Georges Mazeaud

Person

Yerres, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Device for supporting and housing auxiliaries in a bypass turbojet
- Patent number 7,805,949
- Issue date Oct 5, 2010
- SNECMA
- Georges Mazeaud
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbojet engine comprising a connector arm for ancillary systems, a...
- Patent number 7,543,442
- Issue date Jun 9, 2009
- SNECMA
- Jacky Derenes
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbofan jet engine with ancillaries distribution support
- Patent number 7,506,499
- Issue date Mar 24, 2009
- SNECMA
- Jeremy Fert
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Air input device for a turboprop engine
- Patent number 7,461,813
- Issue date Dec 9, 2008
- SNECMA
- Michel Chaumeret
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turboprop carrier structure and an assembly including such a carrie...
- Patent number 7,100,869
- Issue date Sep 5, 2006
- SNECMA Moteurs
- Jean-Louis Picard
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turbojet designed to be fixed onto the AFT part of the fuselage of...
- Patent number 7,007,890
- Issue date Mar 7, 2006
- SNECMA Moteurs
- Bruno Beutin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Suspension system with intrinsic safety features for aircraft power...
- Patent number 6,474,596
- Issue date Nov 5, 2002
- SNECMA Moteurs
- Antoine Emmanuel Cousin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Particle traps for turbo-prop engine
- Patent number 6,129,509
- Issue date Oct 10, 2000
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Antoine Emmanuel Cousin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Cooling device for a turboshaft engine on an aircraft
- Patent number 5,806,793
- Issue date Sep 15, 1998
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Pascal Noel Brossier
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas-turbine engine with detachable combustion chamber
- Patent number 5,524,430
- Issue date Jun 11, 1996
- Societe National d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
- Georges Mazeaud
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Aircraft engine layout
- Patent number 5,410,870
- Issue date May 2, 1995
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Michel G. R. Brault
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Combined jet engine with RAM jet and turbojet
- Patent number 5,347,807
- Issue date Sep 20, 1994
- Societe Nationale D'Etude et de Construction de Moteurs d'Aviaton "SNECMA"
- Pascal N. Brossier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Combined jet engine provided with means for switching between two o...
- Patent number 5,343,695
- Issue date Sep 6, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Noel B. Pascal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Circuit for ventilating compressor and turbine disks
- Patent number 5,327,719
- Issue date Jul 12, 1994
- Societe Nationale d'Etude et de Construction de Moteurs D'Avaiation "SNECMA"
- Georges Mazeaud
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Propulsion engine
- Patent number 5,305,600
- Issue date Apr 26, 1994
- Societe Nationale d'Etude et de Construction de Motors d'Aviation "S.N.E.C.M.A."
- Pascal Brossier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbojet-ramjet hypersonic aircraft engine
- Patent number 5,284,014
- Issue date Feb 8, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation ("S.N.E.C....
- Pascal N. Brossier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Axial compressor and method of carrying out maintenance on the axia...
- Patent number 5,275,532
- Issue date Jan 4, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Georges Mazeaud
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Hollow turbine blade with internal cooling system
- Patent number 5,193,980
- Issue date Mar 16, 1993
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Christian Kaincz
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Cooling system for a gas turbine
- Patent number 5,163,285
- Issue date Nov 17, 1992
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Georges Mazeaud
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Combination turbojet-ramjet-rocket propulsion system
- Patent number 5,052,176
- Issue date Oct 1, 1991
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation
- Josiane M. F. Labatut
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbo-machine with device for automatically controlling the rate of...
- Patent number 4,805,398
- Issue date Feb 21, 1989
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Gerard E. A. Jourdain
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Means for controlling clearance in an intershaft bearing journal of...
- Patent number 4,500,143
- Issue date Feb 19, 1985
- SNECMA
- Robert Kervistin
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Inter-shaft bearing for multibody turbojet engines with damping by...
- Patent number 4,378,197
- Issue date Mar 29, 1983
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation, "S.N.E.C....
- Christian J. Cattaneo
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
DEVICE FOR SUPPORTING AND HOUSING AUXILIARIES IN A BYPASS TURBOJET
- Publication number 20070084216
- Publication date Apr 19, 2007
- SNECMA
- Georges MAZEAUD
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Air input device for a turboprop engine
- Publication number 20070063097
- Publication date Mar 22, 2007
- SNECMA MOTEURS
- Michel Chaumeret
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Turbofan jet engine with ancillaries distribution support
- Publication number 20050247042
- Publication date Nov 10, 2005
- SNECMA MOTEURS
- Jeremy Fert
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbojet engine comprising a connector arm for ancillary systems, a...
- Publication number 20050247043
- Publication date Nov 10, 2005
- SNECMA MOTEURS
- Jacky Derenes
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbojet designed to be fixed onto the AFT part of the fuselage of...
- Publication number 20050178887
- Publication date Aug 18, 2005
- SNECMA MOTEURS
- Bruno Beutin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Cooling system for hot parts of an aircraft engine, and aircraft en...
- Publication number 20050150970
- Publication date Jul 14, 2005
- SNECMA MOTEURS
- Bruno Beutin
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Application
Turboprop carrier structure and an assembly including such a carrie...
- Publication number 20040227033
- Publication date Nov 18, 2004
- SNECMA MOTEURS
- Jean-Louis Picard
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Georges Mazeaud

Person

Patents Grantslast 30 patents

Device for supporting and housing auxiliaries in a bypass turbojet

Turbojet engine comprising a connector arm for ancillary systems, a...

Turbofan jet engine with ancillaries distribution support

Air input device for a turboprop engine

Turboprop carrier structure and an assembly including such a carrie...

Turbojet designed to be fixed onto the AFT part of the fuselage of...

Suspension system with intrinsic safety features for aircraft power...

Particle traps for turbo-prop engine

Cooling device for a turboshaft engine on an aircraft

Gas-turbine engine with detachable combustion chamber

Aircraft engine layout

Combined jet engine with RAM jet and turbojet

Combined jet engine provided with means for switching between two o...

Circuit for ventilating compressor and turbine disks

Propulsion engine

Turbojet-ramjet hypersonic aircraft engine

Axial compressor and method of carrying out maintenance on the axia...

Hollow turbine blade with internal cooling system

Cooling system for a gas turbine

Combination turbojet-ramjet-rocket propulsion system

Turbo-machine with device for automatically controlling the rate of...

Means for controlling clearance in an intershaft bearing journal of...

Inter-shaft bearing for multibody turbojet engines with damping by...

Patents Applicationslast 30 patents

DEVICE FOR SUPPORTING AND HOUSING AUXILIARIES IN A BYPASS TURBOJET

Air input device for a turboprop engine

Turbofan jet engine with ancillaries distribution support

Turbojet engine comprising a connector arm for ancillary systems, a...

Turbojet designed to be fixed onto the AFT part of the fuselage of...

Cooling system for hot parts of an aircraft engine, and aircraft en...

Turboprop carrier structure and an assembly including such a carrie...