Patrick Morel

Person

Chartrette, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Device adapted to be fitted with propeller blades
- Patent number 8,622,699
- Issue date Jan 7, 2014
- SNECMA
- François Gallet
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Three-spool by-pass turbojet with a high by-pass ratio
- Patent number 7,299,621
- Issue date Nov 27, 2007
- SNECMA Moteurs
- Jacques Bart
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Breakable coupling system for a turbojet fan shaft
- Patent number 7,237,959
- Issue date Jul 3, 2007
- SNECMA Moteurs
- Gael Bouchy
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Device for supporting and recentering the shaft of a turbojet fan a...
- Patent number 6,799,416
- Issue date Oct 5, 2004
- SNECMA Moteurs
- Daniel Plona
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Oil separator rotor for lubrication enclosure
- Patent number 5,776,229
- Issue date Jul 7, 1998
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Gerard Antoine Gilbert Blanes
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
DEVICE ADAPTED TO BE FITTED WITH PROPELLER BLADES
- Publication number 20110176924
- Publication date Jul 21, 2011
- SNECMA
- François Gallet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
BLEED SYSTEM FOR A LOW-PRESSURE COMPRESSOR OF A TURBOMACHINE
- Publication number 20080063515
- Publication date Mar 13, 2008
- SNECMA
- Eric Stephan BIL
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbomachine with a decoupling device common to first and second be...
- Publication number 20060110244
- Publication date May 25, 2006
- SNECMA
- Michel Gilbert Roland Brault
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Three-spool by-pass turbojet with a high by-pass ratio
- Publication number 20050241291
- Publication date Nov 3, 2005
- SNECMA MOTEURS
- Jacques Bart
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbojet having two counter-rotatable fans secured to a counter-rot...
- Publication number 20050172610
- Publication date Aug 11, 2005
- SNECMA MOTEURS
- Jacques Bart
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Arrangement of bearing supports for the rotating shaft of an aircra...
- Publication number 20050129343
- Publication date Jun 16, 2005
- SNECMA MOTEURS
- Gael Bouchy
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Breakable coupling system for a turbojet fan shaft
- Publication number 20050117828
- Publication date Jun 2, 2005
- Gael Bouchy
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Device for supporting and recentering the shaft of a turbojet fan a...
- Publication number 20030182926
- Publication date Oct 2, 2003
- SNECMA MOTEURS
- Daniel Plona
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patrick Morel

Person

Patents Grantslast 30 patents

Device adapted to be fitted with propeller blades

Three-spool by-pass turbojet with a high by-pass ratio

Breakable coupling system for a turbojet fan shaft

Device for supporting and recentering the shaft of a turbojet fan a...

Oil separator rotor for lubrication enclosure

Patents Applicationslast 30 patents

DEVICE ADAPTED TO BE FITTED WITH PROPELLER BLADES

BLEED SYSTEM FOR A LOW-PRESSURE COMPRESSOR OF A TURBOMACHINE

Turbomachine with a decoupling device common to first and second be...

Three-spool by-pass turbojet with a high by-pass ratio

Turbojet having two counter-rotatable fans secured to a counter-rot...

Arrangement of bearing supports for the rotating shaft of an aircra...

Breakable coupling system for a turbojet fan shaft

Device for supporting and recentering the shaft of a turbojet fan a...