- SNECMA
- Francois Leglaye
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
SPARK PLUG FOR COMBUSTION CHAMBER OF A GAS TURBINE ENGINE
- Publication number 20130327013
- Publication date Dec 12, 2013
- SNECMA
- Francois LEGLAYE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Francois LEGLAYE

Person

Patents Grantslast 30 patents

Convergent-divergent flap pair for a variable-geometry turbojet eng...

Convergent-divergent flap pair for a variable-geometry turbojet eng...

Turbomachine combustion chamber provided with air deflection means...

Turbine engine, such as a turbojet or a turboprop engine

Turbine engine wall having at least some cooling orifices that are...

Turbomachine sparkplug fixing assembly

Spark plug for combustion chamber of a gas turbine engine

Patents Applicationslast 30 patents

CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENG...

CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENG...

TURBOMACHINE SPARKPLUG FIXING ASSEMBLY

TURBOMACHINE COMBUSTION CHAMBER PROVIDED WITH AIR DEFLECTION MEANS...

TURBINE ENGINE WALL HAVING AT LEAST SOME COOLING ORIFICES THAT ARE...

ANNULAR WALL FOR TURBOMACHINE COMBUSTION CHAMBER COMPRISING COOLING...

TURBINE ENGINE, SUCH AS A TURBOJET OR A TURBOPROP ENGINE

SPARK PLUG FOR COMBUSTION CHAMBER OF A GAS TURBINE ENGINE