Patrick MARCONI

Person

Gelos, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Method for checking the maximum available power of a turbine engine...
- Patent number 11,459,960
- Issue date Oct 4, 2022
- SAFRAN HELICOPTER ENGINES
- Pierre Darfeuil
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Removable pack for reactivating a turboshaft engine, architecture f...
- Patent number 10,858,999
- Issue date Dec 8, 2020
- SAFRAN HELICOPTER ENGINES
- Patrick Marconi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turboshaft engine comprising a controlled mechanical coupling devic...
- Patent number 10,415,482
- Issue date Sep 17, 2019
- SAFRAN HELICOPTER ENGINES
- Patrick Marconi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turboshaft engine, twin-engine helicopter equipped with such a turb...
- Patent number 10,371,062
- Issue date Aug 6, 2019
- SAFRAN HELICOPTER ENGINES
- Patrick Marconi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Device and method for testing the integrity of a helicopter turbine...
- Patent number 10,253,699
- Issue date Apr 9, 2019
- SAFRAN HELICOPTER ENGINES
- Romain Thiriet
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Method and architecture for the optimized transfer of power between...
- Patent number 10,059,460
- Issue date Aug 28, 2018
- SAFRAN HELICOPTER ENGINES
- Pascal Dauriac
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
System and method for emergency starting of an aircraft turbomachine
- Patent number 9,951,694
- Issue date Apr 24, 2018
- SAFRAN AIRCRAFT ENGINES
- Romain Thiriet
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method and architecture for recombining the power of a turbomachine
- Patent number 9,422,863
- Issue date Aug 23, 2016
- Turbomeca
- Olivier Bedrine
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Power generation system for an aircraft using a fuel cell
- Patent number 7,986,052
- Issue date Jul 26, 2011
- Turbomeca
- Patrick Marconi
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
TURBOGENERATOR WITH SIMPLIFIED CONTROL SYSTEM FOR AIRCRAFT
- Publication number 20220213842
- Publication date Jul 7, 2022
- SAFRAN HELICOPTER ENGINES
- Fabien MERCIER-CALVAIRAC
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD FOR CHECKING THE MAXIMUM AVAILABLE POWER OF A TURBINE ENGINE...
- Publication number 20210108578
- Publication date Apr 15, 2021
- SAFRAN HELICOPTER ENGINES
- Pierre DARFEUIL
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
IGNITION SYSTEM FOR A COMBUSTION CHAMBER OF A TURBOSHAFT ENGINE
- Publication number 20170292491
- Publication date Oct 12, 2017
- SAFRAN HELICOPTER ENGINES
- Romain THIRIET
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Removable Pack for Reactivating a Turboshaft Engine, Architecture f...
- Publication number 20170241347
- Publication date Aug 24, 2017
- SAFRAN HELICOPTER ENGINES
- Patrick MARCONI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEVICE AND METHOD FOR TESTING THE INTEGRITY OF A HELICOPTER TURBINE...
- Publication number 20170218847
- Publication date Aug 3, 2017
- SAFRAN HELICOPTER ENGINES
- Romain Thiriet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Turboshaft engine, twin-engine helicopter equipped with SUCH a turb...
- Publication number 20170122221
- Publication date May 4, 2017
- SAFRAN HELICOPTER ENGINES
- Patrick MARCONI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEVICE FOR ASSISTING A SOLID PROPELLANT PROPULSION SYSTEM OF A SING...
- Publication number 20170114723
- Publication date Apr 27, 2017
- SAFRAN AIRCRAFT ENGINES
- Patrick Marconi
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOSHAFT ENGINE COMPRISING A CONTROLLED MECHANICAL COUPLING DEVIC...
- Publication number 20170101936
- Publication date Apr 13, 2017
- SAFRAN HELICOPTER ENGINES
- Patrick MARCONI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD FOR OPTIMISING THE SPECIFIC CONSUMPTION OF A TWIN HELICOPTER
- Publication number 20160237917
- Publication date Aug 18, 2016
- Turbomeca
- Patrick MARCONI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM AND METHOD FOR EMERGENCY STARTING OF AN AIRCRAFT TURBOMACHINE
- Publication number 20160230672
- Publication date Aug 11, 2016
- SNECMA
- Romain Thiriet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD AND ARCHITECTURE FOR THE OPTIMIZED TRANSFER OF POWER BETWEEN...
- Publication number 20150122944
- Publication date May 7, 2015
- Turbomeca
- Pascal Dauriac
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHOD OF OPTIMIZING THE SPECIFIC FUEL CONSUMPTION OF A TWIN ENGINE...
- Publication number 20130219905
- Publication date Aug 29, 2013
- Turbomeca
- Patrick Marconi
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD AND ARCHITECTURE FOR RECOMBINING THE POWER OF A TURBOMACHINE
- Publication number 20130098052
- Publication date Apr 25, 2013
- Turbomeca
- Olivier Bedrine
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD FOR ADAPTING THE AIR FLOW OF A TURBINE ENGINE HAVING A CENTR...
- Publication number 20130034425
- Publication date Feb 7, 2013
- Turbomeca
- Pierre Biscay
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
POWER GENERATION SYSTEM FOR AN AIRCRAFT USING A FUEL CELL
- Publication number 20090309364
- Publication date Dec 17, 2009
- Turbomeca
- Patrick Marconi
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

Patrick MARCONI

Person

Patents Grantslast 30 patents

Method for checking the maximum available power of a turbine engine...

Removable pack for reactivating a turboshaft engine, architecture f...

Turboshaft engine comprising a controlled mechanical coupling devic...

Turboshaft engine, twin-engine helicopter equipped with such a turb...

Device and method for testing the integrity of a helicopter turbine...

Method and architecture for the optimized transfer of power between...

System and method for emergency starting of an aircraft turbomachine

Method and architecture for recombining the power of a turbomachine

Power generation system for an aircraft using a fuel cell

Patents Applicationslast 30 patents

TURBOGENERATOR WITH SIMPLIFIED CONTROL SYSTEM FOR AIRCRAFT

METHOD FOR CHECKING THE MAXIMUM AVAILABLE POWER OF A TURBINE ENGINE...

IGNITION SYSTEM FOR A COMBUSTION CHAMBER OF A TURBOSHAFT ENGINE

Removable Pack for Reactivating a Turboshaft Engine, Architecture f...

DEVICE AND METHOD FOR TESTING THE INTEGRITY OF A HELICOPTER TURBINE...

Turboshaft engine, twin-engine helicopter equipped with SUCH a turb...

DEVICE FOR ASSISTING A SOLID PROPELLANT PROPULSION SYSTEM OF A SING...

TURBOSHAFT ENGINE COMPRISING A CONTROLLED MECHANICAL COUPLING DEVIC...

METHOD FOR OPTIMISING THE SPECIFIC CONSUMPTION OF A TWIN HELICOPTER

SYSTEM AND METHOD FOR EMERGENCY STARTING OF AN AIRCRAFT TURBOMACHINE

METHOD AND ARCHITECTURE FOR THE OPTIMIZED TRANSFER OF POWER BETWEEN...

METHOD OF OPTIMIZING THE SPECIFIC FUEL CONSUMPTION OF A TWIN ENGINE...

METHOD AND ARCHITECTURE FOR RECOMBINING THE POWER OF A TURBOMACHINE

METHOD FOR ADAPTING THE AIR FLOW OF A TURBINE ENGINE HAVING A CENTR...

POWER GENERATION SYSTEM FOR AN AIRCRAFT USING A FUEL CELL