Alain Page

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Montgeron, FR

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Patents Grantslast 30 patents

Information Patent Grant
Device for mounting an air-flow dividing wall in a turbojet engine...
- Patent number 7,908,868
- Issue date Mar 22, 2011
- SNECMA
- Jacques Marcel Arthur Bunel
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbojet engine comprising an afterburner duct cooled by a variable...
- Patent number 7,870,740
- Issue date Jan 18, 2011
- SNECMA
- Jacques Marcel Arthur Bunel
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Exhaust cone for channeling a stream of gas downstream from a turbine
- Patent number 7,866,162
- Issue date Jan 11, 2011
- SNECMA
- Stephane Pierre Guillaume Blanchard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Exhaust assembly forming a horizontal propulsion gas elbow in an ai...
- Patent number 7,784,284
- Issue date Aug 31, 2010
- SNECMA
- Edgar Brunet
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Thrust orienting nozzle
- Patent number 7,631,486
- Issue date Dec 15, 2009
- SNECMA
- Alain Page
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbojet with protection means for a fuel injection device, an inje...
- Patent number 7,600,383
- Issue date Oct 13, 2009
- SNECMA
- Jacques Marcel Arthur Bunel
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Method of improving the ignition performance of an after-burner dev...
- Patent number 7,584,615
- Issue date Sep 8, 2009
- SNECMA
- Sébastien Baboeuf
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Elbow-shaped propulsion gas exhaust assembly in an aircraft
- Patent number 7,581,400
- Issue date Sep 1, 2009
- SNECMA
- Edgar Brunet
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turbo-jet engine with a protective screen of the fuel manifold of a...
- Patent number 7,574,866
- Issue date Aug 18, 2009
- SNECMA
- Jacques Andre Michel Roche
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Ventilation channels in an afterburner chamber confluence sheet
- Patent number 6,976,361
- Issue date Dec 20, 2005
- Snecma Moteurs
- Thierry Cortes
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

Patents Applicationslast 30 patents

Information Patent Application
TURBOJET ENGINE COMPRISING AN AFTERBURNER DUCT COOLED BY A VARIABLE...
- Publication number 20080110176
- Publication date May 15, 2008
- SNECMA
- Jacques Marcel Arthur BUNEL
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
EXHAUST CONE FOR CHANNELING A STREAM OF GAS DOWNSTREAM FROM A TURBINE
- Publication number 20080104941
- Publication date May 8, 2008
- SNECMA
- Stephane Pierre Guillaume BLANCHARD
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
ELBOW-SHAPED PROPULSION GAS EXHAUST ASSEMBLY IN AN AIRCRAFT
- Publication number 20070284005
- Publication date Dec 13, 2007
- SNECMA
- Edgar BRUNET
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
EXHAUST ASSEMBLY FORMING A HORIZONTAL PROPULSION GAS ELBOW IN AN AI...
- Publication number 20070266712
- Publication date Nov 22, 2007
- SNECMA
- Edgar Brunet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEVICE FOR MOUNTING AN AIR-FLOW DIVIDING WALL IN A TURBOJET ENGINE...
- Publication number 20070227152
- Publication date Oct 4, 2007
- SNECMA
- Jacques Marcel Arthur BUNEL
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
THRUST ORIENTING NOZZLE
- Publication number 20070000233
- Publication date Jan 4, 2007
- SNECMA
- Alain Page
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Turbojet with protection means for a fuel injection device, an inje...
- Publication number 20060016192
- Publication date Jan 26, 2006
- SNECMA
- Jacques Marcel Arthur Bunel
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Turbo-jet engine with a protective screen of the fuel manihold of a...
- Publication number 20060016193
- Publication date Jan 26, 2006
- SNECMA
- Jacques Andre Michel Roche
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
VENTILATION CHANNELS IN AN AFTERBURNER CHAMBER CONFLUENCE SHEET
- Publication number 20050274114
- Publication date Dec 15, 2005
- SNECMA MOTEURS
- Thierry Cortes
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Method of improving the ignition performance of an after-burner dev...
- Publication number 20050257527
- Publication date Nov 24, 2005
- SNECMA MOTEURS
- Sebastien Baboeuf
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Person

Patents Grantslast 30 patents

Device for mounting an air-flow dividing wall in a turbojet engine...

Turbojet engine comprising an afterburner duct cooled by a variable...

Exhaust cone for channeling a stream of gas downstream from a turbine

Exhaust assembly forming a horizontal propulsion gas elbow in an ai...

Thrust orienting nozzle

Turbojet with protection means for a fuel injection device, an inje...

Method of improving the ignition performance of an after-burner dev...

Elbow-shaped propulsion gas exhaust assembly in an aircraft

Turbo-jet engine with a protective screen of the fuel manifold of a...

Ventilation channels in an afterburner chamber confluence sheet

Patents Applicationslast 30 patents

TURBOJET ENGINE COMPRISING AN AFTERBURNER DUCT COOLED BY A VARIABLE...

EXHAUST CONE FOR CHANNELING A STREAM OF GAS DOWNSTREAM FROM A TURBINE

ELBOW-SHAPED PROPULSION GAS EXHAUST ASSEMBLY IN AN AIRCRAFT

EXHAUST ASSEMBLY FORMING A HORIZONTAL PROPULSION GAS ELBOW IN AN AI...

DEVICE FOR MOUNTING AN AIR-FLOW DIVIDING WALL IN A TURBOJET ENGINE...

THRUST ORIENTING NOZZLE

Turbojet with protection means for a fuel injection device, an inje...

Turbo-jet engine with a protective screen of the fuel manihold of a...

VENTILATION CHANNELS IN AN AFTERBURNER CHAMBER CONFLUENCE SHEET

Method of improving the ignition performance of an after-burner dev...